饥饿游戏vs 斯巴鲁合作方案
长安福特GFX无尽之旅方案
13
AR增强现实游戏
鼎新恒在为长安福特研制专属的APP软件,使客户充分体验前沿科技带来的乐趣,使长 安福特品牌更深入人心。
体验方式一:福特大搜索 工作人员会事先为来宾手机安装 GFX专属APP,在私房路线环节 中,寻找并扫描事先由工作人员 布置好的福特LOGO,通过AR增 强现实技术,与虚拟的世界进行 互动,拍摄虚拟的翼虎与自己或 随行伙伴的合影,待晚会的时候 由来宾评比选出最佳照片(最文 艺,最创意,最搞笑等),并发 放奖品。
设计研发“中国汉字听写大会” 电视节目形态
名人聚集地 早期:冰心,曹禺;中期:刘震云,贾 平凹;当代:郭敬明,安妮宝贝 中国唯一诺贝尔文学奖获得者:莫言
最庞大的精英作家聚集地,有 近万名优质会员
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长安福特纪念图书馆
一块尚未被发掘的中国文化瑰宝处女地 充满社会责任感的汽车企业
“长安福特纪念图书馆” 传播中国文化,向社会注入“正能量”
23
我们怎么做
1. 公益方面,与“中国作协”近万名作家 形成直接关系,为GFX印刷出版专属图书,
公益方式不仅仅局限于小学捐赠,也可以 是当地社区或支柱企业等
根本上解决图书版权问题,GFX的公益不再是 单纯的扶贫,更是一种文化的传播。
2. 邀请“中国作协”中的知名作家参与 GFX活动
知名作家现场与参与者进行文化的沟通交流,
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27
城市排期
28
媒体场 消费者场
城市排期
日期 4月 5月 6月 7月 8月 9月 10月 11月 12月
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消费者场 金华,常州 温州,芜湖 南昌,赣州 烟台,潍坊
保定 长春 银川,兰州 东莞,佛山 贵阳,重庆
媒体场 二连浩特
西安 包头 沈阳 额济纳旗 湛江
GBA荣誉勋章 渗透者100%完成度详细图文攻略
GBA-<荣誉勋章渗透者>100%完成度详细图文攻略* w* J$ ]5 ?- l& D, M S- u+\+ t: K, ~====================================================== GBA编号1276(英),名称《荣誉勋章渗透者》(Medal of Honor:Infiltrator)7 `( h7 D0 B/ Z3 U$ ?发售日:2003年11月17日標準価格:4,800円(税別)対応人数:1~2人类别:ACT+ L( X, Y6 e9 T1 ]& {* v) p(c)2003 EA Games2 b J: [4 Z. d7 G9 `- p! F====================================================== ~* j, w8 ^4 u7 s5 {. E7 W) X- c8 T5 z* `& Y9 c3 t9 \: \" W& n. n# V5 p1 q' L==========目录==========# A6 J; v7 B* O' U4 W& O& t----------------------- " P! k$ i: F' m4 R1 【菜单目录解说】0 Z4 |* {, ?3 v1 e: y----------------------- # ]! b/ W1 L0 c9 `2 【系统操作介绍】----------------------- ; U& X% H9 ] {; U' a3 【详细图文攻略】------------------------ z9 ~: _. Y; ]0 Q" b$ u9 G( p* ~1 K: O6 H% M: ?1 V; Y9 s$ x' ?; z〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒菜单目录解说〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒8 h5 ]. j6 y* H5 N, u9 J# g x) L5 N' mCampaign) l& q2 G7 r. F战役模式, ?8 e) x2 ]2 m- j5 Y8 H( C4 Y3 c, \7 q: L6 n: fMuti-Player多人模式(联机通讯)5 N8 Y7 h+ f! @5 t$ R3 A2 W" LOption附加选项(音效等)Extra追加内容6 ]$ G+ J: @0 m& |+ I$ w% B-Survival Mode 生存模式(通关战役模式一次后出现)( r4 F$ Z- i# C) p6 E2 }* j-Max-GI Mode 使用速度更快的高级士兵作战(通关战役模式一次后出现)0 K: g. p. L" G9 c1 N' I, _) a9 BQuick Start, D. l/ c I$ V跳过初始CG快速开始游戏+ E9 s) e8 m1 ]5 k5 {# y0 r; o. E }. c+ n) y; P5 b7 A/ f# K, {3 G7 k4 U* o- I$ D! j) }$ `% u$ r X7 n$ ?0 ^! ~4 _- v" h9 t* r+ D9 ia4 H+ |' t$ A3 t g6 o〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒系统操作介绍4 H7 X1 a) w6 u" Z1 x: [( C! x〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒U( C0 P/ ?% |A键---------射击/更换弹匣/投弹/安放B键---------主武器和副武器之间的替换L键---------使用机关枪/搭乘坦克R键---------瞄准START键-Resume 继续游戏-Quit to Title 退回至标题界面* F# F; e( t8 ~: Z" b-Restart Level 重新开始此关3 k7 A& ^% W. w# U-Objective 任务要求/ c9 c$ M8 O& J" N; ]$ o2 g* g- g& C) p" o$ P1 b〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒详细图文流程攻略6 W& |8 p6 A4 c. m! ^* Q〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒〒& h% ]/ S4 [; b. C; ?7 Z! H1 p( ^================================: y+ X7 {4 `9 k* a( QMission 01Tiger at the Gate& N& m( e& e& ?2 Q/ a/ A================================/ e- ~9 T4 I: v' Z& n; C. \9 j-------------------------/ s; n/ W h7 Z/ d* Y: eLevel 1The Beachhead# K. e7 r7 l; W( W! w-------------------------& x p/ K+ e9 p. z5 z原作者Kayin 原出处新慧福任天堂世界一开始先躲过两阵的飞机轰炸。
ISC用户手册
4 管理用户操作..................................................................................................................................... 4-1 4.1 预置位操作 ........................................................................................................................................ 4-3 4.1.1 设置新预置位 .......................................................................................................................... 4-3 4.1.2 调用预置位.............................................................................................................................. 4-4 4.1.3 删除预置位.............................................................................................................................. 4-4 4.2 设置网口参数..................................................................................................................................... 4-4 4.3 设置编码套餐..................................................................................................................................... 4-4
CGA G-4-2008
CGA G-4—2008OXYGENTENTH EDITIONCOMPRESSED GAS ASSOCIATION, INC.4221 Walney Road, 5th FloorChantilly, VA 20151Phone: 703-788-2700Fax: 703-961-1831E-mail: cga@P AGE ii C OMPRESSED G AS A SSOCIATION,I NC. CGA G-4—2008PLEASE NOTE:The information contained in this document was obtained from sources believed to be reliable and is based on technical information and experience currently available from members of the Compressed Gas Association, Inc. and others. However, the Association or its members, jointly or severally, make no guarantee of the results and assume no liability or responsibility in connection with the information or suggestions herein contained. Moreover, it should not be assumed that every acceptable commodity grade, test or safety procedure or method, precaution, equipment or device is contained within, or that abnormal or unusual circumstances may not warrant or suggest further requirements or additional procedure.This document is subject to periodic review, and users are cautioned to obtain the latest edition. The Associa-tion invites comments and suggestions for consideration. In connection with such review, any such comments or suggestions will be fully reviewed by the Association after giving the party, upon request, a reasonable op-portunity to be heard. Proposed changes may be submitted via the Internet at our web site, . This document should not be confused with federal, state, provincial, or municipal specifications or regulations; insurance requirements; or national safety codes. While the Association recommends reference to or use of this document by government agencies and others, this document is purely voluntary and not binding unless adopted by reference in regulations.A listing of all publications, audiovisual programs, safety and technical bulletins, and safety posters is available via the Internet at our website at . For more information contact CGA at Phone: 703-788-2700, ext. 799. E-mail: customerservice@.Work Item 06-063Atmospheric Gases and Equipment Committee NOTE—Technical changes from the previous edition are underlined.TENTH EDITION: 2008REAFFIRMED: 2002NINTH EDITION: 1996EIGHTH EDITION:1987SEVENTH EDITION:1980© 2008 The Compressed Gas Association, Inc. All rights reserved.All materials contained in this work are protected by United States and international copyright laws. No part of this work may be reproduced or transmitted in any form or by any means, electronic or mechanical including photocopying, recording, or any informa-tion storage and retrieval system without permission in writing from The Compressed Gas Association, Inc. All requests for permission to reproduce material from this work should be directed to The Compressed Gas Association, Inc., 4221 Walney Road, Suite 500, Chantilly VA 20151. You may not alter or remove any trademark, copyright or other notice from this work.CGA G-4—2008 C OMPRESSED G AS A SSOCIATION,I NC. P AGE iiiContents Page 1Introduction (1)2Scope (1)3What is oxygen? (1)3.1Physical and chemical properties (1)3.2Manufacture (1)3.3Commercial uses (2)4Oxygen containers (3)4.1Federal regulations applying to containers (3)4.2Cylinders (3)4.3Tank cars (6)4.4Highway vehicles (6)5High pressure oxygen cylinders (7)5.1General (7)5.2Guidelines for safe storage (7)5.3Guidelines for safe handling (8)5.4Guidelines for safe use (9)5.5Procedure for withdrawing oxygen from cylinders (9)5.6Disposition of empty cylinders (10)6Estimating amount of oxygen in a cylinder (10)7Liquid oxygen (10)7.1Guidelines for safe storage, handling, and use (10)7.2Handling liquid oxygen in transfer systems or in open containers (12)8Storing, handling, and using liquid oxygen cylinders (12)8.1General (12)8.2Filling (12)8.3Moving cylinders (13)8.4Storage and use of cylinders (13)8.5Disposition of empty cylinders (14)9Oxygen piping and manifold systems (15)10Bulk oxygen systems (15)11Oxygen mixtures (15)12References (15)TableTable 1—Physical constants of oxygen (2)This page is intentionally blank.CGA G-4—2008 C OMPRESSED G AS A SSOCIATION,I NC. P AGE 11 IntroductionThis publication is one of a series of publications compiled by the Compressed Gas Association, Inc. (CGA) to satisfy the demand for information concerning the transportation, handling, and storage of compressed gases.2 ScopeThis publication provides general information regarding the characteristics and safe handling of oxygen. Re-quests for specialized technical information should be directed to any one of the manufacturers of this gas. This publication is intended primarily for users of oxygen and some of the requirements do not apply to manufactur-ers or distributors of this gas.3 What is oxygen?3.1 Physical and chemical propertiesOxygen is an element that exists at atmospheric temperatures and pressures as a colorless, odorless, tasteless gas. About one-fifth of the atmosphere is oxygen (20.95% by volume).The outstanding property of oxygen is its ability to sustain life and to support combustion. Although oxygen is nonflammable, materials that normally do not burn in air can burn in an oxygen-enriched atmosphere. Materials that burn in air will burn more vigorously and at a higher temperature in an oxygen-enriched atmosphere. Some combustibles, such as oil, burn in oxygen with near explosive violence if ignited by flame, impact, or some other energy source. As a result of these properties, caution should be exercised and special precautions taken when entering areas or confined spaces where an oxygen-enriched atmosphere can exist. Refer to CGA P-39, Oxygen-Rich Atmospheres and National Fire Protection Association (NFPA) 53 Recommended Practice on Materials, Equipment and Systems Used in Oxygen-Enriched Atmospheres,for more information regarding the hazards of oxygen-enriched atmospheres [1, 2].1As a gas, oxygen is 1.1 times heavier than air. It may be cooled and compressed to a pale blue liquid that, un-der