002---FAA Structure
IBM Maximo for Aviation 7.6.4 快速入门指南说明书
IBM Maximo for AviationVersion 7.6.4Quick Start GuideThis guide introduces IBM Maximo for Aviation Version 7.6.4, provides a link to a list of prerequisite software, gets you started with a typical installation, and provides a roadmap to other important information.National Language Version:To obtain the Quick Start Guide in other languages, print the language-specific PDF file from the installation media.Product overviewIBM ®Maximo ®for Aviation provides aviation organizations with features to schedule and manage aircraft maintenance to maintain regulatory compliance and minimize periods when an aircraft is grounded. The efficient maintenance, repair, and overhaul of aircraft increases flight availability and extends the life of airframes, engines, and other components of an aircraft.For complete information, including installation instructions, see IBM Knowledge Center (/support/knowledgecenter/SS5RRF_7.6.4/com.ibm.mavm.doc/welcome.html).2Step 2: Plan the installationYou install Maximo for Aviation on a Microsoft Windows administrative workstation. Ensure that IBM Maximo Asset Management version 7.6.0.6 is installed on the same administrative workstation where you plan to install Maximo for Aviation version 7.6.4, and in the same language as Maximo for Aviation version 7.6.4.You must have system administrator rights and privileges to install the product.For information about the hardware, software, and network requirements for your product, see the System Requirements section in the Overview and Planning page on the Maximo Asset Management wiki (https:///developerworks/community/wikis/home?lang=en#!/wiki/IBM%20Maximo%20Asset%20Management/page/Overview%20and%20planning)3Step 3: Install the productTo install Maximo for Aviation:1.Review the software requirements.2.Prepare to install.3.Install Maximo for Aviation.For Oracle WebLogic Server environments only: you must deploy the Enterprise Application Archive (EAR) files.For IBM WebSphere ®Application Server environments: The EAR files are installed when you install the process automation engine. If this task was deferred during the Maximo for Aviation installation, deploy the EAR files.Detailed installation instructions are in the IBM Maximo for Aviation, 7.6.4 Installation Guide in IBM Knowledge Center (/support/knowledgecenter/SS5RRF_7.6.4/com.ibm.mavm.doc/welcome.html).More informationAfter you install the product, use IBM Knowledge Center to learn more about the product.For more information, see the following resources:v Product support (https:///support/entry/portal/product/tivoli/ibm_maximo_for_aviation )v IBM User Communities (https:///social/aggregator/ibm)IBM®Maximo for Aviation Licensed Materials - Property of IBM. © Copyright IBM Corp. 2016. U.S. Government Users Restricted Rights - Use, duplication or disclosure restricted by GSA ADP Schedule Contract with IBM Corp.IBM, the IBM logo, and are trademarks or registered trademarks of International Business Machines Corp., registered in many jurisdictions worldwide. Other product and service names might be trademarks of IBM or other companies. A current list of IBM trademarks is available on the Web at “Copyright and trademark information” (/legal/copytrade.shtml).Printed in Ireland。
美国FAA民航局零部件认证程序
How Parts Are Made And CertifiedNote: The following is an introductory guideline to the sale of parts for installation in an aircraft. It is a summary only and does not cover all applicable laws, regulations, situations, exceptions, or sales. It is not meant to, nor does it, substitute for specific legal advice with respect to the installation of any particular part in any particular aircraft or with respect to any specific transaction involving the sale of any particular parts. Please consult your own advisors with respect to the installation of any particular parts in your aircraft.Commander Premier Aircraft Corporation wants all Commander owners to fly safely, responsibly, and in conformity with all FAA regulations. Among other things, this requires that an owner have a basic understanding of how and why the FAA regulates the aircraft parts business. While this is not meant to be a complete summary, or to cover all situations, it should help familiarize Commander owners with this area and provoke questions they can ask their A & P mechanics when installing parts in their own Commander aircraft.We want to help Commander owners avoid potential problems and liability that may result from the installation of uncertified parts in their aircraft. These are parts that are produced for sale, or purchased for resale, to Commander owners that are not produced under an FAA certification process. Those parts may appear to (and, it's possible that they could, in fact) be identical to parts that would be sold by the factory under an FAA approved Quality System. However, because such parts are manufactured and sold without being inspected under an FAA approved and monitored Quality System, there is no way that a buyer can be independently assured that such a part is in conformity with the aircraft’s design data or made from the materials specified in the design data.As a basic principal, no part may be sold for installation in an aircraft to be flown in the United States unless that part is made and sold under one or more authorizations issued by the FAA. If the part is sold by a factory with a type certificate for a particular aircraft, its sale may be covered by either a production certificate or parts manufacturing authority. Or, the factory may request that an FAA inspector come to the factory to inspect parts and compare them to specifications and drawings before they are shipped to assure their conformity with aircraft design data. A manufacturer that sells parts only to the factory (not directly to aircraft owners) may not be directly regulated by the FAA. However, if such a manufacturer wants to sell parts directly to aircraft owners (even parts originally produced for the design owner), then it must subject itself to the FAA regulatory process, obtain the required authorizations and maintain the required Quality System.The regulatory system is designed to assure an aircraft owner that a part sold for installation in a type certified aircraft was made to the original design data in all respects or to specifications specifically approved by the FAA. Often times people who sell illegal parts "redesign" the part (perhaps without changing their part number) because of eithercost considerations or because they think the change is unimportant or an improvement. They may also sell the part for less money than a factory certified part because they skip the high cost of the FAA approval process. This is especially true if the original manufacturer is no longer selling the part to the factory and is operating free of any factory surveillance program. Of course, without any FAA oversight, the part may not be as represented to the aircraft owner. The owner would have only the assurance of the private seller that the part is what it is represented to be. And, even if it is as represented, its sale for installation in an aircraft is still illegal because the part is undocumented and its conformity is not assured by an FAA approved Quality System.This would be true even if the owner buys the part from the same vendor as the one from whom the factory would buy the part for resale to owners. In such a case, it is the factory, not the manufacturer, that is directly regulated by the FAA. It is the responsibility of the factory to monitor the manufacturer (the FAA calls it “surveillance”) under specific FAA guidelines and the FAA oversees the quality of those parts through the factory and the surveillance program of the factory. (In effect, the FAA treats the factory as if the factory, not the manufacturer, produced those parts.) As a result, the factory cannot sell a part it purchases from a manufacturer without first inspecting that part to assure the aircraft owner (and the FAA) that the part meets the design data specifications. This process must be fully documented by the factory for every part shipped.When the manufacturer sells such a modified part directly to an aircraft owner, such part (while perhaps bearing the same part number as the one shown on the factory list of parts) will NOT conform to the aircraft design data. And, even if the part specifications have not been changed, and the part fully conforms to the original specifications, without proper documentation under an FAA certification process, it is illegal to install such part in an aircraft. Such a part will be deemed to be non-conforming because of the lack of documented compliance with an FAA approved Quality System.So, what must an aircraft manufacturer do under an FAA approved Quality System before it can ship a part to a customer for installation in an aircraft? First, the individual part must be inspected by the factory for conformity with the aircraft’s design data. To do that, the factory employee designated under the factory's Quality System must actually physically inspect the part and compare it to design specifications and drawings (or the factory must request that an FAA Inspector come to the factory to inspect the part). And, records of each such inspection must be maintained. That's how everyone who flies in an airplane in the United States can be assured that all aircraft with replacement parts (nearly all aircraft more than a year old) will continue to perform in accordance with the standards of their FAA approved type designs. This process costs the factory a substantial amount of money with respect to each part shipped (without regard to the cost of the part, itself). Obviously, the inspection and certification cost must be built into the price of factory parts. However, that's the only way the FAA can assure all of us who share the sky that the aircraft we fly, and those flying around us, are not going to fail because of substandard parts.The FAA takes the sale of unauthorized parts very seriously. The FAA will fine sellers of unauthorized parts up to $1,100 for each individual item sold. And, a plane with such parts installed may be considered by the FAA to no longer conform to the design data basis for the issuance of its airworthiness certificate. (Installing such a part in an aircraft is similar to modifying an aircraft without a Supplemental Type Certificate or specific FAA approval). This means that once such a part is installed in an aircraft, it may not be legal to fly the aircraft without a specific sign off from the FAA.The presence of an illegally sold part in your aircraft could also void your aircraft insurance under the terms of your policy, even if the accident is wholly unrelated to the illegal part. Once you modify an aircraft from its type design, you can't fly it under the airworthiness certificate issued for it as a type certified (vs. experimental) aircraft. Therefore, if you install an uncertified part you may be flying your plane without a valid airworthiness certificate (unless you get specific FAA approval for the modification). This may be an "out" under your aircraft insurance policy. Even if you get such approval from the FAA for the installation of such part, and it is legal to fly your aircraft, your aircraft may no longer be eligible for insurance as a type certified (vs. experimental) aircraft.Finally, because