atmospheric pressure, boils at –297.3 °F (–182.9 °C). As a liquid (at normal boiling point) oxygen is 1.14 times heavier than water. When heated above its critical temperature of –181.4 °F (–118.6 °C) oxygen can exist only as a gas, regardless of the pressure that may be exerted upon it.Oxygen is denoted according to type and grade or quality verification level (QVL). Gaseous oxygen is denoted as Type I and liquefied oxygen as Type II. The QVLs specify the maximum amount of various impurities (also termed limiting characteristics) that may be present. Further details are given in CGA G-4.3, Commodity Speci-fication for Oxygen [3].Some of the physical constants of oxygen are listed in Table 1.3.2 ManufactureBy far the primary method of manufacturing oxygen is by fractional distillation after the liquefaction of air. Liquid air is essentially a mixture of approximately one-fifth oxygen and four-fifths nitrogen. Nitrogen, having a lower boiling point, is allowed to volatilize, leaving oxygen in liquid form, which then can be further purified. Improved efficiency in utilization has led to a generally recognized industry standard of purity which exceeds the 99% required by the United States Pharmacopeia and National Formulary (USP–NF)[4]. Oxygen of lower purity may be used in some chemical and metallurgical processes. Other methods of manufacturing oxygen include pres-sure swing adsorption, vacuum swing adsorption, membrane separation, electrolysis, and chemical reaction. These processes produce oxygen at lower purities than that obtained by fractional distillation at cryogenic tem-peratures.1 References are shown by bracketed numbers and are listed in order of appearance in the reference section.P AGE 2 C OMPRESSED G AS A SSOCIATION,I NC. CGA G-4—2008Table 1—Physical constants of oxygen 2U.S. Units SI UnitsInternational symbol 1)O2O231.9988 Molecular weight 1) 31.9988At 70 °F (21.1 °C) and 1 atm: 2)kg/m3Density of gas 0.083 lb/ft3 1.329Specific gravity of gas 1.10 1.10m3/kgSpecific volume of gas 12.05 ft3/lb 0.752At 59 °F (15 °C) and 1 atm (101.325 kPa (abs): 2)kg/m3Density of gas 0.085 lb/ft3 1.362Specific gravity of gas 1.10 1.10m3/kgSpecific volume of gas 11.76 ft3/lb 0.734Boiling point at 1 atm 2)−297.3 °F –182.9 °CFreezing point at 1 atm 2)−361.1 °F –218.4 °CCritical temperature 2)−181.4 °F –118.6 °CCritical pressure 2)731.4 psia 5043 kPa, abskg/m3lb/ft3 436.1Critical density 2) 27.23Triple point 3)–361.8 °F at 0.0216 psia –218.8 °C at 0.1489 kPa, absLatent heat of vaporization at boiling point and 1 atm 4)91.7 Btu/lb 213 kJ/kgSpecific heat of gas at 70 °F (21.1 °C) and 1 atm: 2)C p0.220 Btu/lb (°F) 0.917 kJ/kg (°C)C v0.157 Btu/lb (°F) 0.653 kJ/kg (°C)Ratio of specific heat 1.40 1.40Solubility in water, vol/vol at 32 °F (0 °C) 1) 0.0489 0.0489Weight of liquid at boiling point 2)9.52 lb/gal 1141 kg/m31)Weast, R.C., Editor, CRC Handbook of Chemistry and Physics. 66th Edition, p. B–121.2)Younglove, B.A., “Interactive Fortran Program to Calculate Thermophysical Properties of Six Fluids.” National Bureauof Standards (U.S.), Tech. Note 1048 (July 1982).3)McCarty, R.D., “Interactive Fortran IV Computer Programs for the Thermodynamic and Transport Properties of Se-lected Cryogens (Fluid Pack).” National Bureau of Standards (U.S.), Tech. Note 1025 (October 1980).4)Snell, F.D. and Ettre, L.S., Encyclopedia of Industrial Chemical Analysis. Vol. 16, Table 3, page 517 (1972).uses3.3 CommercialThe principal uses of oxygen stem from the life-sustaining and combustion-supporting properties of the gas.Oxygen is extensively used for respiratory therapy purposes, for resuscitation in asphyxia, and in conjunctionwith other gases in anesthesia. For further information on the medical applications of oxygen and other gases,see CGA P-2, Characteristics and Safe Handling of Medical Gases [6]. Oxygen is also used to sustain life inhigh altitude aviation, deep sea diving, and similar applications.The industrial uses of oxygen include its use with acetylene or other fuel gases in such processes as metal cut-ting, welding, hardening, scarfing, cleaning, and dehydrating. Oxygen is also used in the manufacture of steeland in various chemical processes and as an oxidizer for fuels in rockets and missiles.2 kPa shall indicate gauge pressure unless otherwise noted as (kPa, abs) for absolute pressure or (kPa, differential) for dif-ferential pressure. All kPa values are rounded off per CGA P-11, Metric Practice Guide for the Compressed Gas Industry [5].CGA G-4—2008 C OMPRESSED G AS A SSOCIATION,I NC. P AGE 34 Oxygen containers4.1 Federal regulations applying to containersOxygen is classified by the U.S. Department of Transportation (DOT) and by Transport Canada (TC) as a non-flammable, oxidizing gas. If it is shipped in containers at a pressure exceeding 40.6 psia (280 kPa, abs) at 68 °F (20 °C), it shall be shipped in containers that meet DOT or TC specifications. DOT regulations are con-tained in Title 49 of the U.S. Code of Federal Regulations (49 CFR), Parts 100-180. TC regulations are con-tained in the Transportation of Dangerous Goods (TDG) Regulations that refers to Canadian Standards Asso-ciation (CSA) B339, Cylinders, Spheres, and Tubes for the Transportation of Dangerous Goods and CSA B340, Selection and Use of Cylinders, Spheres, Tubes and Other Containers for the Transportation of Dangerous Goods, Class 2 [7, 8, 9, 10]. Current authorizing agencies are DOT and TC while previous authorizing agencies included the Interstate Commerce Commission (ICC) in the United States and the Canadian Transport Com-mission (CTC), the Board of Trade Commissioners for Canada (BTC), and the Canadian Railway Commission (CRC) in Canada.Cylinders stamped with current or previous authorizing agency stampings may continue to be used provided they otherwise meet all qualifications for continued service.Cylinder specifications in the United States and Canada require, among other things, that the metal used in oxygen containers meet certain chemical and physical requirements, that the containers pass certain periodic requalification tests, and that the containers be protected by adequate pressure relief devices (PRDs). For oxy-gen containers authorized under DOT special permits/exemptions, the manufacturing, periodic requalifications, and PRD requirements are specified in the special permit/exemption paperwork. Specifications, as well as regulations governing maintenance, requalification, and testing are published by federal authorities of the DOT and TC.DOT specifications and regulations applying to the shipment of compressed gases are published in 49 CFR [7]. Canadian cylinder specifications and regulations applying to the shipment of compressed gases are published in Transportation of Dangerous Goods Regulations, which in turn refer to CSA B339 and CSA B340 [8, 9,10].4.2 Cylinders4.2.1 GeneralGaseous oxygen is commonly shipped in seamless steel cylinders constructed to TC/DOT specifications 3A or 3AA, with nominal capacities of up to 330 standard ft3 (9.34 m3). Higher pressure steel cylinders with greater capacities are also available. Oxygen may also be shipped in disposable (specification 39) or aluminum (speci-fication 3AL) cylinders.Liquid oxygen may be shipped in TC/DOT-4L insulated cylinders (commonly called liquid cylinders). A com-monly used specification 4L cylinder has an approximate equivalent capacity of 5000 ft3 (142 m3) of gaseous oxygen. Specification 4L cylinders having greater capacity are available.Liquid oxygen for home care medical applications is also shipped in smaller liquid cylinders. If the pressure dur-ing transportation does not exceed 25.3 psig (174 kPa), they are not required to meet DOT/TC specifications. See 49 CFR 173.320 for specific exceptions.In addition, oxygen may be shipped in cylinders made to a DOT special permit/exemption or TC special permit, if the exemption or permit allows this.4.2.2 Valve outlet connectionsContainer valve connections that do not fit must not be forced. Threads on regulator connections or other auxil-iary requirements must match those on the container valve outlet. The valve outlet connection should conform to recognized standards such as CGA V-1, Standard for Compressed Gas Cylinder Valve Outlet and Inlet Con-nections [11]. However, it must be acknowledged that connections other than those found in CGA V-1 may ex-ist. If a user chooses such a connection, extreme care must be taken to ensure that such connections do not cross-connect with existing connections in CGA V-1, and that they have been properly engineered for the in-P AGE 4 C OMPRESSED G AS A SSOCIATION,I NC. CGA G-4—2008 tended gas service and pressure. The threads on a cylinder valve outlet, as well as on regulators and other ancillary equipment, should be examined at frequent intervals to ensure they are clean and undamaged.4.2.3 Pressure relief devicesWith few exceptions, oxygen cylinders are required by federal regulations to be equipped with PRDs. These devices consist of a frangible disk designed to burst under excessive pressure, or a combination disk backed with fusible metal with a low melting point designed to melt and release the gas in case of fire. Cryogenic ves-sels may be equipped with spring-loaded pressure relief valves that reseat when the pressure drops to a pre-selected value. These devices are approved with respect to type and location by the federal authorities. See CGA S-1.1, Pressure Relief Device Standards–Part 1–Cylinders for Compressed Gase s[12].limits4.2.4 FillingBecause of the characteristics of any gas confined in a closed container to increase in pressure with rising temperature, the possibility always exists that a cylinder charged with gas at a safe pressure at normal tem-perature could reach a dangerously high pressure at high temperatures. To prevent this with normal usage, federal regulations limit the amount of gas that may be charged into a cylinder.TC/DOT-3A, TC/DOT-3AA and TC/DOT-3AL and TC/DOT-39 cylinders shall not be filled to a pressure higher than the stamped service pressure at 70 °F (21.1 °C). TC/DOT-3A and TC/DOT-3AA cylinders stamped with a plus mark (+) after the last test date may be filled to a pressure 10% higher than the stamped service pres-sure under conditions described in 49 CFR 173.302a [7]. This also applies to cylinders stamped ICC, CTC, BTC, and RTC.Metricated TC-3A and TC-3AA cylinders, identified by the letter M stamped at then end of the specification des-ignation and not stamped with a K after the service pressure, have the 10% overfill included in the stamped service pressure and may be filled to that pressure at 59 °F (15 °C), if equipped with a PRD(s) of the rupture disk type without fusible metal backing. If a K is stamped after the service pressure, the cylinder shall be filled to only 90% of the stamped service pressure. (See CSA B340) [10].Note that metricated TC cylinders have their service pressure stamped in bar. One bar is equal to 100 kPa, or approximately 14.5 psi.If the liquid container pressure is equal to or less than 25.3 psig (174 kPa), TC/DOT-4L container filling opera-tion is not regulated (see 49 CFR 173.320). Above 25.3 psig (174 kPa), TC/DOT-4L cylinders must be filled by weight in accordance with regulations. DOT and TC regulations prescribe permissible fill rates in 49 CFR 173.316 and CSA B340 [7, 10].4.2.5 RetestingIn addition to the hydrostatic testing of cylinders at the time of manufacture, federal regulations provide that specification 3A, 3AA, and 3AL cylinders shall be periodically retested. When using hydrostatic testing methods for retesting, DOT, CTC, ICC, BTC, and CRC cylinders are tested at 5/3 of their stamped service pressure, while metricated TC cylinders are tested at 3/2 of their stamped service pressure. See 49 CFR Part 180 Sub-part C [7]. Specification 3A, 3AA and 3AL cylinders shall be hydrostatically retested at 5-year intervals. Under certain conditions prescribed in federal regulations, the interval may be 10 years for 3A and 3AA cylinders. Such cylinders are stamped with a 5-pointed star following the last test date. Retesting of 4L liquid cylinders is not required. Specification 39 cylinders may not be refilled and hence require no retest. Retesting of 3E cylin-ders is not required.In the United States, specification 3A and 3AA cylinders that have been in a fire shall be removed from service and cannot be returned to service until they meet the requirements of 49 CFR 180.212. Specification 3AL cyl-inders that are exposed to fire or temperatures in excess of 350 °F (177 °C) shall be removed from service and condemned. Specification 4L cylinders that are in a fire shall be removed from service until meet the require-ments of 49 CFR 180.211.If a specification 3A, 3AA, or 3AL cylinder leaks, shows evidence of damage that can weaken it appreciably, or shows a permanent expansion that exceeds 10% of the total expansion in the retest, it shall be condemned.CGA G-4—2008 C OMPRESSED G AS A SSOCIATION,I NC. P AGE 5 See 49 CFR 180.205. Cylinders condemned because of excessive permanent expansion may be rebuilt in ac-cordance with 49 CFR 180.211 and 49 CFR 180.212.Specification 3A and 3AA cylinders to be charged to a pressure 10% in excess of the marked service pressure shall be retested in accordance with conditions prescribed in federal regulations and shall be marked with a plus sign (+) following the last test. See 49 CFR 180.213. Aluminum cylinders may not be charged to a pres-sure 10% in excess of the marked service pressure.Records shall be kept giving data showing the results of the tests made on all cylinders, and each cylinder passing the test shall be plainly and permanently stamped with the month and year of the test as well as the retester’s identification number. Dates of previous tests shall not be obliterated.4.2.6 Marking and labeling4.2.6.1 Department of Transportation and Transport Canada required markingsThe following marks are required by DOT and TC to be plainly and permanently stamped on the shoulder, top, head, or neck of all cylinders:–The authorizing agency abbreviation, followed by the specification and service pressure. For example, a high pressure cylinder may be stamped CTC/DOT-3AA2265 or a metricated TC cylinder may be stamped TC-3AAM 184 where the M denotes that it is a metricated cylinder. On liquid cylinders the stamping is gen-erally on a plate affixed to the container and may be CTC/DOT-4L200 or TC-4LM29;– A serial number and identifying symbol of the cylinder manufacturer. The symbol shall be registered in ac-cordance with federal regulations;–The inspector’s official mark and date of the test to which the cylinder was subjected in manufacture. The word SPUN shall be added when an end closure is made by the spinning process; the word PLUG shall be added when an end closure is effected by plugging; and–All subsequent retest dates, including the registered symbol of the authorized retester.The required markings on cylinders shall not be changed except as provided in federal regulations.4.2.6.2 ShippingPrior to shipment, each cylinder shall be legibly marked in accordance with DOT and TC regulations. Each DOT/TC label shall include the proper shipping name of the contained material, the hazard symbol, and the corresponding identification number. See 49 CFR 172.101 [7]. Such marking shall be by means of stenciling, stamping, or labeling, and shall not be readily removable. See CGA C-7, Guide to the Preparation of Precau-tionary Labeling and Marking of Compressed Gas Containers, for suggested precautionary warning on labels [13].In Canada the set of regulations collectively known as Workplace Hazardous Materials Information System (WHMIS) requires that precautionary labels in a prescribed format shall be applied to all cylinders destined for use in a workplace.4.2.6.3 LabelsDOT regulations require that in addition to marking of the proper shipping name and identification number on a cylinder, a 100 mm (3.9-in) diamond (square-on-point) green label (designating a nonflammable gas) having the number 2 in the lower corner plus a 100 mm (3.9-in) diamond (square-on-point) yellow label (designating a subsidiary risk as an oxidizer) having a 5.1 in the lower corner be attached to each cylinder containing oxygen when transported by common carrier. In lieu of using the two 100 mm (3.9-in) diamond (square-on-point) la-bels, DOT authorizes the use of a single 100 mm (3.9-in) diamond (square-on-point) yellow label (designating an oxidizer) having the number 2 in the lower corner and having the mandatory word OXYGEN printed on it. Alternately, DOT regulations allow the use of 30 mm (1.25-in) square-on-point labels as long as the cylinder(s) is not over packed and are durably and legibly marked in accordance with CGA C-7, Appendix A [13]. See 49 CFR 172.400a(1).P AGE 6 C OMPRESSED G AS A SSOCIATION,I NC. CGA G-4—2008 In Canada one diamond-shaped label is required. The label shall be yellow, have the oxidizer symbol on it, and have a 2 at the bottom corner. In Canada, hazard class wording is not allowed on labels; whereas, in the United States it is optional.In Canada, the general requirement is for each side of a label to be at least 100 mm in length with a line run-ning 5 mm inside the edge. However, if that size label, together with the shipping name, technical name, and UN number, cannot be displayed because of the irregular shape or size of the small means of containment, each side of the label may be reduced in length by the same amount to the point where the label, together with the shipping name, technical name, and UN number, will fit that small means of containment, but must not be reduced to less than 30 mm.The proper shipping name for gaseous oxygen and product identification number is Oxygen, UN 1072. For liq-uid oxygen it is Oxygen, Refrigerated Liquid, UN 1073.4.2.6.4 FillingFederal regulations forbid the shipment of cylinders containing oxygen unless they were charged by or with the consent of the cylinder owner. If this consent should be granted, the recharging of cylinders shall comply in every respect with federal regulations.4.3 Tank carsHigh pressure, gaseous oxygen may be transported in tank cars complying with DOT specification 107A. Such cars are constructed of a number of seamless steel containers (tubes) permanently mounted on a special rail car frame. Regulations for tank cars are found in 49 CFR in the United States and Canadian General Stan-dards Board (CGSB) Standard 43.147, Construction, Modification, Qualification, Maintenance and Selection and Use of Means of Containment for the Handling, Offering for Transport, or Transporting of Dangerous Goods by Rail [7, 14].Liquid oxygen is transported in vacuum insulated tank cars at pressures below 25.3 psig (174 kPa). DOT/TC regulations include requirements that apply to shipping papers, marking the container with the proper DOT/TC identification number, placarding, and incident reporting. Although marking the container with the proper DOT/TC shipping name is not required, it is recommended since the proper shipping name is a cross reference to the emergency response guidebook information. It is prudent, however, to mark tank cars transporting liquid oxygen on each side with the words LIQUID OXYGEN. DOT and TC regulations should be consulted for mark-ing and documentation requirements.4.4 Highway vehiclesFederal regulations authorize the transportation of high pressure, gaseous oxygen in truck trailers. These trail-ers have large tubes permanently installed upon them. These tubes are constructed to TC/DOT specification 3A, 3AA, 3AX, 3T or 3AAX and are manifolded together to a common header. Such trailers are usually towed to the point of use by a truck tractor. The applicable standards for this mode of transport are in 49 CFR in the United States and CSA B339 and B340 in Canada [7, 9, 10].Bulk liquid oxygen is usually transported in vacuum-insulated cargo tanks at pressures below 25.3 psig (174 kPa). Both DOT and TC regulations include requirements that apply to the shipping papers, marking, placarding, and incident reporting.Cargo tanks that operate at an over-the-road pressure below 25.3 psig (174 kPa) are exempted from many requirements of the DOT regulations in the United States, although they are