the installation of an illegally sold part can constitute a “modification” to the aircraft, the aircraft owner that installs such a part may thereafter be deemed to be the “manufacturer” of the aircraft for legal purposes. If the plane is ever in an accident, and a jury determines that there is manufacturer's liability for any reason (however unrelated to the part), the owner may be deemed to be “the manufacturer” of the aircraft and held responsible for that aircraft for all purposes. That could become even more important if the owner sells the aircraft with the illegal part in it and the buyer suffers an accident. We recognize that the absence of factory parts since Commander Aircraft Company stopped shipping parts in 2004 has created a tremendous hardship. We understand the frustration and desperation that this has caused among Commander owners who want to keep their aircraft flying. That is why the establishment of parts and maintenance operations are at the top of our priority list. With the move to our new location at Cape Girardeau now well under way, we hope to have our parts and service operations open for business around the first of the year.Unfortunately, when parts for any aircraft are in short supply and unavailable from a factory source, owner frustration creates an “opportunity” for others to fill the void with the illegal sale of parts. Because aircraft owners often do not understand the FAA requirements for manufacturing and selling replacement parts for aircraft, they may be tempted to buy parts that cannot legally be installed in their aircraft without specific FAA approval and without taking on substantial risk. We hope that this brief summary will prompt all Commander owners to learn more about this area so that they can avoid the pitfalls of installing illegally sold parts in their Commander aircraft.Notice: The foregoing is meant to promote the safe, responsible, and legal use of Commander aircraft. It is meant to promote awareness of the FAA regulatory system thatapplies to this area and to prompt further inquiry by responsible aircraft owners seeking parts for their aircraft. It is not meant to be a complete summary of this area of the law or to constitute legal advice. Neither is it meant to refer to any particular situation or to any particular party who may be selling parts for Commander aircraft (the Company having no direct knowledge that any particular party has engaged in the illegal sale of any particular part). Please be aware that NO PARTY HAS BEEN PROVIDED WITH PARTS by either Commander Premier Aircraft Corporation or CPAC, Inc. TO HOLD FOR SALE AS REPLACEMENT PARTS directly to owners of Commander aircraft. Any representation by any party to the contrary is untrue and should be brought to the attention of the FAA.。
A-T Controls FD9-F3 300# Direct Mount Split Body F
FD9F3Series-20180205Copyright 2013 A-T Controls, Inc.ElectricPneumaticCincinnati, Ohio SERIES FD9 300# Direct Mount Split Body Flanged Ball Valve FiresafeSee automated data sheets for pre-sized assembliesEasy to Automate!Triac FD9 Series Flanged Ball Valves feature adirect mount automation pad. The high quality investment castings feature a fully machined bore. The superior live-loaded packing system is accomplished with Belleville washers, “V” ring packing and a unique primary pyramidal stem seal. This advanced sealing system provides protection against stem leaks experienced by ordinary ball valves.C E R T I F I E DFAX (513) 247-5462********************High Performance, Full Port300# Split Body Flanged Ball Valve Series FD9-F3 (ANSI Class 300)A-T Controls reserves the right to change product designs and technical/dimensional specifications without notice.9955 International Blvd.Cincinnati, Ohio 45246PHONE (513) 247-5465FAX (513) 247-5462********************Pressure vs. Temperature Chart for Valves 1/2” to 6”FD9F3DA-20180205Copyright 2013 A-T Controls, Inc.300# FlangedFiresafe Tested to API-607Direct Mount9955 International Blvd.Cincinnati, Ohio PHONE (513) 247-5465FAX (513) 247-5462********************C E R T I F I E DSERIES FD9-F3 300# Flanged Direct Mount FiresafeFD9F3SR-20180205Copyright 2013 A-T Controls, Inc.300# FlangedFiresafe Tested to API-607Direct Mount9955 International Blvd.Cincinnati, Ohio PHONE (513) 247-5465FAX (513) 247-5462********************Actuators are sized based on clean/clear fluid.API 607 - 6th EditionC E R T I F I E DSAMPLE PART #Valve Series Carbon Steel Valve SizeSeat MaterialEnd ConnectionTRIAC Actuator SeriesActuator Size Spring ReturnSolenoidLimit SwitchFiresafeSee valve part number matrix for complete part number and options.FD9C-3X-150/2R3S-XXSERIES FD9-F3 300# Flanged Direct Mount Firesafe300# Flanged Firesafe Tested to API-607Direct Mount9955 International Blvd. Cincinnati, Ohio 45246 PHONE (513) 247-5465 FAX (513) 247-5462********************Other options available - call for details Actuators are sized based on clean/clear fluid.API 607 - 6th EditionC E R T I F I ED SERIES FD9-F3300# Flanged Direct Mount FiresafeFD9F3EL-20180205 Copyright 2013 A-T Controls, Inc.Manual and automated valve assemblies for gas burner management applicationsand safety shutoffVarious Seat MaterialsPTFE, RTFE, 50/50 STFE, 25% CTFE, Delrin,PEEK, UHMWPE, TFM-1600Operator OptionsQuarter-turn Gear OperatorsSpring Return “Deadman” HandlesOval handles, TEE HandlesSpecials and SolutionsSteam JacketsStem ExtensionsV-ported Control ValvesMulti-port Valve SolutionsFugitive Emissions Bonnets (TSM’s)Oxygen CleaningLockout BracketsVented Balls“No Play” Mounting Kits• FM ApprovedValves and AssembliesSpecial SeatsBalls and Seal DesignsFloor MountedDamper DrivesFusible LinkAssembliesLockoutMounting KitsSpecialMulti-Port ValvesSteam JacketedValvesLimit SwitchesMounted on Manual Valves180º ActuatorsStem ExtensionsDual ValveAssembliesCincinnati, Ohio 45246FAX (513) 247-5462********************。
Schlumberger - Well Integrity Program 斯伦贝谢井眼完整性程序
Well Integrity Framework
Component of our “Excellence in Execution” Program
Schlumberger Confidential
Schlumberger Well Integrity Program
Hussam Al Quassar MEA WSV Technique Manager
Well Integrity
Recent industry incidents led to an increase focus on Well Integrity.
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车缝拉力标准
车缝拉力标准通常是指用于测试车缝（缝纫线或线缝）的强度和耐久性的相关标准。
这些标准通常由国际、国家或行业标准组织制定，并用于评估缝纫线的性能，以确保其符合特定用途的要求。
以下是一些常见的车缝拉力标准的示例：1. **ASTM D2256 - Standard Test Method for Tensile Properties of Yarns by the Single-Strand Method**：这是美国材料和试验协会（ASTM）发布的标准，用于测试纱线的拉伸性能。
2. **ISO 2062 - Textiles - Yarns from Packages - Determination of Single-End Breaking Force and Elongation at Break Using the Grab Method**：这是国际标准化组织（ISO）发布的标准，用于测试纱线的单头断裂力和断裂伸长率。
3. **EN ISO 13934-1 - Textiles - Tensile Properties of Fabrics - Part 1: Determination of Maximum Force and Elongation at Maximum Force Using the Strip Method**：这是欧洲标准化委员会（CEN）和国际标准化组织（ISO）发布的标准，用于测试织物的最大拉力和最大拉伸率。
4. **GB/T 3923.1-2013 - Textiles - Tensile Properties of Fabrics - Part 1: Determination of Maximum Force and Elongation at Maximum Force**：这是中国国家标准，用于测试织物的最大拉力和最大拉伸率。
这些标准通常包括实验方法，以便在标准化条件下测试车缝的拉力性能。
jboss-deployment-structure 的声明 -回复
jboss-deployment-structure 的声明-回复JBoss中的Deployment Structure（部署结构）是指配置JBoss应用服务器上部署的应用程序的特定方式。
通过调整部署结构，开发人员可以对应用程序进行精确控制，以满足特定的需求和要求。
本文将深入探讨JBoss Deployment Structure的声明并详细介绍其各个方面。
第一部分：什么是JBoss Deployment StructureJBoss Deployment Structure是一种管理和组织应用程序部署的方法。
它定义了应用程序的目录结构、库的位置、模块依赖关系以及其他相关配置。
通过使用JBoss Deployment Structure，开发人员可以确保应用程序能够在JBoss应用服务器中顺利运行，并与其他应用程序和资源进行正确的交互。
第二部分：JBoss Deployment Structure的主要组件1. META-INF目录：该目录包含应用程序的元数据信息，如MANIFEST.MF 文件、persistence.xml文件等。
这些文件用于配置应用程序的行为和特性。
2. WEB-INF目录：该目录是用于Web应用程序的特定目录，它包含了应用程序的配置文件、类文件、静态资源等。
在WEB-INF目录下，还可以有lib目录用于存放应用程序所需的库文件。
3. JBoss Modules：JBoss Deployment Structure支持使用JBoss Modules来管理和组织应用程序的依赖关系。
通过在模块描述文件module.xml中定义模块的依赖关系，开发人员可以确保应用程序能够正确载入所需的模块。
4. Classpath：JBoss Deployment Structure允许开发人员自定义类加载路径。
通过在jboss-deployment-structure.xml文件中配置<class-loading>元素，开发人员可以定义特定的类加载行为，以确保应用程序能够正确访问所需的类。
AJA FS2 Installation and Operation Guide
AJA FS2 Installation and Operation Installation and Operation GuideB e c a u s e i t m a t t e r s .7/31/2012 Version: 1.1.0.0TrademarksAJA®, KONA®, Ki Pro®, KUMO®, and XENA® are registered trademarks of AJA Video, Inc. Io Express™,Io HD™ and Io™ are trademarks of AJA Video, Inc. Apple, the Apple logo, AppleShare, AppleTalk,FireWire, iPod, iPod Touch, Mac, and Macintosh are registered trademarks of Apple Computer, Inc.Final Cut Pro, QuickTime and the QuickTime Logo are trademarks of Apple Computer, Inc. All othertrademarks are the property of their respective holders.NoticeCopyright © 2012 AJA Video, Inc. All rights reserved. All information in this manual is subject tochange without notice. No part of the document may be reproduced or transmitted in any form,or by any means, electronic or mechanical, including photocopying or recording, without theexpress written permission of AJA Inc.FCC Emission InformationThis equipment has been tested and found to comply with the limits for a Class A digital device,pursuant to Part 15 of the FCC Rules. These limits are designed to provide reasonable protectionagainst harmful interference when the equipment is operated in a commercial environment. Thisequipment generates, uses and can radiate radio frequency energy and, if not installed and usedin accordance with the instruction manual, may cause harmful interference to radiocommunications. Operation of this equipment in a residential area is likely to cause harmfulinterference in which case the user will be required to correct the interference at his own expense.Changes or modifications not expressly approved by AJA Video can effect emission complianceand could void the user’s authority to operate this equipment.Contacting SupportTo contact AJA Video for sales or support, use any of the following methods:180 Litton Drive, Grass Valley, CA. 95945 USATelephone: +1.800.251.4224 or +1.530.274.2048Fax: +1.530.274.9442Web: SupportEmail:***************SalesEmail:*************1FS2 Installation and Operation Manual — Limited Warranty Limited WarrantyAJA Video warrants that this product will be free from defects in materials and workmanship for aperiod of five years from the date of purchase. If a product proves to be defective during thiswarranty period, AJA Video, at its option, will either repair the defective product without charge forparts and labor, or will provide a replacement in exchange for the defective product.In order to obtain service under this warranty, you the Customer, must notify AJA Video of the defectbefore the expiration of the warranty period and make suitable arrangements for the performanceof service. The Customer shall be responsible for packaging and shipping the defective product to adesignated service center nominated by AJA Video, with shipping charges prepaid. AJA Video shallpay for the return of the product to the Customer if the shipment is to a location within the countryin which the AJA Video service center is located. Customer shall be responsible for paying allshipping charges, insurance, duties, taxes, and any other charges for products returned to any otherlocations.This warranty shall not apply to any defect, failure or damage caused by improper use or improper orinadequate maintenance and care. AJA Video shall not be obligated to furnish service under thiswarranty a) to repair damage resulting from attempts by personnel other than AJA Videorepresentatives to install, repair or service the product, b) to repair damage resulting from improperuse or connection to incompatible equipment, c) to repair any damage or malfunction caused bythe use of non-AJA Video parts or supplies, or d) to service a product that has been modified orintegrated with other products when the effect of such a modification or integration increases thetime or difficulty of servicing the product.THIS WARRANTY IS GIVEN BY AJA VIDEO IN LIEU OF ANY OTHER WARRANTIES, EXPRESS OR IMPLIED.AJA VIDEO AND ITS VENDORS DISCLAIM ANY IMPLIED WARRANTIES OF MERCHANTABILITY ORFITNESS FOR A PARTICULAR PURPOSE. AJA VIDEO’S RESPONSIBILITY TO REPAIR OR REPLACEDEFECTIVE PRODUCTS IS THE WHOLE AND EXCLUSIVE REMEDY PROVIDED TO THE CUSTOMER FORANY INDIRECT, SPECIAL, INCIDENTAL OR CONSEQUENTIAL DAMAGES IRRESPECTIVE OF WHETHERAJA VIDEO OR THE VENDOR HAS ADVANCE NOTICE OF THE POSSIBILITY OF SUCH DAMAGES. Important Safety InformationHazard!This symbol, when used in the manual, indicates a serious health hazard with risk of injury ordeath.Warning!This symbol, when used in the manual, indicates a serious risk or threat to personal safety.Caution!This symbol, when used in the manual, indicates important safety and complianceinformation.Table of Contents ContentsAJA FS2 Installation and Operation Guide. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .i Trademarks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ii Notice . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . iiFCC Emission Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ii Contacting Support . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ii Limited Warranty. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . iii Important Safety Information. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . iii Contents. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . vChapter 1:Introduction. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 Overview . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 Video Features . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 Available Video Formats. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 Audio Features. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2Control and Other Features. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2Typical Applications. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3FS2 Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 Front Panel Control. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4Remote Web Browser Control. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 SNMP Interface. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4GPI Inputs and Outputs. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 Optional Remote Control Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 Optional Fiber I/O. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 Optional Dolby E Decoder and Encoder Cards. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 Technical Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6 Video Processors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 73G Support. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7Audio Processors. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8 What’s In The Box? . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9In This Manual . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10Chapter 2:Controls, Indicators, and Connections . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .11 Control and Indicator Descriptions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11 Front Panel Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12 Alphanumeric Display. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12 Operational Summary. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12 Pushbuttons. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13 Control Knobs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15 LED Indicators . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16 Incompatibility Alarms . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17 Incompatible Video Formats. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17 Example Reference and Video Incompatibility Alarms . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17 Rear Panel Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18 Connectors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18 Connector Descriptions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19 AC Power Connectors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19 AES/EBU Digital Audio In and Out. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19 Balanced Analog Audio In and Out. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19 RS-422 Port . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19 GPI Inputs and Outputs. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19 LAN. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19 SDI In and Out . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20 Optical Fiber In and Out . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20 Component/Composite Analog Video In and Out . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20 HDMI In and Out . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20 Composite NTSC/PAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20 Reference Video (looping) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20 About Inputs and Outputs. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21Chapter 3:Installation & Configuration . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .23 Installation Overview. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23 Installation Summary. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 24 Unpacking. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 25 Shipping Box Contents. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 25 Installing Optional Fiber Optic I/O Modules . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 26 Installing Optional Cards . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 26 Dolby Decoder Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 27 FS2 Chassis Installation. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 27 Physical Requirements for Mounting the Chassis. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 27 Chassis Dimensions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 27 Cabling and Cooling Requirements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 27 Power Requirements. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 27 Network Connection. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 291FS2 Installation and Operation Manual — ContentsNetwork Address . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 30Networking Using DHCP or Default Static IP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 30Networking the FS2 Using Your Own Static IP. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 30Using Ping to Test the Network Connection. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 32Mac Ping Procedure. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 32Windows PC Ping Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 32Web Browser Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 32Software Update Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 33Download the Latest FS2 Software . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 33Unpack the Software. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 33Uploading and Installing the Software to the FS2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 33System Cabling. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 34System Video/Audio Cable Connections. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 34GPI Connections . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 34FS2 Audio Level Choices—Pro or Consumer, US or EBU . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 35Chapter 4:Display Menus. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .37Controlling the FS2 via Front Panel Display Menus. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 37Parameter Menus. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 38Menu Group Buttons. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 39SELECT and ADJUST Knobs. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 39Menu Operation Examples. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 40Status Pages. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 40Simple Menus: Config Format Alarm Filters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 41Multiple Parameter Menus: Video 1 ProcAmp. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 42Multiple Field Parameters: IP Address. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 43STATUS Menu Group. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 44S.1 I/O Status . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 44S.2 Vid1 Format Status . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 44S.3 Vid1 Format Alarm Status. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 44S.4 Vid2 Format Status . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 45S.5 Vid 2 Format Alarm Status . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 45S.6 Output Status . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 45S.7 Power/Temp Alarm. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 45S.8 Caption Status. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 46S.9 Dolby Status . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 46S.10 System Name . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 46REMOTE Menu Group. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 471 Remote Control. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 471.1 Authentication . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 472.1–4 GPI IN 1–4 Response . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 483.1–4 GPI 1–4 OUT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 49Interaction of Presets and GPIs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 49Example of a Serial Recall. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 49Example of an Unintended Recall. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 49CONFIG Menu Group. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 501 System Name . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 502.1 IP Config . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 502.2 IP Address. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 512.3 Subnet Mask . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 512.4 Default Gateway. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 513 MAC Address (view only) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 524.0 SNMP Enable . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 524.1 SNMP Trap Destination 1. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 524.2 SNMP Trap Port 1. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 534.3 SNMP Trap Destination 2. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 534.4 SNMP Trap Port 2. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 545 Power Supply Alarm. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 546.1 Vid1 Format Alarm. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 546.2 Vid2 Format Alarm. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 557 Reference Alarm. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 558 Hidden Menus . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 559 Display Intensity. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5510 Serial Number. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5611 Software Version. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5612 Reboot . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 56 PRESET Menu Group . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 571 Recall Preset . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 572 Store Preset . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 57Interaction of Presets and GPIs. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 57 SYSTEM Menu Group. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 581 Component In Format. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 582 Component Out Format . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 583 Analog Audio Std . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 584 SDI1 3G Detect. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 595 SDI2 Input Protect. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 596 Fiber1 3G Detect . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 607 Fiber2 Input Protect . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 618 Genlock Source . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 619 Frame Rates. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6110 NTSC Standard. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6211 Composite Downconv. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6212 HDMI RGB Range. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6214.0 AES/EBU SRC Mode. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6314.1–14.8 AES/EBU SRC. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6315 Dolby Decoder Input. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6416 Dolby Decoder Mode. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6417 Dolby Decoder Aux Out . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6518 Dolby Decoder Aux Mode . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 65。
碳纤维复合材料在民用航空上的应用
大型客机，采用复合材料达到 8－9t， 占 该 机 结 构 质 量 的 9% 左 右 。 欧 洲 空 中 客 车 公 司 生 产 的 超 大
料 科 学 与 工 程 系 和 机 械 工 程 系 等 ， 与 有 关 教 授 、 型 客 机 A380-800 可 搭 乘 555 名 旅 客 ， 起 飞 质 量
空中客车法国分公司用于制备中模碳纤维复合材料构件包括水平安定面垂直安定面中翼盒等用高强中模碳纤维处制备包括水平安定面和垂直安定面蒙皮中翼盒等用自动纤维铺层法制备后机身蒙皮制备拉挤桁条垂直安定面加t800s碳纤维im600碳纤维日本东丽toray公司日本东邦toho公司24k24khexplym21碳纤维预浸料美国赫克塞尔hexcel公司m21是第三代增韧树脂hexply8552as4碳纤维预浸料带hexply6376hexply250酚醛预浸料hexply913美国赫克塞尔hexcel公司美国赫克塞尔hexcel公司美国赫克塞尔hexcel公司美国赫克塞尔hexcel公司美国赫克塞尔hexcel公司hexply8552是180固化的高韧树脂用东邦公司hta碳纤维机舱内壁板阻燃自熄hexply913用120低温固化的树脂nc2用新缝纫工艺使碳布定位用作腹部整流装置nc2制备中翼盒中梁等saertexcycom9772增韧环氧树脂cycom997环氧树脂cycom919环氧树脂cycom799h酚醛树脂fm300粘结膜后压力舱壁美国苏泰克cytec公司用树脂膜工艺制备用于制备水平安定面和垂直安定面蒙皮中翼盒等用于制备主承力构美国苏泰克cytec公司高玻璃化转变温度美国苏泰克cytec公司制备后机身蒙皮发动机舱等tg210121低温固化的树脂用作腹部整流装置美国苏泰克cytec公司美国苏泰克cytec公司机舱内壁板阻燃自熄用于复合材料粘结美国苏泰克cytec公司备和成型技术等
杜仲雌雄株叶片的解剖结构比较
杜仲雌雄株叶片的解剖结构比较石匡正;杨晴;郭学民【摘要】为确定杜仲雌雄株叶片的第二性征,采用石蜡切片法观察了杜仲雌雄株叶片解剖结构的差异.结果表明:(1)杜仲雌、雄叶片均由表皮、叶肉和叶脉3部分构成,上下表皮细胞均由一层细胞构成,下表皮具表皮毛;叶肉的栅栏组织和海绵组织分化明显;叶脉维管束均由木质部、少量形成层和韧皮部构成,主脉维管束为外韧型.(2)雌株的叶片厚度、上表皮厚度、栅栏组织厚度以及栅栏组织厚度/海绵组织厚度值大于雄株的,而雄株的下表皮厚度和海绵组织厚度大于雌株的,且雄株主脉维管束更加发达.这些结果证明,杜仲雌雄株在结构上有着明显的差异,这是第二性征的体现,也是杜仲长期进化中为了更好的生存而产生的策略,可能有利于其繁衍生息.【期刊名称】《河北科技师范学院学报》【年(卷),期】2017(031)002【总页数】5页(P24-27,80)【关键词】杜仲;叶片;比较解剖;雌雄异株【作者】石匡正;杨晴;郭学民【作者单位】河北科技师范学院生命科技学院,河北秦皇岛,066600;河北科技师范学院生命科技学院,河北秦皇岛,066600;河北科技师范学院生命科技学院,河北秦皇岛,066600【正文语种】中文【中图分类】Q944.56杜仲(Eucommia ulmoides)又名胶木，是一种极其重要的药用植物，其应用价值已引起各国学者的浓厚兴趣。
已有学者对杜仲叶乙醇提取物的降糖作用机理[1]、杜仲胶在杜仲叶发育过程中含量的变化[2]、杜仲叶片活性成分积累变化规律[3]、杜仲的化学药理及临床应用[4]、生理功能[5]、药理作用[6]、雌雄异株植物对环境胁迫响应的性别差异[7]以及杜仲叶综合利用生产工艺优化[8]进行了大量的研究。
在杜仲雌雄株叶片的研究上，赵云云等[9]发现雌株氨基酸总量高于雄株，王丙武等[10]发现，雌株叶片的含胶量都明显高于雄株叶片，叶东旭等[11]认为，性别对杜仲叶绿原酸含量、京尼平苷含量以及京尼平苷酸含量无明显影响。
1-_公司内部英文缩写(非正式文件,仅限内部参考使_用)
英文缩写 （按首字母排序） 100% Cal 100% IVER 100% PPAP 100% SVER 65% Cal 80% Cal 8D A A MRD A/T A/T AA AAM ABS AC ACE ACT ACT BOM AD ADV ADV AE AE AEM AFI AIAC ALY AMT ANSI AP AP APB APD APE APEC APQP/CP APSB AR ARC ASB ASC ASE ASE ASN ASSI Assy Check-in Assy PPAP Assy PPAP Assy PPV Automotive Safety Engineering Aftersales Engineering Advanced shipping notice Architecture Statement of Strategic Intent Assembly Line Check-in Assembly Line PPAP Assembly Line PPAP Assembly Line Products and Process Validation 100% Calibration 100% Integration Vehicle Engineering Release All parts at full PPAP for Vehicle program 100% Structure Vehicle Engineering Release 65% Calibration 80% Calibration 8 Disciplines Alpha Alpha Material Required Date Automatic Transmission Automatic Transmission Architecture Approval Alliance of Automobile Manufactures Anti-lock Brake System or Anti-Block Steering Architecture Confirmation Assistant Chief Engineer Activity Assembly Component Tree BOM Alternatives Development Analysis / Development / Validation Analysis, Development and Validation Application Engineer Application Engineer Assimilability evaluation method Architecture Framing Initiation Automotive Industry Action Group Alloy Automatic Machincal Transmission American National Standards Institute Advanced Purchasing Assembly Plant Automotive Product Board Approved Product Description Annual Program Execution Asia Pacific Economic Cooperation 英文全称 100%标定 100%集成车工程发布 为了整车项目，所有零件须完全通过PPAP 100%结构车工程发布 65%的动力总成标定 80%的动力总成标定 问题解决8步法 Alpha阶段（动力总成产品开发的一个阶段） Alpha样件需求日期 自动变速器 自动变速器 架构批准 汽车制造商联盟 防抱死制动系统 架构确认 总工助理 工艺路线 总成件树形BOM 主题开发 分析/开发/验证 分析，开发和认证 应用工程师 应用工程师 可装配性评估方法 架构框架启动 美国汽车工业行动集团 铝合金 机械式自动变速器 美国国家标准协会 提前采购 总装厂 汽车产品委员会 批准的产品描述 年度项目执行 中文含义
富林泰克变送器FAA-25 Manual
Type FAA-25 Analogue AmplifierT E C H N I C A L M A N U A LFlintec GmbHBemannsbruch 9DE 74909 MeckesheimGERMANYTable of Contents:1.Features (3)1.1.Technical Specification (3)1.2.Housing Dimensions (4)1.3.Model Identification (4)2.Installation and Commissioning (5)2.1.Mechanical Installation (5)2.2.Electrical Connections (5)2.3.Load Cell Connection (6)2.4.Analogue Output Connection (6)2.5.Optional Digital Inputs / Outputs (6)2.6.Optional RS232C Serial Interface (6)missioning (6)3.Operation (7)4.Setup and Calibration by using the Key Buttons (7)4.1.Setup of the Analogue Output Mode (7)4.2.Setup and Calibration (7)4.2.1.Entering Setup & Calibration (8)4.2.2.Setup & Calibration (8)4.2.3.Exit from Setup & Calibration (8)5.Setup and Calibration via Serial Interface (9)6.Troubleshooting (9)7.Declaration of Conformity (10)PRECAUTIONSDONT LET UNAUTHORIZED PEOPLE INTERFERE WITH THE INSTRUMENT.CHECK THE SUPPLY VOLTAGE, THE LOAD CELL AND ESPECIALLY THE GROUND CONNECTIONS BEFORE ENERGISING FAA-25.DON’T ENERGISE FAA-25 BEFORE MAKING THE LOAD CELL CONNECTION.DON’T CONNECT / DISCONNECT THE CABLES AND/OR CONNECTORS WHILE FAA-25 IS ENERGISED.DO NOT OPEN THE ENCLOSURE WHILE FAA-25 IS CONNECTED TO THE POWER SUPPLY.WARNING !The Error LED can be active before calibration. Do not care the error status before performing the calibration of your weighing system.1. FeaturesThe amplifier type FAA-25 is an accurate and economic load cell transmitter, easy to integrate into process controll systems. By its “digital heart” – modern microcontroller technology – type FAA-25 allows a comfortable calibration and setup with a combination of LED’s and push buttons.The analogue signal output is programmable to 0 – 10 V and 4 – 20 mA.An opto-isolated interface option offers two setpoints, one error output, one input for zeroing by external command and one RS232C serial interface for setup and electronic calibration (PC software eCal-Transmitter).1.1. Technical SpecificationINPUT & A/D CONVERTERLinearity 0.01 % or betterAnalogue input range 0 mV to 20 mVMin. input range < 1 mVA/D Converter 24 bit Delta-Sigma ratiometric with integral analog and digital filtersResolution Min. 0.50 μV/dInternal resolution Min. 8 000 000 countsConversion rate Up to 100 measurements per secondSCALE CALIBRATION & ANALOGUE OUTPUTCalibration Performed with keys. There is no switch or resistor for adjustment in the instrument; alternatively by PC-software (option board required)Digital Filter 2 step adjustable digital adaptive filterWeighing Functions Zeroing via opto-isolated digital input (option board required) D/A Converter 16 bitAnalogue output Current output 4-20 mA (at max. 500 Ω load) or voltage output 0-10 V (at min. 10 kΩ load)Set points 2 programmable free setpoints (option board required)LOAD CELLSExcitation 5 V DCNumber of Load Cells Up to 4 units of 350 Ω or 12 units of 1100 Ω (min. 85 Ω)Connection 4 or 6 wire technique. Cable length 274 m/mm² for 6 wire connectionSETUP & COMMUNICATIONFront panel Membrane keypad including 2x LED and 3x programming keyseCal Electronic calibration without test weights using PC software (option board required) POWERPower supply 230 V AC, 50 Hz , 6 VA OR 24 V DC (18…30 V DC), 200 mA ENVIRONMENT AND ENCLOSUREOperation Temperature Between -10 °C and +40 °C at 85% RH max, non-condensingEnclosure Polyamide, for DIN-rail mount, IP20OPTIONDigital I/O Option 2 opto-isolated outputs for 2 setpoints, 1 opto-isolated error output, 1 opto-isolated input for zeroing and 1 RS232C serial interfaceCharacteristics of thedigital outputsNPN open collector; 18…30 V DC, max. 50 mA1.2. HousingDimensionsBelow you find the coding system to identify the features of your FAA-25 amplifier.2. Installation and CommissioningPRECAUTION: Please read this manuel carefully before energizing the amplifier and perform the commission-ing operation according the procedure given here. Use trained personnel for commissioning, checking and service of the instrument. The interference of untrained personnel may cause unwanted damages or injures. 2.1. M echanical InstallationFirst of all please determine the place where your instrument can operate safely. The place where you willuse/install your instrument should be clean, not getting direct sunlight if possible, with a temperature between -10ºC and +40ºC, 85% maximum relative humidity non-condensing.The cables should be installed safely to avoid mechanical damages.Take care to the housing dimensions given in chapter 1.2. To avoid electrical noise protect your transmitter which has very low input signal level, from the equipment that produces electrical noise.Place your transmitter in a separate panel from the frequency converters and motor contactors, or at least place it in another partition of the panel. Do not combine signal cables and power cables in cable trays. And check that the cables are wired properly in order to prevent mechanical damage.2.2. E lectrical ConnectionsThe pin layout of FAA-25 is shown below. Electrical connections should be done carefully. FAA-25 requires a power supply of 230 V AC (50 Hz, 6 VA, see figure 1) or 24 V DC (200 mA, see figure 2 ) to operate.The meanings of the pins are:Pin DefinitionLOAD CELL CONNECTION- Ex - Excitation- Se - Sense+ Se + Sense+ Ex + Excitation- Si - Signal+ Si + SignalShieldDIGITAL I/O OPTIONErr Erroroutput+ Vc Common +24V DC for outputsO1 Digital output no. 1O2 Digital output no. 2NC NotConnectedCom Zeroing input (0 V)Z Zeroing input (+24 V)TX Transmit (RS232C)RX Receive (RS232C)G Ground (RS232C)ANALOGUE OUTPUTI 0 - 20mA output (+ Signal)G GND (- Signal)V 0 - 10V output (+Signal)ShieldNETZANSCHLUSSN NeutralL 230 V Phase0V 0 V24V 24 V DCNC NotConnectedShieldFigure 1 & 2: FAA-25, front view and pin layoutFigure 1: 230 V AC version Figure 2: 24 V DC