usually manufactured in accor-dance with the CGA 341 specification [15]. See 49 CFR 173.320 for specific exceptions. In Canada, TC 341 specification highway tanks are used to transport bulk liquid oxygen at an over-the-road pressure at or below 175 kPa (25.3 psig), in accordance with CSA B620, Highway Tanks and Portable Tanks for the Transportation of Dangerous Goods and CSA B622, Selection and Use of Highway Tanks, Multi-Unit Tank Car Tanks, and Portable Tanks for the Transportation of Dangerous Goods, Class 2 [16, 17]. CSA B622 also grandfathers CGA 341 specification cargo tanks manufactured prior to January 1, 2003 and permits their use as a substitute for TC 341 specification highway tanks.Cargo tanks that operate at an over-the-road pressure above 25.3 psig (174 kPa) shall be constructed in ac-cordance with the TC/MC-338 specification covered in 49 CFR, CSA B620, and CSA B622 [7, 16, 17].The applicable standards are found in 49 CFR, CSA B620, and CSA B622 [7, 16, 17].5 High pressure oxygen cylinders5.1 GeneralOxygen cylinder users should comply with all federal, state, provincial, territorial, and local regulations.5.2 Guidelines for safe storageThe following are guidelines for safe storage:–Cylinders should be stored in a definitely assigned location;–Do not place cylinders near flammable material, especially oil, grease, or any other readily combustible substance;–Do not allow oxygen cylinders to stand under places where oil can drip on the cylinder, its valve, or other attachments;–Cylinders shall not be stored in an acetylene generator room or in close proximity to cylinders containing acetylene or other flammable gases. Unless separated by a distance of 20 ft (6.1 m), there shall be a non-combustible barrier at least 5 ft (1.5 m) high with a fire-resistance rating of at least 1/2 hour between the oxygen cylinders and the acetylene or other flammable gas cylinders;–Cylinders should not be stored above 125°F (51.7 °C) or used above 120 °F (48.9 °C). Cylinders should never be allowed to reach a temperature exceeding 125 °F (51.7 °C) because of the rise in pressure in the cylinder with increasing temperature. Therefore, cylinders should never be placed near furnaces, radiators, or any other source of heat;–Cylinders should be protected from abnormal mechanical shock, which is liable to damage the cylinder, valve, or PRD;–Do not place cylinders near elevators, gangways, or in locations where heavy moving objects can strike them or fall on them;–Cylinders in service or in storage shall be stored standing upright where they are not likely to be knocked over, or the cylinders shall be secured;–Small cylinders may be stored and used in a horizontal position if the cylinder is installed in a holder or cradle designed to secure the cylinder and protect the valve and regulator;–Valve protection caps, when provided, shall be in place and fastened hand-tight, except when cylinders are in use or connected for use;–Cylinders should be protected from tampering;–Storage should be planned so cylinders can be used in the order they are received from the supplier;–Empty and full cylinders should be stored separately and empty cylinders should be marked to avoid con-fusion;–Cylinders should be stored in dry, well-ventilated locations in such a manner as to prevent accidental movement;–Cylinders should not be exposed to continuous dampness and should not be stored near salt or other cor-rosive chemicals or fumes. Rusting will damage the cylinders and can cause the valve protection caps to stick;–Cylinders should be stored on a suitable foundation such as concrete or steel grating; and。
黑翼飞行模拟器用户手册说明书
IntroductionThe Blackwing BW 635RG is an ultralight two-seater aeroplane designed for recreational flying and training purposes. It features a sleek and modern design, with a composite airframe and a low-wing configuration. The Blackwing has a cruising speed of up to 120 knots and a range of approximately 700 nautical miles, making it suitable for both short and long-distance flights. The cockpit is equipped with state-of-the-art avionics, including a glass cockpit display and an autopilot system. The Blackwing is also known for its superior handling and stability, making it a popular choice among flying enthusiasts and flight schools. The BW 635RG is powered by the venerable Rotax 915 iS engine.Development Credits:Mal Cartwright Product LeadRuss White3D Modelling, Interior and Exterior TexturingJack Lavigne IntegrationHarry Stringer AnimationPropAir Flight Model and SystemsJordan Gough ManualWith special thanks to our Beta Testers:Rob Abernathy John BurgessNick Cooper John DowMatt McGee Darryl WightmanTable of ContentsIntroduction (2)Development Credits: (2)With special thanks to our Beta Testers: (2)Table of Contents (3)Notes on Hardware (4)Overview (5)Aircraft Limitations (6)Airspeed Limitations (6)Engine Limitations (6)Operating Conditions (6)Fuel (7)Other Limitations (7)Emergency Procedures (8)Engine Failure on the Take-off Roll (8)Engine Failure after Take-off (8)Glide Performance (8)Emergency Landing (9)Spin Recovery (9)Normal Procedures (10)Before Starting Engine (10)Starting Engine (10)Before Taxiing (11)Taxiing (11)Engine Runup (11)Before Take-off (11)Take-Off (12)Initial Climb (12)Cruise Climb (12)Cruise (12)Landing (13)Balked Landing (13)After Landing (13)Securing Aircraft (14)Basic Performance (15)Stall Speeds (15)Take-Off Performance (15)Landing Performance (16)Systems Description (17)Instrument Panel Layout (17)Switch Logic and Electrical System (18)Master Switch (18)Fuel Pump Switch (19)LAND/TAXI Switch (19)Strobe/Nav Switch (19)Electrical System Diagram (20)Engine (21)Propeller (21)Fuel (21)Notes on HardwareDue to the unusual 3-position switches in this aircraft, conventional hardware 2position toggle switches (eg. strobe or nav light switches) cannot be translated tothe single 3-position switch which combine these.Additionally, as this aircraft utilises a single level power control (throttle), conventional throttle/prop/mixture hardware may interfere with the function of this system, and not work as intended. It is recommended to place your propeller and mixture levers in the IDLE position, and not move them while the engine is running.OverviewThe Orbx BW 635RG has been developed using official documentation and Computer Aided Design (CAD) resources from Blackwing Sweden. As a result, the aeroplane has been created through masterful modelling, texturing, systems integration, and flight model development.Figure 1 – Aircraft 3-viewAircraft DimensionsLength 6.6m Height 2.2m Wingspan8.4mWeightsBasic Empty Weight 375kg Maximum Take-off Weight 600kg Maximum Fuel Capacity (Litres)130LThe content in this manual and the operation of the BW 635RG in Microsoft Flight Simulator strictly must not be used as reference material in any form for operating the real aircraft.Aircraft LimitationsAirspeed LimitationsAirspeed Description Airspeed (KIAS) RemarksVne Never Exceed Speed 157 Must not exceed this speed in any operation.Va Manoeuvring Speed 109 If full or abrupt control deflection is made, the airframe may be overstressed.Vfe1 Max flap extended speed20 degrees90 Maximum speed for flaps 20°Vfe2 Max flap extended speed35-45 degrees 70 Maximum speed for flaps 35-45°Vlo Maximum landing gearoperating speed 70Do not extended or retract the landing gearabove this speed.Vle Maximum landing gear extended speed 90 Do not exceed this speed with the landing gearalready down.Vs0 Stall speed flaps/gearextended 38 Stall speed with gear down/flaps >0° and in level flight at MTOWVs1 Stall speed clean 49 Stall speed flaps retracted, gear up and in level flight at MTOWEngine LimitationsEngineEngine Manufacturer Rotax Engine Model Rotax 915 iSMaximum Power Take-off (Max 5 min.) 141 hp Continuous 135 hpMaximum RPM Take-off (Max 5 min.) 5800 Continuous 5500Critical Altitude 15000ft AMSL Maximum OperatingAltitude23000ft AMSL Operating ConditionsAerobatic manoeuvres, flight in IFR conditionsand flights in icing conditions are prohibited inthis aircraft.FuelFuel TanksLeft Right Litres US Gal Litres US GalTotal Fuel in Tank 67.5 17.8 62.5 16.5Unusable Fuel 2.5 0.7 2.5 0.7 Total Useable Fuel in Tanks 66.5 17.6 61.5 16.2Other LimitationsMaximum demonstrated crosswind for the BW 635RG is 20 knots.Emergency ProceduresNote: The following procedures have been modified to be suitable for simulation. It does not cover emergencies that are a) not simulated and b) not reasonable. Checklist items from the real procedures have been omitted and these procedures must not under any circumstances be used for training purposes.Engine Failure on the Take-off RollThrottle: IDLEIgnition: OFFFuel Pump: MAIN (DOWN POS)Brakes: APPLYWhen stopped: SECURE AIRCRAFTEngine Failure after Take-offNose: IMMEDIATELY LOWERAirspeed: 65 KNOTSLanding Area: DETERMINE WITHIN 30° OF NOSEFlaps: USE AS REQUIREDLanding Gear: USE DESCRETIONFuel Selector: OFFIgnition: OFFMaster Switch: OFFGlide PerformanceThe BW 635RG, the approximate performance for a glide is 65 KIAS which willgive approximately a 545ft/min rate of descent in the clean configuration.Glide performance will degrade significantly on extension of flaps and landinggear.Emergency LandingAirspeed: 65 KIASField: PICK BEST OPTIONLanding Gear: USE DISCRETION DEPENDING ON FIELD TYPEFlaps: AS REQUIREDFuel Selector: OFFIgnition: OFFFuel Pump: MAIN (down)Master Switch: OFF BEFORE LANDINGSpin RecoveryThrottle: IDLEControl Stick: AILERON NEUTRALRudder: FULL OPPOSITE TO DIRECTION OF ROTATIONControl Stick: POSITIVELY FORWARD OF NEUTRALRudder: NEUTRAL WHEN ROTATION STOPSControl Stick: SMOOTHLY PULL OUT OF DIVEWARNING:INTENTIONAL SPINS ARE NOT APPROVED INTHIS AIRCRAFT.Normal ProceduresNote: The pre-flight inspection portion of the normal procedures has been removed due to impracticality in the simulator.Before Starting EngineIgnition: OFFMaster Switch: OFF (down)Backup Battery: OFF/AUTO (down)Landing Gear Lever: DOWNCircuit Breakers: INCanopy CLOSED (CLICKING THE LATCHON THE INSIDE LEFT SIDEWALL.) Starting EngineParking Brake: HOLD TOE BRAKES AND ENGAGE PARKINGBRAKEMaster Switch: ENGINE START (middle position)Fuel Selector: SETFuel Gauge: CHECKFuel Pump: BOTH (up)Ignition: BOTHNav Lights: STROBE (middle position)Throttle: SET ½-1 INCH OPENIgnition: STARTOil Pressure: GREEN WITHIN 10 SECWarnings: NONEBefore TaxiingMaster Switch: NORMAL OPERATION (up)Altimeter: SETAvionics: SETParking Brake: DISENGAGETaxiingInstruments: CHECKED (COMPASS/HSI/BALL/ATT) Engine RunupParking Brake: ENGAGERPM: 2500 RPMFuel Pump: CYCLE, CHECK FUEL PRESSUREIdle: CHECK IDLE 1800 +/- 100 RPM Before Take-offCanopy: CLOSED AND LOCKEDFlaps: 1 STAGE (20°)Elevator Trim: SET FOR TAKE-OFFEngine Instruments: NORMALLanding Light: ON (up)Controls: FULL FREE AND CORRECT MOVEMENTParking Brake: DISENGAGETake-OffThrottle: FULLControls: NEUTRAL45 Knots: ROTATEAccelerate: NOSE ON HORIZON, ACCEL TO 80 KIASPositive Rate of Climb: GEAR UPLanding Light: OFF (down)Flaps: RETRACT ABOVE 500’ AGLInitial ClimbThrottle: MAX CONTINUOUS (5500 RPM)Airspeed: 90 KIASFuel Pump: MAIN (down) ABOVE 500’ AGL Cruise ClimbThrottle: MAX CONTINUOUS (5500 RPM)Airspeed: 130 KIASCruiseThrottle: 55-75% PowerAirspeed: 120-157 KIAS (<130 KIAS IN TURB)LandingFuel: QTY CHECKEDFuel Selector: FULLEST TANKFuel Pump: BOTH (up position)Airspeed: 90 KIASFlaps: EXTEND FLAP 1 <90 KIASDownwind Airspeed: 65 KIASLanding Gear: DOWN @ 65 KIAS; CHECK 3 GREENLanding Light: ON (up position)Base Leg: EXTEND FLAP 2 < 65 KIASFinal Approach Airspeed: 60 KIASBalked LandingThrottle: SMOOTHLY INCREASEAirspeed: 60 KIASTrim: COURSE TRIM TO RELIEVE PRESSUREFlaps: RETRACT TO POSITION 1 (20°)Gear: UPTrim: TRIM FOR CLIMBAfter LandingFlaps: RETRACTExterior Lights: AS REQ’DFuel Pump: MAIN (down)Securing AircraftParking Brake: ENGAGEDThrottle: IDLESwitches: ALL OFF EXCEPT ACL AND MASTERIgnition: OFFNav Lights: OFF (down)Master Switch: OFFBasic PerformanceStall SpeedsMTOW 600kg | CG 32% MAC | Power Idle | Level FlightFlap Position Stall Speed (KIAS) 0° 49 20° 44 35° 39 45°38Take-Off PerformanceMTOW | ISA CONDITIONS | SEA LEVEL | FLAPS 1 (20°) | MTOW (600kg)Cruise PerformanceRunway Surface Ground RollOver 50ft Obstacleft mft mPaved Runway328 100 656 200 Unpaved (Grass) Runway 361110689208Pressure Altitude Power (%) TAS Fuel Flow LPH MAP (inHg) Endurance(hr)Range (nm) 500055 161 19.7 30 5.8 941 65 170 23.3 34.1 4.9 827 7517826.937.44.1738Landing PerformanceMTOW | ISA CONDITIONS | FLAPS 2 (35°) | MTOW (600kg) | Speed 1.3 x VsoRunway Surface Ground Roll Over 50ft Obstacle ft m ft mPaved Runway 525 160 951 290 Unpaved (Grass) Runway 558 170 984 300Systems Description Instrument Panel LayoutSwitch Logic and Electrical SystemThe electrical switches in the BW 635RG are 3-position switches. These are generally known as “DOWN”, “MIDDLE” and “UP”. They are briefly explained below.Master SwitchThe MASTER switch functions in a unique way, with the following switch logic:1.When the MASTER switch is DOWN, all battery power is off. There will beno electrical power provided to the aircraft.•Note: The engine CANNOT be shut down when the master switch isoff. Electrical power must be present for the engine to turn off.2.When the MASTER switch is in the MIDDLE (Engine Start) position, limitedsystem functionality will be present. The backup battery will be activatedand power the following systems:•Primary Flight Display•Compass•AHRS (Attitude Heading Reference System)•Radio3.When the MASTER switch is UP (Normal Operation), full electrical supplywill be provided to the aircraft. The following systems will be powered on: •Note: the engine CANNOT be started with the MASTER switch in theUP position. If the engine won’t start, check the switch is in theMIDDLE position•Multi-Function Display•Transponder•Autopilot•Audio panel•STBY instruments•Pitot Heat•Main battery is disconnected from running engine. Alternatorprovides power.See Section NORMAL PROCEDURES for positioning of the MASTER switch.Fuel Pump SwitchThe Fuel Pump switch also has some advanced logic to it, due to two fuel pumpsbeing present, however, to put it simply, it operates in the following way:1.In the DOWN position, the main fuel pump is in use.2.In the MIDDLE position, the auxiliary fuel pump is in use.3.In the UP position, both fuel pumps will be on.LAND/TAXI SwitchThe LAND/TAXI switch powers the Taxi and Landing lights. It operates in the following logic:1.In the DOWN position, both lights will be OFF.2.In the MIDDLE position, the taxi light will switch on when the landinggear is extended.3.In the UP position, the Landing Light will switch on when the landinggear is extended.Strobe/Nav SwitchThe Strobe/Nav switch powers the Navigation (Red/Green) and Strobe (flashingwhite) lights. It operates in the following logic:1.In the DOWN position, both lights will be OFF.2.In the MIDDLE position, the STROBE light will be on.3.In the UP position, both the strobe and Nav lights will be on.Electrical System DiagramThe BW 635RG’s electrical system is modelled in the following way in Microsoft Flight Simulator.Because the starter system is connected to the BACKUP BUS, this means you cannot start the engine with the MASTER switch in the UP position, due to the BACKUP BUS being disconnected from the circuit once the MAIN BAT BUS is powered.Page 21 of 21User Guide v1.0 –RevisionEngineThe BW 635RG is powered by the Rotax 915iS. The Rotax 915iS is a four-stroke, four-cylinder, fuel-injected, turbocharged aircraft engine with a maximum power output of141 horsepower. The engine utilizes electronic fuel injection (EFI) technology toprovide precise fuel delivery and improved fuel efficiency. It also features a modernliquid-cooling system and a dual electronic ignition system for reliable performance.The Rotax 915iS engine has a maximum operating RPM of 5,200, with a recommended continuous operation range of 5,000 RPM or less.PropellerThe propeller is a 3-blade wood-composite design, which is hydraulically adjustable for operation at various pitch angles, controlled independently of the pilot. The propeller is linked to the engine through an electronically controlled governor, where RPM isadjusted in accordance with the position of the throttle control. This pitch curve cannot be adjusted in flight, however is designed to ensure maximum performance in allphases of flight.FuelBoth wings have fuel tanks, which are fed to the engine via electric fuel pumps. Fuelsystem information is fed via sensors to the Garmin avionics suite and can be viewedon the displays inside the cockpit.AIRPLANE WEIGHTSBasic Empty Weight……………………….…375 KgMaximum Takeoff Weight…………………..600 KgMaximum Fuel Weight………………………...95 Kg Maximum Landing Weight………………….600 Kg TANK USABLE FUEL LEFT WING TANK67.5 litres 17.8 US Gallons RIGHT WING TANK62.5 litres 16.5 US Gallons TOTAL 130 litres34.3 US GallonsFUEL CAPACITY AIRSPEEDS Never Exceed Speed ……….…………….173 KIAS Max Structural Cruising Speed…………..156 KIAS Maneuvering Speed MTOW……………….109 KIAS Initial Climb………………………………………80 KIASBest Angle Climb……………………………….75 KIASBest Rate of Climb……………………………..90 KIASMax Flap Ext 20°……………………..............90 KIASMax Flap Ext 35-45°……………………………70 KIASMax Landing Gear Operation……………….70 KIASMax Landing Gear Extended………………..90 KIASPlanned Cruise TAS………………………….130 KIASFinal Approach Speed………………………..60 KIAS POWERPLANT LIMITATIONSENGINE LIMITS (RPM)Take-off (5 Minutes)………....5800 RPM Max Continuous……………….5500 RPMALTITUDE LIMITSMaximum Operating Altitude………………23 000ftFor Microsoft Flight Simulator Use Only0-12023 Orbx Simulation Systems Pty. Ltd BW 635RG QUICK REFERENCESHEETIssued: 21 Apr 2023Revised: 21 Apr 20230-2PROCEDURESBEFORE STARTING ENGINEPreflight Inspection………………………….COMPLETECrew Briefing………………………………….COMPLETEIgnition…………………………………………………….OFFMaster Switch…………………………………………..OFFBackup Battery …..…………………………….OFF/AUTOLanding Gear Lever………………………………..DOWNCircuit Breakers…………………………………………..IN Canopy………………………………………………CLOSED STARTING ENGINEArea……………………………………………………..CLEARParking Brake……………….HOLD TOE BRAKES ANDENGAGEMaster Switch …..……………….ENGINE START (MID)Fuel Selector…………………………………………….SETFuel Pump………………………………………BOTH (UP)Ignition………………………………………………….BOTHExternal Lights……………………………………..AS REQThrottle ………………………..………..Τ12-1 INCH OPENIgnition………………………………………………….START AFTER START Oil Pressure.…………………………………………RISING Master Switch ……………………………..NORMAL (UP)Radios………………………………………………………SET Altimeter…………………………………………………..SET ATIS and Clearance…………………………..OBTAINEDBEFORE TAXIBrakes/Park Brake ………………………….DISENGAGEFlight Instruments……………………………..CHECKEDCompass…………………………………………CHECKED BEFORE TAKEOFFCanopy/Harnesses………………………………SECURE Flaps…………………………………….……1 STAGE (20°)Trim ..……………………………………SET FOR TAKEOFF Flight Instruments………………………………………SET Engine Instruments………………CHECKED NORMAL Avionics…………………………………………………….SET External Lights………………………………………AS REQ Flight Controls…………..FULL, FREE AND CORRECT Takeoff Safety Brief………………………….DELIVERED TAKEOFFBrakes/Park Brake………………………….DISENGAGEPower…………SMOOTHLY INCREASE TO MAXIMUM45 knots………………………………………………ROTATEAccelerate……….…NOSE ON HORIZON, TO 80 KTSPositive Rate of Climb………………………….GEAR UPLanding Light.……………………………….OFF (DOWN)Flaps ………………………..RETRACT ABOVE 500’ AGLMEMORY ITEMS 2023 Orbx Simulation Systems Pty. Ltd ENGINE RUN UP Parking Brake ……………………………………..ENGAGE Engine Instruments……………………………CHECKED Engine RPM…………………………………SET 2500 RPM Fuel Pump…………………………………………….CYCLE Idle …………………..…..CHECK IDLE 1800 ±100RPM Navigation Equipment …..…………………………….SETFor Microsoft Flight Simulator Use OnlyIssued: 21 Apr 2023Revised: 21 Apr 2023AFTER TAKEOFF Engine Instruments……………………..WITHIN LIMITS Climb Speed…………………………………………90 KIAS Fuel Pump………….MAIN (DOWN ) ABOVE 500’ AGL0-3CRUISEPower….……………………………………….SET 55-75%Airspeed…..……….120-157KTS (<130KTS IN TURB.)DESCENTAltimeter…………………………………………………..SETFuel Selector………………………………FULLEST TANKPower Lever………………….AS REQUIRED FOR RODApproach Brief………………………………PLETE BEFORE LANDINGBrakes……………………………………………………..OFFFuel ………….………………………………QTY CHECKEDFuel Selector………………………………FULLEST TANK Fuel Pump……….………………………………BOTH (UP)LANDINGDOWNWINDAirspeed….………………………………………….90 KIASFlaps….………………………………………STAGE 1 (20°)Airspeed………….………………………………….65 KIASLanding Gear…..…………………….DOWN @ 65 KIASCHECK 3 GREENLanding Light………………………………………ON (UP)BASEFlaps…………………………… STAGE 2 (35°) < 65 KIASFINALAirspeed………….………………………………….60 KIASTouchdown ……………………….MAIN WHEELS FIRSTStick………………………………………………FULL BACK Brakes…………………………………………………..APPLYAFTER LANDING Flaps………………………………………………..RETRACT Landing Lights…………………………………………..OFFFuel Pump….………………………………MAIN (DOWN)SHUTDOWNParking Brake ……………………………………..ENGAGE Throttle……………………………………………………IDLE Switches….………………………….OFF EXCL. MASTERIgnition..…………………………………………………..OFFLights….……………………………………….OFF (DOWN)Master Switch..……………………………..OFF (DOWN)MEMORY ITEMS 2023 Orbx Simulation Systems Pty. Ltd For Microsoft Flight Simulator Use OnlyPROCEDURESIssued: 21 Apr 2023Revised: 21 Apr 2023。