versionDo not forget to connect the shield of the load cell cable and the analogue output cable to FAA-25 at the correct ground terminals.The quality of the grounding of your system provides the accuracy of your weighing system beside it’s safety. If the condition of the power line in the plant is bad, prepare a special power line and grounding.If you have to service the instrument, turn off the power and wait at least for 30 seconds before interfering. Perform the other connections to FAA-25 as described below.2.3. L oad Cell ConnectionThe load cell wiring should be made carefully before energizing to avoid damages to the instrument and the load cells. The input resistance of the load cells that you want to connect should be more than 85 Ω. The sense pins of the instrument must absolutely be connected. In 4-wire installations the sense and the excitation pins with the same polarity should be short circuited at the connector side.Pin 6-wire Load Cell Connection 4-wire Load Cell Connection+ Ex + Excitation + Excitation + Se + Sense + Excitation - Se- Sense - Excitation - Ex - Excitation - Excitation + Si + Signal + Signal - Si - Signal - SignalShield Shield2.4. A nalogue Output ConnectionThere are 2 analogue outputs on FAA-25, one is for 0 – 10 volt and the other for 4 – 20 mA. But only one of them can be used at the same time and has to be selected in the setup mode.The wiring of the analogue output should be done according to the pin configuration given in the table below.Pin DefinitionV 0 – 10 V output (+ Signal) I 0 – 20 mA output (+ Signal)G GND (- Signal)Shield2.5. Optional Digital Inputs / OutputsOptionally two setpoint outputs, one error output and one zeroing input can be added to type FAA-25.If an input signal is supplied to the zeroing input, the analogue output signal of FAA-25 will be set to “0 kg”. The setpoints will be active when the weight value is higher than the entered setpoint value.If any failure occurs within FAA-25, an error output will be indicated with the LED on the front panel.If you want to use these I/O, prepare the circuits as shown below.+Vc Zero Error or setpoint Common R load Error Output Status Definition 1 OK0 ErrorFigure 3. Optional digital I/O connection diagram and error output description2.6. Optional RS232C Serial InterfaceThe optional serial interface can be used for eCAL (electronic calibration), adjusting filters, entering setpoint values, exporting status information, etc. The pin configuration is shown in Figure 1 & 2.2.7. CommissioningAfter making the connections of FAA-25 as described above, energize FAA-25 carefully. Then set the instrument to the desired analogue output mode and perform the setup and calibration operations.Check the performance of your system with different test weights. After you have assured the accuracy of the system you can use it.3. OperationThere are 2 LEDs and 3 keys on the front panel of FAA-25. The keys are used for setup and adjustments and the LEDs have different meaning in operation and setup mode. The usage of the keys is described in chapter 4.In operation mode with connected electrical load the green RUN LED is on and the red ERROR LED is off. See chapter 6 in case of the red LED turns on.The status of the LEDs during normal operation is given in the table below.In normal operation0 – 10 V output4 – 20 mA outputGreen RUN LED Flashes (on for 4 seconds)On Red ERROR LEDOffOffFor troubleshooting see chapter 6.The analogue output signal gives information about the status of the system and the weighing process:Condition 0 – 10 V output 4 – 20 mA output Error (option)Operation X XHigh Setup X X Low Weight is higher than the range (Over) 13 V 24 mA Low Weight is lower than the zero range (Under) -1.4 V 0 mA Low System Error 13 V 24 mA Low ADC is out of operating range -1.4 V 0 mA Low4. Setup and Calibration by using the Key ButtonsDuring the power on period the green and red LEDs are lightened for 3 seconds. After both LEDs turned off for a short period, one of them will be lightened. If you did not follow this LED signalization sequence, power off the instrument, check the power and the load cell cables and power it on again.In this step the lightened LED informs you about the active analogue output mode of the instrument. If the green RUN LED is continuously lightened, the analogue output mode is 4 – 20 mA; if it flashes, the analogue output mode is 0 – 10 V (the electrical load should be connected before). If the planned usage is different from the active mode, you have to select the analogue output mode first, see Chapter 4.1. After this the instrument is set up and calibrate as described in Chapter 4.2.Finally check the performance of your system with different test weights. After being sure of the accuracy of the system you can use it.4.1. Setup of the Analogue Output ModeThe selected analogue output mode (voltage or current) is indicated by the RUN LED and the ERROR LED as described in chapter 3.If you want to change the analogue output mode pressand keys simultaneously. If you have changed the analogue output mode, you have to recalibrate the transmitter – regardless if it has already been calibrated for the other output mode.4.2. Setup and CalibrationWarning: The analogue output mode shall be selected as 0 – 10 V or 4 – 20 mA before the calibration. Do not forget to calibrate the instrument after changing the analogue output mode.In this chapter you will find the required information for the setup and the calibration of FAA-25. The symbols at the right bottom of the keys show the function of the keys in setup mode. The meanings of the keys in the setup mode are given in the table below.• Enter / exit the setup mode • Go to the next step • Save• Increase the value • Setup Setpoint no. 1 •Filter type “High”• Decrease the value • Setup Setpoint no. 2 •Filter type “Low”4.2.1. Entering Setup & CalibrationPress and keys simultaneously to enter the “Setup and Calibration” menu. The transmitter indicates the started setup mode by flashing the two LEDs on the front panel three times sequentially. Then the green LED flashes.4.2.2. Setup & CalibrationThe status of the LEDs on the front panel indicates the setup step. You can go to the next step by pressing thekey (in setup mode).Unload the scale. Adjust the analogue output to 0 V or 4 mA by using the arrow keys(decrease).key. If you press the arrow key you will skip this step.for this load by using the arrow keys keys(increase) and(decrease).key. If you press the arrow key you will skip this step.Put a load equal to the desired setpoint value on the scale. Press presskey to assign this value as the second setpoint value (O2).key. If you press the arrow key you will skip this step.If you press the key in this step, the filter type will be set to “High”. Low filtering (higher frequency cut-off; shorter settling time)If you press thekey, the filter type will be set to “Low”. need a faster response in your application set the filter type to “Low”. key. If you press the arrow key you will skip this step.Press the and the and return to the operation mode. Without doing this step the amplifier will loose4.2.3. Exi t from Setup & CalibrationPress the and the keys simultaneously to save the changes, exit from the setup mode and return tothe operation mode.5. Setup and Calibration via Serial InterfaceIf the FAA-25 amplifier includes the optional RS232C serial interface, you can perform eCal (electroniccalibration), normal calibration, adjust the filter, download setpoint values and indicate status information by using the eCal-Transmitter software installed on a PC.The minimum PC requirements are: MS Windows 2000/XP or Vista operating system RS232C serial interface Serial cable for RS232C signals between FAA-25 and PCFor installing the eCal-Transmitter follow the steps described in the Readme.txt file in the eCal setup directory.The main tab of this software is shown at the left.eCal is made very easy:1. Enter the total load cell capacity in [kg], the averaged load cell’s rated output in [mV/V], the scale capacity in [kg] and the estimated deadload value in [kg] into the eCal window.2. Click the button “Write eCal Data to Transmitter”.After performing eCal as described in the software manual, check the performance of your system. After you have assured the accuracy of the system you can use it. You can find essential information for using the eCal-Transmitter software in its help file.6. TroubleshootingThe type FAA25 amplifier has been designed as a very reliable and virtually error free instrument. However if an error occurs do not attempt to repair the equipment before you understand what caused the error. Note the status of the front panel LEDs, and try to find the problem with the help of the table given below. Don’t let unauthorized people interfere with the instrument.In case of an error the ERR LED indicates the analogue output mode like the RUN LED.If the output mode is set to 4 -20 mA, the ERR LED lights continuously in case of an error. If the analogue output mode is set to 0 – 10 V, the ERROR LED flashes.FRONT PANEL LEDSGreen RUN LED Red ERROR LEDERROR OUTPUT(Option)DEFINITIONOn / FlashingOff1• Normal operation Off Off 0• No power• Board failure Off On / Flashing 0• Input signal is out of range • Calibration needed• Check output circuit & cables • Board failureThe analogue output also gives additional information about the weighing system as described in chapter 3.If the calibration was done wrong (e.g. the adjustment of the zero and the span was done with the same load by accident) then following procedure has to be done:1. De-power FAA-25 and re-power it again.2. Switch the analogue output to the other non-active output mode.3. Perform a …rough“ zero and span adjustment according chapter4.2.2 respective chapter5. 4. Switch the analogue output back to the wished output mode.5. Perform a proper adjustment according chapter 4.2.2 respective chapter 5.7.Declaration of ConformityFlintec GmbH Bemannsbruch 9D 74909 MeckesheimKonformitätserklärungDeclaration of conformity Déclaration de conformitéHersteller: Manufacturer. Fabricant: Flintec GmbHTyp/ Modell: Type l Model: Type / modèle:FAA-25entspricht dem in der Bescheinigung über die Bauartzulassung beschriebenen Baumuster sowie den Anforderungen der EG-Richtlinie 90/384/EWG in der jeweils geltenden Fassung und den Anforderungen folgender Richtlinien:corresponds to the production model described in the EC type-approval certificate and to the requirements of the Council Directive 901384lEEC as amended and to the requirements of the following EC directives: correspond au modèle décrit dans le certificat d'approbation CE de type, aux exigences de la directive 90/384/CEE modifiée et aux exigences des directives CE suivantes:89/336/EWG 891336lEE 89/336/CEE 73/23/EWG 73123lEEC 73/23/CEEentsprechend den folgenden Normen: in conformity with the following standards: conforme aux normes suivantes:EN 45501 EN 50081-1 EN 50082-1 EN 60950Diese Erklärung gilt nur in Verbindung mit einer Konformitätsbescheinigung einer benannten Stelle. This declaration is only valid with a certificate of conformity by a notified body.Cette déclaration est valide seulement avec une attestation de conformité d'un organisme notifié.Unterschrift Signature Signature Datum 8. Februar 2007 Date 8th February 2007 Date 8ième février 2007Gerhard K. Adam Geschäftsführer General ManagerDirecteur。
ams4124f标准 -回复
ams4124f标准-回复AMS 4124F Standard: An Overview of its Significance in the Aerospace IndustryIntroduction:AMS 4124F is a widely recognized standard within the aerospace industry. It is a specification that outlines the requirements for aluminum alloy forgings utilized in the manufacturing of aerospace components. This article aims to provide a comprehensive overview of AMS 4124F, its significance, and its impact on the aerospace industry.Background on AMS 4124F:AMS stands for "Aerospace Material Specification," and it is a set of standards established by the Society of Automotive Engineers (SAE)-International. These specifications are developed to ensure consistency, quality, and safety in the aerospace industry. AMS 4124F specifically focuses on the properties and characteristics of aluminum forgings, which are extensively used in the aerospace sector due to their lightweight and high-strength features.Properties and Characteristics of Aluminum Alloy Forgings:Aluminum alloy forgings offer several advantages in aerospace applications. They possess an excellent strength-to-weight ratio, making them suitable for components subjected to high stress and load conditions. These forgings also exhibit exceptional corrosion resistance, which is crucial for aerospace components exposed to harsh environments. Additionally, aluminum forgings provide good formability, allowing for the production of intricate and complex shapes that are often required in aerospace manufacturing.Overview of AMS 4124F Requirements:AMS 4124F specifies the requirements for aluminum alloy forgings in terms of their chemical composition, mechanical properties, heat treatment, and testing procedures. The standard outlines the acceptable limits for elements such as copper, magnesium, zinc, and silicon, which are critical in determining the strength and performance of the forgings. It also defines the required mechanical properties, including tensile strength, yield strength, and elongation, ensuring the forgings meet the demanding structural needs of aerospace components.Heat treatment is another crucial aspect covered by AMS 4124F. It defines the specific temperature ranges and cooling rates thatforgings must undergo to achieve the desired metallurgical properties. This ensures consistent mechanical performance and uniformity in the finished product. Additionally, the standard establishes the testing procedures for dimensional measurements, ultrasonic inspections, and visual inspections to verify the quality and integrity of the forgings.Significance of AMS 4124F in the Aerospace Industry:AMS 4124F plays a significant role in the aerospace industry for multiple reasons. First and foremost, it ensures uniformity in the quality of aluminum alloy forgings used in aerospace components. By adhering to this standard, manufacturers can deliver products that meet the specific requirements and expectations of aircraft manufacturers and regulatory bodies. This standardization promotes safety, reliability, and performance consistency in the aerospace industry.Moreover, AMS 4124F provides a common language and framework for communication between manufacturers, suppliers, and customers. It establishes a clear set of expectations and specifications, streamlining the procurement process and facilitating efficient supply chain management. This reduces thepotential for errors, misunderstandings, and delays, ultimately leading to cost savings and improved productivity.Additionally, compliance with AMS 4124F can enhance customer confidence in the products offered by manufacturers. The aerospace industry's stringent safety regulations necessitate the use of reliable and high-quality materials. By meeting the requirements outlined in AMS 4124F, manufacturers can demonstrate their commitment to delivering trustworthy and durable products, reinforcing their reputation and competitiveness in the aerospace market.Conclusion:AMS 4124F is a crucial standard that ensures the quality, reliability, and performance consistency of aluminum alloy forgings used in the aerospace industry. By adhering to this standard, manufacturers can meet the demanding requirements of aircraft manufacturers and regulatory bodies, promote safety, streamline procurement processes, and enhance customer confidence. As the aerospace industry continues to advance, AMS 4124F will continueto play a critical role in ensuring the reliability and success of aerospace components.。
hongkong code of steel structure -回复
hongkong code of steel structure -回复Hong Kong Code of Steel Structure: Ensuring Safety and Efficiency in Construction ProjectsIntroductionIn Hong Kong, a bustling metropolis known for its iconic skyscrapers and modern infrastructure, the implementation of a comprehensive code for steel structures is essential to ensure the safety and efficiency of construction projects. This code serves as a vital guideline for architects, engineers, and contractors, providing standards and specifications for the design, fabrication, and erection of steel structures. In this article, we will delve into the intricacies of the Hong Kong Code of Steel Structure, exploring its importance, key features, and the process of its implementation.Importance of the Hong Kong Code of Steel StructureSafety is paramount in the construction industry, especially when it comes to tall buildings, bridges, and other structures. The Hong Kong Code of Steel Structure plays a crucial role in achieving this objective by providing guidelines that ensure the structuralintegrity and stability of steel buildings. It considers factors such as load resistance, fire resistance, seismic performance, and durability, among others.Furthermore, the code enhances the efficiency and effectiveness of construction projects. By outlining the specifications and requirements for steel structures, it aids in improving their quality, reducing construction time, and minimizing costs. Adhering to the code facilitates coordination and compatibility between various professionals involved in the project, including architects, engineers, and contractors.Key Features of the Hong Kong Code of Steel Structure1. Structural Design Requirements: The code encompasses various design requirements for steel structures, such as determining the design loads, designing according to limit states, and ensuring appropriate structural configurations.2. Material Specifications: It provides detailed specifications for the selection and use of structural steel, including grade, strength, and quality criteria. This ensures that the steel used in constructionmeets the required standards.3. Fabrication and Erection Guidelines: The code outlines the procedures and guidelines for fabricating and erecting steel structures. It covers aspects such as welding, bolting, connections, and quality control during construction.4. Fire and Seismic Safety: Given Hong Kong's susceptibility to both fires and seismic activities, the code includes specific provisions to enhance the fire and seismic safety of steel structures. This involves determining fire resistance ratings, implementing fire protection measures, and designing structures to withstand seismic forces.Implementation ProcessThe implementation of the Hong Kong Code of Steel Structure involves a step-by-step process, including the following stages:1. Development: The code is developed by a team of experts, including structural engineers, architects, and government representatives. They consider international standards, local regulations, and best practices to ensure the code's relevance andeffectiveness in the Hong Kong context.2. Consultation and Review: The draft code is then subject to extensive consultation and review processes. Stakeholders, including industry professionals, academic institutions, and relevant government bodies, provide feedback and suggestions to refine and enhance the code.3. Approval and Publication: Following the necessary revisions, the code is finally approved by the relevant regulatory authority, such as the Buildings Department in Hong Kong. It is then published and made available to the public.4. Training and Education: To ensure effective implementation, training programs and educational initiatives are conducted to familiarize professionals with the code and its requirements. These programs enhance their capacity to apply the code accurately and efficiently in their respective roles.5. Compliance and Enforcement: Compliance with the code is monitored and enforced through building inspections, certification requirements, and ongoing surveillance. Non-compliance mayresult in penalties and, if necessary, rectification measures to ensure the safety and quality of steel structures.ConclusionThe Hong Kong Code of Steel Structure is an indispensable tool for the construction industry, supporting the safe and efficient erection of steel structures across the city. Its importance lies in enhancing safety, promoting quality, and streamlining construction processes. With its comprehensive guidelines, the code ensures that steel structures in Hong Kong adhere to the highest standards of structural integrity, enabling the city's skyline to continue to thrive and grow.。
HS22 轻型螺纹编码器说明书
MODEL HS22® | INCREMENTAL OPTICAL ENCODERIntroductionThe HS22 series of hollow shaft incremental encoder offers application advantages over conventional optical encoders. This heavy duty unit is designedfor ease of installation to a servo motor, the encoder’s flexible coupling fits over the driven motor shaft to provide an accurate, backlash-free method of attachment.The mounting method eliminates the need for couplings, sprockets, or gearing. The integral flex mount provides for a 20-degree angular adjustment. Through-shaft or blind shaft configurations of the HS22 encoder are available.Through-shaft units allow for applications where the center of the encoder must be used for transmission of fluids, cabling, or optics. Blind shaft units are designed to mate with shaft lengths of 0.50 to 1.50 inch. Standard outputs for both configurations include: A and B in quadrature with indexand optional commutation signals for brushless motor control.SPECIFICATIONSMechanicalEnvironmentalNotes and Tables:All notes and tables referred to in the text can be found in the pages that follow.ElectricalTable 1 —Output Terminations Pinouts1. Mounting is usually done either using the D-style square flange mount, E- or G-style servo mounts, or one of the standard face mounts, F1 for example. Consult factory for additional face mount options.2. The shaft seal is recommended in virtually all installations. The most common exceptions are applications requiring a very low starting torque or those requiring operation at both high temperature and high speed.3. Non-standard index widths and multiple indices are available by special order. Consult factory.4. Complementary outputs are recommended for use with line driver type (source/sink) outputs. When used with differential receivers, this combination provides a high degree of noise immunity5.Output IC’s: Output IC’s are available as either Line Driver (LD) or NPN Open Collector (OC) types. Open Collectors require pull-up resistors, resulting in higher output source impedance (sink impedance is similar to that of line drivers). In general, use of a Line Driver style output is recommended. Line Drivers source or sink current and their lower impedance mean better noise immunity and faster switching times. Warning: Do not connect any line driver outputs directly to circuit common/OV, which may damage the driver. Unused outputs should be isolated and left floating. Our applications specialists would be pleased to discuss your system requirements and the compatibility of your receiving electronics with Line Driver type outputs. 