IATA AHM目录
Airport Handling ManualEffective 1 January—31 December 201838NOTICEDISCLAIMER. The information contained in thispublication is subject to constant review in the lightof changing government requirements and regula-tions. No subscriber or other reader should act onthe basis of any such information without referringto applicable laws and regulations and/or withouttak ing appropriate professional advice. Althoughevery effort has been made to ensure accuracy, theInternational Air Transport Association shall not beheld responsible for any loss or damage caused byerrors, omissions, misprints or misinterpretation ofthe contents hereof. Furthermore, the InternationalAir Transport Association expressly disclaims anyand all liability to any person or entity, whether apurchaser of this publication or not, in respect ofanything done or omitted, and the consequencesof anything done or omitted, by any such person orentity in reliance on the contents of this publication.Opinions expressed in advertisements appearing inthis publication are the advertiser’s opinions and donot necessarily reflect those of IATA. The mentionof specific companies or products in advertisementdoes not imply that they are endorsed or recom-mended by IATA in preference to others of a simi-lar nature which are not mentioned or advertised.© International Air Transport Association. AllRights Reserved. No part of this publication maybe reproduced, recast, reformatted or trans-mitted in any form by any means, electronic ormechanical, including photocopying, record-ing or any information storage and retrieval sys-tem, without the prior written permission from:Senior Vice PresidentAirport, Passenger, Cargo and SecurityInternational Air Transport Association800 Place VictoriaP.O. Box 113Montreal, QuebecCANADA H4Z 1M1Airport Handling ManualMaterial No.: 9343-38ISBN 978-92-9229-505-9© 2017 International Air Transport Association. All rights reserved.TABLE OF CONTENTSPage Preface (xv)Introduction (xvii)General (1)AHM001Chapter0—Record of Revisions (1)AHM011Standard Classification and Numbering for Members Airport Handling Manuals (2)AHM012Office Function Designators for Airport Passenger and Baggage Handling (30)AHM020Guidelines for the Establishment of Airline Operators Committees (31)AHM021Guidelines for Establishing Aircraft Ground Times (34)AHM050Aircraft Emergency Procedures (35)AHM070E-Invoicing Standards (53)Chapter1—PASSENGER HANDLING (91)AHM100Chapter1—Record of Revisions (91)AHM110Involuntary Change of Carrier,Routing,Class or Type of Fare (92)AHM112Denied Boarding Compensation (98)AHM120Inadmissible Passengers and Deportees (99)AHM140Items Removed from a Passenger's Possession by Security Personnel (101)AHM141Hold Loading of Duty-Free Goods (102)AHM170Dangerous Goods in Passenger Baggage (103)AHM176Recommendations for the Handling of Passengers with Reduced Mobility(PRM) (105)AHM176A Acceptance and Carriage of Passengers with Reduced Mobility(PRM) (106)AHM180Carriage of Passengers with Communicable Diseases (114)AHM181General Guidelines for Passenger Agents in Case of SuspectedCommunicable Disease (115)Chapter2—BAGGAGE HANDLING (117)AHM200Chapter2—Record of Revisions (117)AHM210Local Baggage Committees (118)AHM211Airport Operating Rules (124)Airport Handling ManualPageChapter2—BAGGAGE HANDLING(continued)AHM212Interline Connecting Time Intervals—Passenger and Checked Baggage (126)AHM213Form of Interline Baggage Tags (128)AHM214Use of the10Digit Licence Plate (135)AHM215Found and Unclaimed Checked Baggage (136)AHM216On-Hand Baggage Summary Tag (138)AHM217Forwarding Mishandled Baggage (139)AHM218Dangerous Goods in Passengers'Baggage (141)AHM219Acceptance of Firearms and Other Weapons and Small Calibre Ammunition (142)AHM221Acceptance of Power Driven Wheelchairs or Other Battery Powered Mobility Aidsas Checked Baggage (143)AHM222Passenger/Baggage Reconciliation Procedures (144)AHM223Licence Plate Fallback Sortation Tags (151)AHM224Baggage Taken in Error (154)AHM225Baggage Irregularity Report (156)AHM226Tracing Unchecked Baggage and Handling Damage to Checked and UncheckedBaggage (159)AHM230Baggage Theft and Pilferage Prevention (161)AHM231Carriage of Carry-On Baggage (164)AHM232Handling of Security Removed Items (168)AHM240Baggage Codes for Identifying ULD Contents and/or Bulk-Loaded Baggage (169)Chapter3—CARGO/MAIL HANDLING (171)AHM300Chapter3—Record of Revisions (171)AHM310Preparation for Loading of Cargo (172)AHM311Securing of Load (174)AHM312Collection Sacks and Bags (177)AHM320Handling of Damaged Cargo (178)AHM321Handling of Pilfered Cargo (179)AHM322Handling Wet Cargo (180)AHM330Handling Perishable Cargo (182)AHM331Handling and Protection of Valuable Cargo (184)AHM332Handling and Stowage of Live Animals (188)AHM333Handling of Human Remains (190)Table of ContentsPageChapter3—CARGO/MAIL HANDLING(continued)AHM340Acceptance Standards for the Interchange of Transferred Unit Load Devices (191)AHM345Handling of Battery Operated Wheelchairs/Mobility AIDS as Checked Baggage (197)AHM350Mail Handling (199)AHM351Mail Documents (203)AHM353Handling of Found Mail (218)AHM354Handling of Damaged Mail (219)AHM355Mail Security (220)AHM356Mail Safety (221)AHM357Mail Irregularity Message (222)AHM360Company Mail (224)AHM380Aircraft Documents Stowage (225)AHM381Special Load—Notification to Captain(General) (226)AHM382Special Load—Notification to Captain(EDP Format and NOTOC Service) (231)AHM383Special Load—Notification to Captain(EDP NOTOC Summary) (243)AHM384NOTOC Message(NTM) (246)Chapter4—AIRCRAFT HANDLING AND LOADING (251)AHM400Chapter4—Record of Revisions (251)AHM411Provision and Carriage of Loading Accessories (252)AHM420Tagging of Unit Load Devices (253)AHM421Storage of Unit Load Devices (263)AHM422Control of Transferred Unit Load Devices (268)AHM423Unit Load Device Stock Check Message (273)AHM424Unit Load Device Control Message (275)AHM425Continued Airworthiness of Unit Load Devices (279)AHM426ULD Buildup and Breakdown (283)AHM427ULD Transportation (292)AHM430Operating of Aircraft Doors (295)AHM431Aircraft Ground Stability—Tipping (296)AHM440Potable Water Servicing (297)AHM441Aircraft Toilet Servicing (309)Airport Handling ManualPageChapter4—AIRCRAFT HANDLING AND LOADING(continued)AHM450Standardisation of Gravity Forces against which Load must be Restrained (310)AHM451Technical Malfunctions Limiting Load on Aircraft (311)AHM453Handling/Bulk Loading of Heavy Items (312)AHM454Handling and Loading of Big Overhang Items (313)AHM455Non CLS Restrained ULD (316)AHM460Guidelines for Turnround Plan (323)AHM462Safe Operating Practices in Aircraft Handling (324)AHM463Safety Considerations for Aircraft Movement Operations (337)AHM465Foreign Object Damage(FOD)Prevention Program (340)Chapter5—LOAD CONTROL (343)AHM500Chapter5—Record of Revisions (343)AHM501Terms and Definitions (345)AHM503Recommended Requirements for a New Departure Control System (351)AHM504Departure Control System Evaluation Checklist (356)AHM505Designation of Aircraft Holds,Compartments,Bays and Cabin (362)AHM510Handling/Load Information Codes to be Used on Traffic Documents and Messages (368)AHM513Aircraft Structural Loading Limitations (377)AHM514EDP Loading Instruction/Report (388)AHM515Manual Loading Instruction/Report (404)AHM516Manual Loadsheet (416)AHM517EDP Loadsheet (430)AHM518ACARS Transmitted Loadsheet (439)AHM519Balance Calculation Methods (446)AHM520Aircraft Equipped with a CG Targeting System (451)AHM530Weights for Passengers and Baggage (452)AHM531Procedure for Establishing Standard Weights for Passengers and Baggage (453)AHM533Passengers Occupying Crew Seats (459)AHM534Weight Control of Load (460)AHM536Equipment in Compartments Procedure (461)AHM537Ballast (466)Table of ContentsPageChapter5—LOAD CONTROL(continued)AHM540Aircraft Unit Load Device—Weight and Balance Control (467)AHM550Pilot in Command's Approval of the Loadsheet (468)AHM551Last Minute Changes on Loadsheet (469)AHM561Departure Control System,Carrier's Approval Procedures (471)AHM562Semi-Permanent Data Exchange Message(DEM) (473)AHM564Migration from AHM560to AHM565 (480)AHM565EDP Semi-Permanent Data Exchange for New Generation Departure Control Systems (500)AHM570Automated Information Exchange between Check-in and Load Control Systems (602)AHM571Passenger and Baggage Details for Weight and Balance Report(PWR) (608)AHM580Unit Load Device/Bulk Load Weight Statement (613)AHM581Unit Load Device/Bulk Load Weight Signal (615)AHM583Loadmessage (619)AHM587Container/Pallet Distribution Message (623)AHM588Statistical Load Summary (628)AHM590Load Control Procedures and Loading Supervision Responsibilities (631)AHM591Weight and Balance Load Control and Loading Supervision Training and Qualifications (635)Chapter6—MANAGEMENT AND SAFETY (641)AHM600Chapter6—Record of Revisions (641)AHM610Guidelines for a Safety Management System (642)AHM611Airside Personnel:Responsibilities,Training and Qualifications (657)AHM612Airside Performance Evaluation Program (664)AHM615Quality Management System (683)AHM616Human Factors Program (715)AHM619Guidelines for Producing Emergency Response Plan(s) (731)AHM620Guidelines for an Emergency Management System (733)AHM621Security Management (736)AHM633Guidelines for the Handling of Emergencies Requiring the Evacuation of an Aircraft During Ground Handling (743)AHM650Ramp Incident/Accident Reporting (745)AHM652Recommendations for Airside Safety Investigations (750)AHM660Carrier Guidelines for Calculating Aircraft Ground Accident Costs (759)Airport Handling ManualChapter7—AIRCRAFT MOVEMENT CONTROL (761)AHM700Chapter7—Record of Revisions (761)AHM710Standards for Message Formats (762)AHM711Standards for Message Corrections (764)AHM730Codes to be Used in Aircraft Movement and Diversion Messages (765)AHM731Enhanced Reporting on ATFM Delays by the Use of Sub Codes (771)AHM780Aircraft Movement Message (774)AHM781Aircraft Diversion Message (786)AHM782Fuel Monitoring Message (790)AHM783Request Information Message (795)AHM784Gate Message (797)AHM785Aircraft Initiated Movement Message(MVA) (802)AHM790Operational Aircraft Registration(OAR)Message (807)Chapter8—GROUND HANDLING AGREEMENTS (811)AHM800Chapter8—Record of Revisions (811)AHM801Introduction to and Comments on IATA Standard Ground Handling Agreement(SGHA) (812)AHM803Service Level Agreement Example (817)AHM810IATA Standard Ground Handling Agreement (828)AHM811Yellow Pages (871)AHM813Truck Handling (872)AHM815Standard Transportation Documents Service Main Agreement (873)AHM817Standard Training Agreement (887)AHM830Ground Handling Charge Note (891)AHM840Model Agreement for Electronic Data Interchange(EDI) (894)Chapter9—AIRPORT HANDLING GROUND SUPPORT EQUIPMENT SPECIFICATIONS (911)AHM900Chapter9—Record of Revisions (911)AHM901Functional Specifications (914)AHM904Aircraft Servicing Points and System Requirements (915)AIRBUS A300B2320-/B4/C4 (917)A300F4-600/-600C4 (920)A310–200/200C/300 (926)A318 (930)A319 (933)Table of ContentsPageChapter9—AIRPORT HANDLING GROUND SUPPORT EQUIPMENT SPECIFICATIONS(continued) AHM904Aircraft Doors,Servicing Points and System Requirements for the Use of Ground Support Equipment(continued)A320 (936)A321 (940)A330-200F (943)A330-300 (948)A340-200 (951)A340-300 (955)A340-500 (959)A340-600 (962)Airbus350900passenger (965)AIRBUS A380-800/-800F (996)ATR42100/200 (999)ATR72 (1000)AVRO RJ70 (1001)AVRO RJ85 (1002)AVRO RJ100 (1003)B727-200 (1004)B737–200/200C (1008)B737-300,400,-500 (1010)B737-400 (1013)B737-500 (1015)B737-600,-700,-700C (1017)B737-700 (1020)B737-800 (1022)B737-900 (1026)B747–100SF/200C/200F (1028)B747–400/400C (1030)B757–200 (1038)B757–300 (1040)Airport Handling ManualPageChapter9—AIRPORT HANDLING GROUND SUPPORT EQUIPMENT SPECIFICATIONS(continued) AHM904Aircraft Doors,Servicing Points and System Requirements for the Use of Ground Support Equipment(continued)B767—200/200ER (1041)B767—300/300ER (1044)B767—400ER (1048)B777–200/200LR (1051)B777–300/300ER (1055)Boeing787800passenger (1059)BAe ATP(J61) (1067)Bombardier CS100 (1068)Bombardier CS300 (1072)CL-65(CRJ100/200) (1076)DC8–40/50F SERIES (1077)DC8–61/61F (1079)DC8–62/62F (1081)DC8–63/63F (1083)DC9–15/21 (1085)DC9–32 (1086)DC9–41 (1087)DC9–51 (1088)DC10–10/10CF (1089)DC10–30/40,30/40CF (1091)EMBRAER EMB-135Regional Models (1092)EMBRAER EMB-145Regional Models (1094)Embraer170 (1096)Embraer175 (1098)Embraer190 (1100)Embraer195 (1102)FOKKER50(F27Mk050) (1104)FOKKER50(F27Mk0502) (1106)Chapter9—AIRPORT HANDLING GROUND SUPPORT EQUIPMENT SPECIFICATIONS(continued) AHM904Aircraft Doors,Servicing Points and System Requirements for the Use of Ground Support Equipment(continued)FOKKER70(F28Mk0070) (1108)FOKKER100(F28Mk0100) (1110)FOKKER100(F28Mk0100) (1112)IL-76T (1114)MD-11 (1116)MD–80SERIES (1118)SAAB2000 (1119)SAAB SF-340 (1120)TU-204 (1122)AHM905Reference Material for Civil Aircraft Ground Support Equipment (1125)AHM905A Cross Reference of IATA Documents with SAE,CEN,and ISO (1129)AHM909Summary of Unit Load Device Capacity and Dimensions (1131)AHM910Basic Requirements for Aircraft Ground Support Equipment (1132)AHM911Ground Support Equipment Requirements for Compatibility with Aircraft Unit Load Devices (1136)AHM912Standard Forklift Pockets Dimensions and Characteristics for Forkliftable General Support Equipment (1138)AHM913Basic Safety Requirements for Aircraft Ground Support Equipment (1140)AHM914Compatibility of Ground Support Equipment with Aircraft Types (1145)AHM915Standard Controls (1147)AHM916Basic Requirements for Towing Vehicle Interface(HITCH) (1161)AHM917Basic Minimum Preventive Maintenance Program/Schedule (1162)AHM920Functional Specification for Self-Propelled Telescopic Passenger Stairs (1164)AHM920A Functional Specification for Towed Passenger Stairs (1167)AHM921Functional Specification for Boarding/De-Boarding Vehicle for Passengers withReduced Mobility(PRM) (1169)AHM922Basic Requirements for Passenger Boarding Bridge Aircraft Interface (1174)AHM923Functional Specification for Elevating Passenger Transfer Vehicle (1180)AHM924Functional Specification for Heavy Item Lift Platform (1183)AHM925Functional Specification for a Self-Propelled Conveyor-Belt Loader (1184)AHM925A Functional Specification for a Self-Propelled Ground Based in-Plane LoadingSystem for Bulk Cargo (1187)Chapter9—AIRPORT HANDLING GROUND SUPPORT EQUIPMENT SPECIFICATIONS(continued) AHM925B Functional Specification for a Towed Conveyor-Belt Loader (1190)AHM926Functional Specification for Upper Deck Catering Vehicle (1193)AHM927Functional Specification for Main Deck Catering Vehicle (1197)AHM930Functional Specification for an Upper Deck Container/Pallet Loader (1201)AHM931Functional Specification for Lower Deck Container/Pallet Loader (1203)AHM932Functional Specification for a Main Deck Container/Pallet Loader (1206)AHM933Functional Specification of a Powered Extension Platform to Lower Deck/Container/ Pallet Loader (1209)AHM934Functional Specification for a Narrow Body Lower Deck Single Platform Loader (1211)AHM934A Functional Specification for a Single Platform Slave Loader Bed for Lower DeckLoading Operations (1213)AHM936Functional Specification for a Container Loader Transporter (1215)AHM938Functional Specification for a Large Capacity Freighter and Combi Aircraft TailStanchion (1218)AHM939Functional Specification for a Transfer Platform Lift (1220)AHM941Functional Specification for Equipment Used for Establishing the Weight of aULD/BULK Load (1222)AHM942Functional Specification for Storage Equipment Used for Unit Load Devices (1224)AHM950Functional Specification for an Airport Passenger Bus (1225)AHM951Functional Specification for a Crew Transportation Vehicle (1227)AHM953Functional Specifications for a Valuable Cargo Vehicle (1229)AHM954Functional Specification for an Aircraft Washing Machine (1230)AHM955Functional Specification for an Aircraft Nose Gear Towbar Tractor (1232)AHM956Functional Specification for Main Gear Towbarless Tractor (1235)AHM957Functional Specification for Nose Gear Towbarless Tractor (1237)AHM958Functional Specification for an Aircraft Towbar (1240)AHM960Functional Specification for Unit Load Device Transport Vehicle (1242)AHM961Functional Specification for a Roller System for Unit Load Device Transportation on Trucks (1245)AHM962Functional Specification for a Rollerised Platform for the Transportation of Twenty Foot Unit Load Devices that Interfaces with Trucks Equipped to Accept Freight ContainersComplying with ISO668:1988 (1247)AHM963Functional Specification for a Baggage/Cargo Cart (1249)AHM965Functional Specification for a Lower Deck Container Turntable Dolly (1250)AHM966Functional Specification for a Pallet Dolly (1252)Chapter9—AIRPORT HANDLING GROUND SUPPORT EQUIPMENT SPECIFICATIONS(continued) AHM967Functional Specification for a Twenty Foot Unit Load Device Dolly (1254)AHM968Functional Specification for Ramp Equipment Tractors (1256)AHM969Functional Specification for a Pallet/Container Transporter (1257)AHM970Functional Specification for a Self-Propelled Potable Water Vehicle with Rear orFront Servicing (1259)AHM971Functional Specification for a Self-Propelled Lavatory Service Vehicle with Rear orFront Servicing (1262)AHM972Functional Specifications for a Ground Power Unit for Aircraft Electrical System (1265)AHM973Functional Specification for a Towed Aircraft Ground Heater (1269)AHM974Functional Specification for Aircraft Air Conditioning(Cooling)Unit (1272)AHM975Functional Specifications for Self-Propelled Aircraft De-Icing/Anti-Icing Unit (1274)AHM976Functional Specifications for an Air Start Unit (1278)AHM977Functional Specification for a Towed De-Icing/Anti-Icing Unit (1280)AHM978Functional Specification for a Towed Lavatory Service Cart (1283)AHM979Functional Specification for a Towed Boarding/De-Boarding Device for Passengers with Reduced Mobility(PRM)for Commuter-Type Aircraft (1285)AHM980Functional Specification for a Self-Propelled Petrol/Diesel Refueling Vehicle forGround Support Equipment (1287)AHM981Functional Specification for a Towed Potable Water Service Cart (1289)AHM990Guidelines for Preventative Maintenance of Aircraft Towbars (1291)AHM994Criteria for Consideration of the Investment in Ground Support Equipment (1292)AHM995Basic Unit Load Device Handling System Requirements (1296)AHM997Functional Specification for Sub-Freezing Aircraft Air Conditioning Unit (1298)Chapter10—ENVIRONMENTAL SPECIFICATIONS FOR GROUND HANDLING OPERATIONS (1301)AHM1000Chapter10—Record of Revisions (1301)AHM1001Environmental Specifications for Ground Handling Operations (1302)AHM1002Environmental Impact on the Use of Ground Support Equipment (1303)AHM1003GSE Environmental Quality Audit (1305)AHM1004Guidelines for Calculating GSE Exhaust Emissions (1307)AHM1005Guidelines for an Environmental Management System (1308)Chapter11—GROUND OPERATIONS TRAINING PROGRAM (1311)AHM1100Chapter11—Record of Revisions (1311)AHM1110Ground Operations Training Program (1312)Appendix A—References (1347)Appendix B—Glossary (1379)Alphabetical List of AHM Titles (1387)IATA Strategic Partners..............................................................................................................................SP–1。
D1226宁波联众LF金点子大赛
预热方案
预热方案
活动时间:上市前一个月。
活动地点:展厅门口和银泰城
(展厅门口:吸引来店客流,斯柯达客流,大众客 流)
(银泰城:人流量集中,地标性购物城)
预热方案
主题:
以“猜”为预热主题, 设置悬念,悬念结果 是索九产品的大亮点 之一。从而既增加了 关注度,又让产品卖 点让客户铭记
预热方案
目标人群
阿拉宁波网首页通栏
预热方案
活动费用:
序号 1 2 3 4 5
物品 竞猜物(产品卖点相关) 竞猜宝箱X2 竞猜礼品 广宣费用
银泰场地租赁(1个月)
费用
3000元 200元/个 55000元 暂未定
上市方案
上市方案
主题:
揭秘
揭开预热活动 “宝箱”的秘
密
揭开公布索九 车型价格以及
卖点
上市方案
地点:宁波联众展厅 时间:宁波区域上市后 第一个周末
D级车市场从来不乏有能者。近年 来,以美系,德系车为代表的涡轮 增压车型牢牢占据着D级车的市场
。北京现代以2.0流体雕塑自 成一派,此次搭载涡轮增压的动力 总成,兼顾外形,动力,无疑成为 欧美车型市场中的一个极富竞争力
的“搅局者”。
营销方案
时间 地点
上市会后,持续两个月,每个周末以及周 五晚上