28V/V: Multi-voltage Line Driver (7272*): 100 mA source/sink. Input voltage 5 to 28 VDC +/- 5% standard (Note: V out = V in). This driver is TTL compatible when used with 5 volt supply. Supply lines are protected against overvoltage to 60 volts and reverse voltage. Outputs are short circuit protected for one minute. Supply current is 120 mA typical (plus load current). This is the recommended replacement for 3904R and 7406R open collector outputs with internal pullup resistors. It is also a direct replacement for any 4469, 88C30, 8830 or 26LS31 line driver. 28V/5: Multi-voltage Line Driver (7272*): 100 mA source/sink. Input voltage 5 to 28 VDC +/- 5% standard, internally regulated with 5V (TTL compatible) logic out. Supply lines are protected against overvoltage to 60 volts and reverse voltage. Outputs are short circuit protected for one minute. Supply current is 90 mA typical (plus load current). 15V/V: Multi-voltage Line Driver (4469*): 100 mA source/sink. Input voltage 5 to 15 VDC +/- 5% standard (Note: V out = V in). TTL compatible when used with 5 volt supply. Supply lines are protected against overvoltage to 60 volts and reverse voltage. Outputs are short circuit protected for one minute. Supply current is 90 mA typical (plus load current). This is a direct replacement for the 4469 Line Driver. 28V/OC: NPN Open Collector (3904*, 7273*). Current sink of 80 mA max. Current sourced by external pull- up resistor. Output can be pulled up to voltage other than supply voltage (30 V max). Input voltage 5 to 28 VDC +/- 5% standard. Supply current is 120 mA typical. This replaces prior IC’s with designations of 3904, 7406, 3302, 681 and 689. 5V/OCR, 15V/OCR, 24V/OCR: Open Collector (3904R*, 7406R*, 7273R*): Current sink of 70 mA max. Includes internal pull-ups sized at approximately 100 ohms/volt. Max current source is 10 mA. Supply current is 100 mA typical, 120 mA with internal pull-ups. The 5V/OCR, 15V/OCR and 24V/OCR are often replaced by the 28V/V in system upgrades. 3904, 3904R, 4469, 5V/V, 5V/OC, 5V/OCR, 9V/OC: Intrinsically safe line driver and open collector outputs. These drivers are specific to intrinsically safe encoders, and are installed per the appropriate control drawings listed in Table 2.1 on page 48 of the 2008 BEI Spec Guide.6. Special –S at the end of the model number is used to define a variety of non-standard features such as special shaft lengths, voltage options, or special testing. Please consult the factory to discuss your special requirements.7. Higher frequency response may be available. Please consult with the factory.8. Extended temperature ratings are available in the following ranges: -40 to 70°C, -40 to 85°C, –20 to 105°C and –40 to 105°C depending on the particular model. Some models can operate down to -55°C. Extended temperature ranges can affect other performance factors. Consult with factory for more specific information.9. Mating straight plug receptacles may be ordered from the factory:For M12 use MS3116F12-10S, For M14 use MS3106F14S-6SFor M14/19 use MS3116J14-19S, For M16 use MS3106F16S-1SFor M18 use MS3106F18-1S, For M20 use MS3106F20-29SPage 6CONTACT USAmericas+1 (800) 350 2727 – Option 1****************************Europe, Middle East & Africa +33 (3) 88 20 8080****************************Asia Pacific*************************.com China +86 (21) 2306 1500Japan +81 (45) 277 7117Korea +82 (31) 601 2004India +91 (80) 67920890Rest of Asia +886 (2) 27602006 ext 2808Sensata Technologies, Inc. (“Sensata”) data sheets are solely intended to assist designers (“Buyers”) who are developing systems that incorporate Sensata products (also referred to herein as “components”). Buyer understands and agrees that Buyer remains responsible for using its independent analysis, evaluation and judgment in designing Buyer’s systems and products. Sensata data sheets have been created using standard laboratory conditions and engineering practices. Sensata has not conducted any testing other than that specifically described in the published documentation for a particular data sheet. Sensata may make corrections, enhancements, improvements and other changes to its data sheets or components without notice.Buyers are authorized to use Sensata data sheets with the Sensata component(s) identified in each particular data sheet. HOWEVER, NO OTHER LICENSE, EXPRESS OR IMPLIED, BY ESTOPPEL OR OTHERWISE TO ANY OTHER SENSATA INTELLECTUAL PROPERTY RIGHT, AND NO LICENSE TO ANY THIRD PARTY TECHNOLOGY OR INTELLECTUAL PROPERTY RIGHT, IS GRANTED HEREIN. SENSATA DATA SHEETS ARE PROVIDED “AS IS”. SENSATA MAKES NO WARRANTIES OR REPRESENTATIONS WITH REGARD TO THE DATA SHEETS OR USE OF THE DATA SHEETS, EXPRESS, IMPLIED OR STATUTORY, INCLUDING ACCURACY OR COMPLETENESS. SENSATA DISCLAIMS ANY WARRANTY OF TITLE AND ANY IMPLIED WARRANTIES OF MERCHANTABILITY, FITNESS FOR A PARTICULAR PURPOSE, QUIET ENJOYMENT, QUIET POSSESSION, AND NON-INFRINGEMENT OF ANY THIRD PARTY INTELLECTUAL PROPERTY RIGHTS WITH REGARD TO SENSATA DATA SHEETS OR USE THEREOF.All products are sold subject to Sensata’s terms and conditions of sale supplied at SENSATA ASSUMES NO LIABILITY FOR APPLICATIONS ASSISTANCE OR THE DESIGN OF BUYERS’ PRODUCTS. BUYER ACKNOWLEDGES AND AGREES THAT IT IS SOLELY RESPONSIBLE FOR COMPLIANCE WITH ALL LEGAL, REGULATORY AND SAFETY-RELATED REQUIREMENTS CONCERNING ITS PRODUCTS, AND ANY USE OF SENSATA COMPONENTS IN ITS APPLICATIONS, NOTWITHSTANDING ANY APPLICATIONS-RELATED INFORMATION ORDERING OPTIONSBlank: None S: Special。
ENG FAILURE AFTER TAKEOFF No Damage
PERF
THE END...
SYNTHESIS
•Engine Failure
• Gear UP • Observe Pitch & Target
• EO ACCEL ALT
• Push to level off
• At GREEN DOT
• Pull ALT knob • Set THR LVR to MCT • Continue ECAM
priority. Performing ECAM action before stabilization
ECAM ACTIOundNerSmines actions efficiency due to PF low availability
PF
ECAM PROCEDURE DAMAGE ?
COMMUNICATE
ENG FAILURE AFTER TAKEOFF (No Damage)
At EO ACCEL ALT
ECAM ACTIONS
STOP ECAM
At Green Dot
CONTINUE ECAM
(ENG RELIGHT)
PUSH to…
PITCH : 12,5° L/G up
LEVEL OFF
-F Flaps 1
ß TARGET
Once centered : Appropriate sideslip for
optimum climb PERF
In this exercise, the Autopilot will center the ß TARGET.
PF
ENG FAIL
PNF
DETECTION
FLY THE AIRCRAFT Beta Target NAVIGATE LAND ASAP COMMUNICATE CONSIDER AUTOMATION USE
海夫主轴科技（上海）有限公司介绍企业发展分析报告
Enterprise Development专业品质权威Analysis Report企业发展分析报告海夫主轴科技（上海）有限公司免责声明:本报告通过对该企业公开数据进行分析生成，并不完全代表我方对该企业的意见，如有错误请及时联系;本报告出于对企业发展研究目的产生，仅供参考，在任何情况下，使用本报告所引起的一切后果，我方不承担任何责任:本报告不得用于一切商业用途，如需引用或合作，请与我方联系:海夫主轴科技（上海）有限公司1企业发展分析结果1.1 企业发展指数得分企业发展指数得分海夫主轴科技（上海）有限公司综合得分说明：企业发展指数根据企业规模、企业创新、企业风险、企业活力四个维度对企业发展情况进行评价。
该企业的综合评价得分需要您得到该公司授权后，我们将协助您分析给出。
1.2 企业画像类别内容行业专业技术服务业-工业与专业设计及其他专业技术服务资质空产品服务物进出口。
（依法须经批准的项目，经相关部1.3 发展历程2工商2.1工商信息2.2工商变更2.3股东结构2.4主要人员2.5分支机构2.6对外投资2.7企业年报2.8股权出质2.9动产抵押2.10司法协助2.11清算2.12注销3投融资3.1融资历史3.2投资事件3.3核心团队3.4企业业务4企业信用4.1企业信用4.2行政许可-工商局4.3行政处罚-信用中国4.4行政处罚-工商局4.5税务评级4.6税务处罚4.7经营异常4.8经营异常-工商局4.9采购不良行为4.10产品抽查4.11产品抽查-工商局4.12欠税公告4.13环保处罚4.14被执行人5司法文书5.1法律诉讼（当事人）5.2法律诉讼（相关人）5.3开庭公告5.4被执行人5.5法院公告5.6破产暂无破产数据6企业资质6.1资质许可6.2人员资质6.3产品许可6.4特殊许可7知识产权7.1商标信息最多显示100条记录，如需更多信息请到企业大数据平台查询7.2专利7.3软件著作权7.4作品著作权7.5网站备案7.6应用APP7.7微信公众号8招标中标8.1政府招标8.2政府中标8.3央企招标8.4央企中标9标准9.1国家标准9.2行业标准9.3团体标准9.4地方标准10成果奖励10.1国家奖励10.2省部奖励10.3社会奖励10.4科技成果11 土地11.1大块土地出让11.2出让公告11.3土地抵押11.4地块公示11.5大企业购地11.6土地出租11.7土地结果11.8土地转让12基金12.1国家自然基金12.2国家自然基金成果12.3国家社科基金13招聘13.1招聘信息感谢阅读:感谢您耐心地阅读这份企业调查分析报告。
java康纳塔参数
java康纳塔参数
- EPS内模成型工艺：该工艺是康纳塔最大的亮点。
它通过内模和外模双模系统完成，完全淘汰了传统的通过无法保证强度和控制韧性比反复叠加碳布的解决方案。
这种工艺改进从根本上提高了车架的质量，使内壁更加光滑细腻，同时兼具更好的韧性和强度。
-AIR空气动力学系统：有效集中在3个点，创造出一个智能化的几何框架，最小化空气阻力，框架结构同时也在为精密科技代言。
-价格：标配版为7998元。
如果你想了解更多java康纳塔的参数信息，可以补充细节继续向我提问。
高级塔板和舱身注释说明书
Advanced Towers and VesselsAnnotated Instructor’s GuideMODULE OVERVIEWThis module covers the function and operation of vessels and towers, especially those used in refineries. Information is provided about safety issues associated with the refinery process. The use of hydraulic torquing and tensioning equipment is also covered.PREREQUISITESPrior to training with this module, it is recommended that the trainee shall have successfully completed Core Curriculum; Industrial Maintenance Mechanic Level One; Industrial Maintenance Mechanic Level Two; Industrial Maintenance Mechanic Level Three; and Industrial Maintenance Mechanic Level Four.OBJECTIVESUpon completion of this module, the trainee will be able to do the following:1.Describe basic reactor mechanics and functions, including vacuum distillation towers and strippertowers.2.Demonstrate hydraulic torquing and tensioning.PERFORMANCE TASKUnder the supervision of the instructor, the trainee should be able to do the following:ing equipment provided by your instructor, demonstrate hydraulic torquing and tensioning.MATERIALS AND EQUIPMENT LISTOverhead projector and screen TransparenciesBlank acetate sheetsTransparency pensWhiteboard/chalkboardMarkers/chalkPencils and scratch paperAppropriate personal protective equipment Pictures of various types of towers and vessels Pictures of refinery fires or explosions Hydraulic torquing and tensioning equipment Examples of manual ratcheting wrenches Appropriate nuts, bolts, and tensioning discs Hydraulic hose connectorsCopies of the Quick Quizzes*Module Examinations**Performance Profile Sheets***Located at the back of this module.**Located in the Test Booklet.SAFETY CONSIDERATIONSEnsure that the trainees are equipped with appropriate personal protective equipment and know how to use it properly. Trainees will be required to perform hydraulic torquing and tensioning. Ensure that they are properly briefed on the safe use of hydraulic torquing and tensioning tools and are familiar with all appropriate safety precautions and procedures.ADDITIONAL RESOURCESThis module is intended to present thorough resources for task training. The following reference works are suggested for both instructors and motivated trainees interested in further study. These are optional materials for continued education rather than for task training.OSHA Technical Manual, Section IV, Chapter 2,Petroleum Refining Processes. Available at:/dts/osta/otm/otm_iv/otm_iv_2.html.American Petroleum Institute at: .TEACHING TIME FOR THIS MODULEAn outline for use in developing your lesson plan is presented below. Note that each Roman numeral in the outline equates to one session of instruction. Each session has a suggested time period of 21⁄2hours. This includes 10 minutes at the beginning of each session for administrative tasks and one 10-minute break during the session. Approximately 15 hours are suggested to cover Advanced Towers and Vessels. You will need to adjust the time required for hands-on activity and testing based on your class size and resources. Because laboratories often correspond to Performance Tasks, the proficiency of the trainees may be noted during these exercises for Performance Testing purposes.Topic Planned Time Sessions I-II.Introduction; Separation ProcessesA.Introduction____________B.Separation Processes ____________1.Desalting____________2.Atmospheric Distillation____________3.Vacuum Distillation____________4.Distillation Tower Hazards____________ Sessions III-IV.Conversion and Other Refining ProcessesA.Conversion Processes ____________1.Solvent Extraction and Dewaxing____________2.Cracking Processes and Hazards____________B.Treatment, Formulating, and Blending Processes ____________C.Other Refining Processes ____________1.Heating and Cooling____________2.Steam____________3.Recovery____________4.Discharge Management____________ Session V.Hydraulic Torquing and TensioningA. Torquing and Tensioning Basics____________B.Torquing Devices____________boratory____________Have trainees practice hydraulic torquing. This laboratory corresponds toPerformance Task 1.C.Tensioning Devices____________boratory____________Have trainees practice hydraulic tensioning. This laboratory corresponds toPerformance Task 1.D.Torquing and Tensioning Hazards; Tool Maintenance____________Session VI.Review and TestingA.Trade Terms Quick Quiz____________B.Module Review ____________C.Module Examination____________1.Trainees must score 70% or higher to receive recognition from NCCER.2.Record the testing results on Craft Training Report Form 200, andsubmit the results to the Training Program Sponsor.D.Performance Testing____________1.Trainees must perform each task to the satisfaction of the instructorto receive recognition from NCCER. If applicable, proficiency noted duringlaboratory exercises can be used to satisfy the Performance Testingrequirements.2.Record the testing results on Craft Training Report Form 200, and submitthe results to the Training Program Sponsor.Troubleshooting and Repairing ConveyorsAnnotated Instructor’s GuideMODULE OVERVIEWThis module explains how to maintain, troubleshoot, and repair conveyors, including how to splice belts and replace sprockets, bearings, and conveying devices.PREREQUISITESPrior to training with this module, it is recommended that the trainee shall have successfully completed Core Curriculum; Industrial Maintenance Mechanic Level One; Industrial Maintenance Mechanic Level Two; Industrial Maintenance Mechanic Level T hree; Industrial Maintenance Mechanic Level Four, and Industrial Maintenance Mechanic Level Five, Module 32501-09.OBJECTIVESUpon completion of this module, the trainee will be able to do the following:1.Maintain, troubleshoot, and repair belt and roller conveyors.2.Maintain, troubleshoot, and repair chain conveyors.3.Maintain, troubleshoot, and repair screw conveyors.4.Maintain, troubleshoot, and repair pneumatic conveyors.PERFORMANCE TASKSUnder the supervision of the instructor, the trainee should be able to do the following:1.Simulate splicing a belt.2.Repair one of the following:•Belt conveyor•Chain conveyor•Screw conveyor•Pneumatic conveyorMATERIALS AND EQUIPMENT LISTOverhead projector and screen TransparenciesBlank acetate sheetsTransparency pensWhiteboard/chalkboardMarkers/chalkPencils and scratch paperAppropriate personal protective equipment GlovesStraightedgeTape measuresPlywood or other suitable surface on which to cut and repair beltsMechanical belt fasteners or other splicing materials Conveyor setups or broken or damaged conveyors for the repair of belt, chain, screw, or pneumatic conveyorsDamaged drive rollers, sprockets, and bearings Damaged chains, sprockets, and carrying devices Maintenance manuals for belt, chain, screw, and pneumatic conveyorsReplacement links for chain conveyors Replacement belt materialsSling and hardware for riggingTools for marking, measuring, cutting, and splicing conveyor beltsTools for installing replacement linksAllen wrenchesArbor press or length of pipe to install bearingscontinued*Located at the back of this module**Located in the Test Booklet SAFETY CONSIDERATIONSEnsure that the trainees are equipped with appropriate personal protective equipment and know how to use it properly. This module requires trainees to repair conveyors. Ensure that all trainees are briefed on appropriate shop safety procedures. This module may require that the trainees visit job sites. Ensure that trainees are briefed on site safety policies prior to any site visits.ADDITIONAL RESOURCESThis module is intended to present thorough resources for task training. The following reference works are suggested for both instructors and motivated trainees interested in further study. These are optional ma-terials for continued education rather than for task training.Rexnord Power Transmission and Conveying Components, Catalog #R85, 1984. Atlanta, GA: Rexnord Inc. Goodyear Belt Splicing Manual.Akron, OH: Goodyear Tire and Rubber Co.TEACHING TIME FOR THIS MODULEAn outline for use in developing your lesson plan is presented below. Note that each Roman numeral in the outline equates to one session of instruction. Each session has a suggested time period of 21⁄2hours.This includes 10 minutes at the beginning of each session for administrative tasks and one 10-minute break during the session. Approximately 121⁄2hours are suggested to cover Troubleshooting and Repairing Conveyors . You will need to adjust the time required for hands-on activity and testing based on your class size and resources. Because laboratories often correspond to Performance Tasks, the proficiency of the trainees may be noted during these exercises for Performance Testing purposes.Topic Planned Time Sessions I-II.Introduction; Maintaining, Troubleshooting, and Repairing Belt and Roller ConveyorsA.Introduction ____________B.Maintaining and Repairing Belt and Roller Conveyors ____________boratory ____________Have trainees simulate splicing a belt. This laboratory corresponds to Performance Task 1.boratory ____________Have trainees practice repairing a belt conveyor. This laboratory corresponds to Performance Task 2.Assorted screwdriversBearing pullersGrease gun and lubricantNeedle-nose pliersTorque wrenches Copies of the Quick Quizzes*Module Examinations**Performance Profile Sheets**Sessions III-IV.Maintaining, Troubleshooting, and Repairing Chain, Screw,and Pneumatic ConveyorsA.Chain Conveyors ____________boratory____________Have trainees practice repairing a chain conveyor. This laboratorycorresponds to Performance Task 2.C.Screw Conveyors ____________boratory____________Have trainees practice repairing a screw conveyor. This laboratory correspondsto Performance Task 2.E.Pneumatic Conveyors ____________boratory____________Have trainees practice repairing a pneumatic conveyor. This laboratorycorresponds to Performance Task 2.Session V. Review and TestingA.Module Review ____________B.Module Examination____________1.Trainees must score 70% or higher to receive recognition from NCCER.2.Record the testing results on Craft Training Report Form 200, and submitthe results to the Training Program Sponsor.C.Performance Testing____________1.Trainees must perform each task to the satisfaction of the instructor to receiverecognition from NCCER. If applicable, proficiency noted during laboratoryexercises can be used to satisfy the Performance Testing requirements.2.Record the testing results on Craft Training Report Form 200, and submit theresults to the Training Program Sponsor.。
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FAA ACADEMY September 2008
Federal Aviation Administration
3
Federal Aviation Administration
Our Mission
To provide the safest, most efficient aerospace system in the world
William J. Hughes Technical Center
Research and testing
FAA ACADEMY September 2008
Federal Aviation Administration
9
Regional Offices
FAA ACADEMY September 2008
FAA ACADEMY September 2008
Federal Aviation Administration
5
Federal Aviation Administration
• Organization
FAA Administrator
Appointed by the President with advice and consent of the Senate Serves a 5 year term Assisted by the Deputy Administrator
FAA Headquarters establishes policy and oversees the nation’s civil aviation system through nine regional offices Each region is responsible for providing oversight and guidance to the facilities and offices within their geographical area In addition to the nine regions the FAA’s mission is supported by two major centers:
Two additional support offices include:
Office of Safety Office of Acquisition and Business Services
FAA ACADEMY September 2008 Federal Aviation Administration
FAA Academy International Training
Federal Aviation Administration
Executive Management Development Training
FAA Structure and Management
Beijing, China, 1–5 September 2008
FAA ACADEMY September 2008
Federal Aviation Administration
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FAA Responsibilities
• The FAA is responsible for the safety of civil aviation • Major roles include: • Regulating civil aviation to promote safety • Encouraging and developing civil aeronautics, including new aviation technology • Developing and operating a system of air traffic control and navigation for both civil and military aircraft • Researching and developing the National Airspace System and civil aeronautics • Developing and carrying out programs to control aircraft noise and other environmental effects of civil aviation • Regulating U.S. commercial space transportation
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Federal Aviation Administration
• Organization
The Chief Counsel and nine Assistant Administrators also report to the Administrator. The Assistant Administrators oversee key programs
Human Resources Aviation Policy, Planning and Environment International Aviation Civil Rights Regions and Center Operations Communications Information Technology Security and Hazardous Materials Government and Industry Affairs
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Federal Aviation Administration
11
Federal Aviation Administration
• Air Traffic Organization
The ATO was established in 2003 as a performance-based organization by Executive Order of the President To provide safe, secure and cost effective air traffic management services while being responsive to customers and accountable to the public 35,000 controllers, technicians, engineers and support personnel
Airports Aviation Safety Commercial Space and Transportation Air Traffic Organization Financial Services
FAA ACADEMY September 2008 Federal Aviation Administration
Federal Aviation Administration
10
Federal Aviation Administration
• Relationship between FAA and Regional Offices
Civil aviation policy for the United States is the responsibility of FAA Headquarters Policy is implemented through the nine regional offices by each facility and individual in the FAA Complying with chain of command promotes standardization and consistency throughout the FAA Business Plan process ensures all activities are aligned with national goals and objectives
FAA ACADEMY September 2008
Federal Aviation Adme
• FAA Responsibilities • FAA Mission • Organizational Structure • Regional Offices • Relationship between Regional Office and FAA Headquarters • Air Traffic Organization
Mike Monroney Aeronautical Center
Managerial and Technical Training National Airspace System Logistical Support Information Technology Financial Services
Our Vision
To improve the safety and efficiency of aviation, while being responsive to our customers and accountable to the public.
FAA ACADEMY September 2008
Operations
En Route and Oceanic System Operations Technical Operations Terminal Technical Training Service Centers
Next Generation Air Transportation System (NextGen) and Operations Planning Strategy and Performance Finance
Federal Aviation Administration
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Federal Aviation Administration