北仑区,镇海区及周边人流量密集区域 (CBD商务中心,大型综合广场,中高端社 区附近,娱乐场所等)
北京现代其他车型 客户
上市方案
上市活动内容:
1,播放开场视频 2,主持人开场白 3,开场沙画表演(演艺索纳塔演变史) 4,预热期的竞猜揭晓,并中奖客户发奖品。 5,视频过渡,引出索九 6,灯光关闭,索九启动驶向舞台,音乐效果为汽车排 气声浪以及漂移声音。 7,主持人上台,邀请总经理公布索九价格 8,销售经理介绍阐述索九。 9,泡泡舞表演。(此类表演容易利用观众自媒体) 10,自由赏车洽谈,自助餐点,拉斯维加斯赌博游戏赢 礼品(与索九合影并发送微信微博等即多送一组筹码)。 11,活动结束。
PWD22用户指南
天气现象传感器PWD22用户指南目录第一章概述 (6)操作手册介绍 (6)安全说明 (6)ESD 静电放电保护 (7)第二章产品总体介绍 (8)维萨拉能见度传感器 PWD10/20 (8)硬件结构 (8)使用 PWD10/20 (9)产品专有名词 (10)第三章功能描述 (11)光学测量 (11)光路 (11)维萨拉发射机单元 PWT11 (12)光接受机 (13)背景亮度传感器 PWL111 (可选) (13)BLSC 命令 (14)连续模式 (14)昼/夜/转换模式 (14)取消 PWL111 (14)BCAL 命令 (15)温度传感器 (15)运算方法 (15)能见度 (15)内部监测 (16)内置检测 (16)存储检测 (17)信号监测 (17)硬件监测 (18)污染监测 (18)第四章安装 (19)选择安装方位 (19)接地和防雷电保护 (20)设备接地 (20)内部接地 (21)远程单元和通讯电缆接地 (21)安装程序 (21)卸货和开箱 (21)存放 (22)固定 (22)连接 (23)电缆连接 (23)基本接线 (24)PWD10/20供电电源 (25)无PWL111(缺省)内部加热器 (26)无 PWL111 (可选) 内部加热器 (26)Hood 加热器PWH111 (26)通信选项 (26)串行通信设置 (27)串行 RS-232 (27)串行多点传输 RS-485 (27)维护终端的连接 (27)继电控制 (28)继电器命令 (30)初始设置 (31)开机验证 (32)第五章操作 (33)总述 ................................................................ 错误!未定义书签。
操作说明 (33)进入/退出命令模式 .................................... 错误!未定义书签。
OPEN命令 (34)CLOSE命令 (35)信息类型 (35)Message 0 (36)Message 1 (37)Message 2 (37)Message 3 (37)Message 4 (38)Messages 5 and 6 (38)Message 7 (38)自动信息发送 (39)信息查询 (39)命令列表 (41)PWD10/20 命令 (41)HELP帮助 (41)MES (42)AMES (42)系统配置命令 (42)PAR (42)CONF (43)Hood Heaters加热器 (47)BAUD波特 (47)模拟输出 (47)模拟输出模式 (49)Mode 0 (49)Mode 1 (49)Mode 2 (50)Mode 3 (51)Mode 4 (51)模拟输出标定 (51)维护命令 (52)STA (53)CAL (54)CLEAN (55)ZERO (55)CHEC (56)HEAT (56)其它命令 (57)TIME (57)DATE (57)RESET (58)VER (58)第六章维护 (59)周期性维护 (59)清洁 (60)清洁镜头和护罩 (60)标定 (61)能见度标定 (61)标定检查程序 (61)标定程序 (62)拆卸和更换 (63)拆卸和更换光学单元 (63)拆卸发射机 PWT11 (63)拆卸PWC10/20 (65)第七章故障排除 (66)常见问题 (66)信息指示警告或者报警 (66)信息缺失 (66)有信息无能见度值 (67)能见度值持续过好 (68)能见度值持续过差 (68)PWD10/20 电气故障 (68)第八章技术数据 (70)技术参数 (70)Mechanical Specifications (70)Electrical Specifications (71)Optical Specifications (71)Visibility Measurement Specifications (72)Environmental Specifications (72)APPENDIX A内部监控值 (74)APPENDIX BPWC10/20 连接器和跳线器设置 (78)第一章概述操作手册介绍本说明书提供了能见度传感器PWD10/20的安装、操作和维护的有关信息。
考生姓名代码在线查询
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草 谷 公 司 在 I C2 1 发 布 了 E US最 新 版 本 60 E US B 0 0上 DI ,。 DI
6支 持所 有视 频格 式 ,包括 1 8 p 06 0 0 5 /0和 4 K数字 电影 格式 ,采 用业内速度最快的 A VCHD编辑格 式,同日支 持所有 业内主流编解 寸 码格式。EDIS 6可 数字 SL U R摄 像机 拍摄的视 频内容 进行编辑。 EDI US 6的用户可 采用来自 SDI 基带视频的代理 服务器素材 。编 辑人员可将任何摄 录一体机的代理服务 器与 EDI US代理服务器在
大连地铁七号线工程
3.1 环境空气质量.......................................................................................................... 24
4 环境影响预测与评价 ..................................................................................................... 27
4.1 声环境影响预测与评价.......................................................................................... 27 4.1.1 声环境影响预测与分析...................................................................................... 27 4.1.2 声环境保护措施.................................................................................................. 28
2.3 环境保护目标...........................................................................................................11 2.3.1 声和大气环境保护目标.......................................................................................11 2.3.2 振动环境保护目标.............................................................................................. 14 2.3.3 生态环境保护目标.............................................................................................. 24
SPD-M20A说明书
第 1 章 配置
1.1 概述 ..................................................................................................................1-2 1.2 特性 ..................................................................................................................1-2 1.3 组成部件 ...........................................................................................................1-4 1.4 操作所需的物品 ................................................................................................1-5
! 可选的流通池 ............................................................................................................ 1-6 ! 其他选件 .................................................................................................................... 1-7
野战“敢死队”
野战“敢死队”作者:王博来源:《汽车与运动》2007年第07期本栏目从未介绍过越野游戏,本期我们推荐5大系列作品,车迷朋友可上网用中英文搜索下载,再结合本刊关于中国越野赛事的报道,希望您把这项车赛看出门道儿。
以下,我们采用类似NBA“五佳球”的形式,逐一拆解下列作品。
第5名:《巴黎-达喀尔》1代、2代(Paris Dakar Rally)出品年代:1代/2001年、2代/2002年国内曾有公司在2002年引进1代,花大把钞票购买了“巴黎一达喀尔”的官方授权。
但是游戏品质实属一般,赛车过弯的物理计算太简单,车头转向角速度取决于赛车过弯速度,车速越快,转向越慢车速越慢。
转向越快,这属于十几年前的古董算法,老掉牙!好在游戏中的车型比较丰富,包括四驱越野车、两轮越野摩托、四轮ATV车和大卡车共计四大车系。
赛段距离比较短,一个赛段大致耗时5—10分钟,新手觉得轻松,老手不大过瘾。
如果程序员将场景数据设为随机,游戏就能自动生成无数沙丘,玩家一口气跑完800km马拉松赛段,那该多爽,遗憾的是,2代游戏并未增加这个功能,而且游戏平台从1代PC转为2代PS2,玩家必须购买PS2游戏机才能玩到2代,限制了它的普及。
真实的达喀尔拉力赛举世无双,不过达喀尔赛车游戏实属一般。
第4名:《4驱进化》1代、2代、(4×4Evo)出品年代:1代/2001年、2代/2002年游戏1代和2代的间隔时间只有1年,2代画面和音效比1代略有进步,但物理完全相同。
两代作品都表现出严重转向不足,你必须一边踩足油门、一边拉动手刹,一边快打方向,听到轮胎发出“嘎嘎”摩擦声,车身才开始飘移过弯,很累,建议车迷朋友下载2代,它模拟福特、通用,丰田、日产、本田、奔驰克莱斯勒等几乎所有品牌的越野车,可作为越野车资料库。
1代和2代都采用户外越野赛道。
这比体育场越野赛道更开阔,但容易迷路,而且每个计时点设有“龙门架”,赛车必须从中间穿过,否则成绩无效。
CX600产品描述
产品描述
文档版本 03 发布日期 2012-06-08
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HUAWEI CX600 综合业务承载路由器 产品描述
目录
假面骑士营销策划方案
假面骑士营销策划方案一、背景分析假面骑士(Kamen Rider)是日本著名的特摄剧系列,由石森章太郎创作,以“假面战队”为主题,每一季带领不同的特摄英雄与邪恶势力战斗。
自1971年首播以来,假面骑士系列一直深受年轻观众的喜爱,并积累了庞大且忠实的粉丝群体。
从最初的“仮面ライダー”到后来的“仮面ライダージオウ”,假面骑士已经成为日本特摄剧的代表作之一。
在中国,假面骑士曾经在上世纪90年代引起一股风潮,无论是《奧特曼力量36计》还是《假面骑士黑RX》,都深入人心。
随着中国市场的发展以及特摄剧在中国的受众群体不断壮大,将假面骑士引进中国市场,并进行有效的营销策划,不仅可以满足粉丝的需求,也有望在中国市场取得成功。
二、目标市场分析1. 目标群体目标群体主要包括以下几个方面:(1)特摄剧的忠实粉丝:主要是80后和90后,他们在童年时期热衷于特摄剧,对假面骑士系列有着深厚的情感基础,具有较高的忠诚度。
(2)新一代年轻观众:随着中国特摄剧市场的发展,越来越多的年轻观众对特摄剧产生了兴趣。
这一群体具有较强的消费能力和消费意愿,对于新奇、创新的内容和产品有着很高的接受度。
2. 市场需求基于目标群体的特点以及对特摄剧的兴趣和需求,市场需求主要集中在以下几个方面:(1)官方授权正版商品:粉丝群体对于官方授权的正版商品具有较高的购买意愿,如假面骑士周边产品、玩具、服装等。
(2)线下互动活动:粉丝群体希望能够与假面骑士进行近距离的互动,参与相应的线下活动,如粉丝见面会、动漫展等。
(3)视频游戏和手机游戏:粉丝群体对于与假面骑士相关的游戏有较高的兴趣,这既能满足他们对假面骑士的需求,也能提供一种与偶像互动的方式。
三、营销策略1. 宣传推广(1)社交媒体营销:通过微博、微信公众号等社交媒体平台,定期发布假面骑士的最新消息、剧集预告、粉丝互动等,吸引目标群体的关注和参与,提高品牌知名度。
(2)明星代言:邀请当红明星或网红进行假面骑士形象代言,并通过线上线下的宣传推广来提高品牌曝光度。
四驱车活动策划方案
四驱车活动策划方案一、活动背景四驱车(Four-wheel drive vehicle)是指车辆具备四个驱动轮,并能通过驱动系统实现四个轮子同时驱动。
四驱车拥有强大的动力和出色的越野性能,适合在各种恶劣路况下行驶,因此一直以来都受到越野爱好者的喜爱。
四驱车活动是一种基于四驱车的户外运动活动,为参与者提供了与自然亲密接触、挑战自我、释放压力的机会。
其丰富多彩的活动形式吸引了越来越多的人参与和关注。
本文将对四驱车活动进行详细的策划方案。
二、目标群体1. 越野爱好者:对于越野运动感兴趣,乐于挑战自我,喜欢与自然亲近的人群。
2. 车迷群体:热爱汽车,对四驱车有着浓厚的兴趣,希望亲身体验四驱车的驾驶乐趣。
3. 广大市民:希望通过参与四驱车活动,接触自然、放松心情的人群。
三、活动目标1. 提供参与者良好的户外活动环境,感受四驱车的驾驶乐趣和自然的美妙。
2. 增进越野爱好者的交流与合作,促进越野文化的传承和发展。
3. 宣传和推广四驱车文化,提高四驱车的知名度和市场份额。
四、活动形式1. 越野考验:设立不同难度的越野赛道,组织参与者驾驶四驱车在恶劣的路况下进行比赛。
通过赛道的设计和设置,考察参与者的驾驶技巧和应变能力。
2. 越野拉力赛:模拟真实的拉力赛形式,组织四驱车车手们在规定的路段和时间内完成比赛任务。
赛道设置复杂多样,要求车手具备高度的技术性和团队合作精神。
3. 越野户外拓展:组织参与者驾驶四驱车深入自然,进行拓展训练,挑战自我。
通过开展多种拓展项目,引导参与者发现自身潜能,拓展潜能,提升团队协作能力。
4. 越野趣味竞技:设计多种有趣的竞技项目,如越野考验、车辆徒手搬运、车辆装备快速拆装等,让参与者在竞技中感受到四驱车的魅力。
五、活动流程活动时间:两天一夜。
第一天:- 上午:参与者到达活动现场,进行签到和安全顶峰活动培训。
- 下午:开展越野考验项目,评选出最佳驾驶者和最佳车队。
- 傍晚:进行开幕式和欢迎晚宴,为参与者们提供交流和放松的机会。
赛车线下比赛方案策划书3篇
赛车线下比赛方案策划书3篇篇一《赛车线下比赛方案策划书》一、活动背景随着赛车运动的日益普及和受欢迎程度的不断提高,我们计划举办一场精彩的赛车线下比赛,为赛车爱好者提供一个展示实力和交流的平台,同时也吸引更多人关注和参与到赛车运动中来。
二、活动目的1. 提供一个高水平的赛车竞技平台,让选手们能够充分展示自己的驾驶技术和赛车性能。
2. 增强赛车爱好者之间的交流与合作,促进赛车文化的传播和发展。
3. 吸引更多观众参与,提高赛车运动的影响力和知名度。
三、比赛时间和地点时间:[具体日期]地点:[详细比赛场地]四、参赛资格1. 持有有效的赛车驾驶证。
2. 符合比赛车辆的相关规定和要求。
五、比赛规则1. 采用国际通用的赛车比赛规则,包括起跑、超车、进站等环节。
2. 比赛分为多个回合,根据累计成绩确定最终名次。
3. 严格遵守安全规定,确保选手和观众的安全。
六、比赛车辆1. 参赛车辆必须符合比赛规则和安全标准。
2. 车辆可以由选手自行准备或由主办方提供租赁服务。
七、活动流程1. 报名阶段:选手在规定时间内提交报名材料。
2. 赛前培训:对参赛选手进行安全培训和比赛规则讲解。
3. 车辆检查:对参赛车辆进行严格检查,确保符合比赛要求。
4. 比赛阶段:开幕式:介绍嘉宾、选手和比赛规则。
排位赛:确定选手的起跑顺序。
正赛:进行多回合的激烈比赛。
颁奖典礼:为获奖选手颁发奖杯和奖品。
5. 赛后活动:组织选手和观众进行交流互动。
八、宣传推广1. 通过社交媒体、赛车论坛等渠道进行广泛宣传。
2. 邀请知名赛车手和媒体参与,提高活动的影响力。
3. 制作宣传海报、视频等资料,在比赛场地和周边地区进行宣传。
九、奖项设置1. 设立冠、亚、季军奖项,以及其他单项奖项,如最佳车手奖、最快圈速奖等。
2. 为获奖选手提供丰厚的奖品和奖金。
十、安全保障1. 配备专业的医疗急救团队和设备,确保在紧急情况下能够及时进行救援。
2. 设立安全警示标识和防护设施,保障比赛现场的安全。
急难先锋4:全球行动——所有应急车辆图文一览
Canadair (救火飞机) 费用:4000 速度:160 公里/时 空间:0 装备:无 用途:扑灭大片火灾(比如山林火灾)
Troop Carrier - MTW (警用运输车) 费用:500 速度:100 公里/时 空间:6 & 4个嫌犯位置 装备:钉带路障 用途:搭载大量警方人员,押送大量嫌犯
Police helicopter - PHC (警用直升机) 费用:3000 速度:180 公里/时 空间:2 & 1个嫌犯位置 装备:无 用途:快速警用侦查单位
A B C - D e c o n t a m i n a t i o n Ve h i c l e ( H A Z M AT ) - D e k o n - P ( 防 化 消 防 车) 费用:2500 速度:70 公里/时 空间:3 & 2个受污染人员位置 装备:无 用途:清洁受污染人员
Crane - FGRR (工程救援吊车) 费用:2000 速度:60 公里/时 空间:0 装备:无 用途:起吊汽车或其他重型障碍物
TEC Helicopter - FGRT (工程救援直升机) 费用:3000 速度:200 公里/时 空间:1 & 1个伤员担架 & 4个被救助者位置 装备:无 用途:索降工程人员,营救位于屋顶和高处以及无法地面抵达区域的 人员
A r m o r e d P u m p e r ቤተ መጻሕፍቲ ባይዱe h i c l e - L P F ( 装 甲 消 防 车 ) 费用:3000
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节目来源梗概
制作团队—作人、导演个人简述
晁若闻
台湾金牌电视 制作人、导演
以积极却平和的态度对待工作、生活、以及身边的人 ,爱工作,爱生活,也爱身边的每一个人
2014年至今 江苏卫视《最强大脑》导演 2014年至今 上海东方卫视《中国梦之声》导演 2014年至今 上海东方卫视《生活大爆笑》导演 2013年至今 江苏卫视《最强大脑》导演 2014年至今 北京卫视《梦想合伙人》导演 2014年至今 第一财经《梦想下一战》导演 2014年 中央电视台《出彩中国人》导演 2013年至今 上海东方卫视《不朽名曲》导演 2014年 上海东方卫视《笑傲江湖》导演 2014年 上海东方卫视《妈妈咪呀》导演 2013年 上海东方卫视《妈妈咪呀》导演 2012年 上海东方卫视《妈妈咪呀》导演 2011年至2012年 南京快视动漫科技有限公司(快TV)艺术总监 、导演
饥饿游戏vs 斯巴鲁合作方案
饥饿游戏 vs 斯巴鲁 合作方案
中国好味道
New Places New Lives
节目来源介绍:韩国《无限挑战》
《饥饿游戏》 是结合了韩国真人秀《无限挑战》的精华所演变而来。《无限挑战》是由韩国 MBC制作及播出的真人秀综艺节目,由2005年4月23日开始播出。节目原本是综艺时段《星期 六》内的其中一个环节,经过多次节目改革,最终在2006年5月6日以韩国电视史上第一个“真 实综艺节目”独立呈现,以每周不同主题和形式独立制作,《无限挑战》名称由当时沿用至今, 是韩国十几年经久不衰的冠军综艺节目。
哈哈绝对小孩》、《贝婴美母爱总动员》、《娱乐财富》 节目总导演、策划 《爽食赢天下》节目策划 江苏卫视:
《统一南航新空姐》节目总导演 《2010名师高徒》视觉导演 CCTV: 《三星智力快车》《全家总动员》节目总导演
谢涤葵,现为《爸爸去哪儿》栏目总制片人兼总导演。 1996年武汉大学新闻系毕业,先后在《新闻汇报》、《湖 南新闻联播》担任编辑、记者
节东目东方来方源卫卫梗视视概优的势平台优势
“三高人群”收视率为全国省级卫视频道第四名
Ø东方卫视 定位“高端、时尚”,近年来”三高人群”收视率以大幅优势稳居全 国省级卫视频道第四名;
Ø东方卫视平均到达率与忠实率双高最均衡,有利于各大品牌进行广告投放。
各大卫视热门综艺节目档期比较(7月-10月)
同期,周末档综艺节目:
节目梗概:
《无限挑战》是由韩国MBC制作及播出的真人秀综 艺节目,由2005年4月23日开始播出。节目原本是 综艺时段《星期六》内的其中一个环节,经过多次 节目改革,最终在2006年5月6日以韩国电视史上 第一个“真实综艺节目”独立呈现,以每周不同主 题和形式独立制作,《无限挑战》名称由当时沿用 至今。现是MBC星期六黄金时段综艺中的第二线综 艺,每期设定不同主题,艺人完成节目组设定任务。
刘在石个人简介:
刘在石 韩国主持人、搞笑艺人。1972年8月14日出生于韩 国首尔特别市。1991年考入首尔艺术大学放送演艺系,于 KBS第一届大学喜剧节出道。2001年开始主持综艺节目。凭 借2003年-2007年主持的SBS《X-Man》和2005年起主持 的MBC《无限挑战》获得了高度评价,被誉为“国民MC” 。
同期,中国好声音7、8月在 浙江卫视开播,爸爸去哪儿第 三季9月在湖南卫视开播ห้องสมุดไป่ตู้均 是周五。
不同平台,不同时间段
“周间档”真人秀节目 没有竞争对手
英翼介绍
上海英翼文化传播有限公司
WING Capital Investment Management
上海英翼文化传播有限公司(以下简称“英翼传媒”)成立于2007年10
1998年湖南卫视创办《晚间新闻》,开始担任该栏目记者 和责任编辑,在此期间,他采写的多篇新闻获得省级各种 奖励,并于2003年担任《晚间新闻》栏目制片人。
2006年策划推出的《洞穴之光》系列节目。期间,更是多 次获得十佳制片人等称号,并荣立湖南广播电视台二等功 一次,荣立三等功多次。第十一届湖南省十佳新闻工作者。
东方卫视: 2006-2008年《我型我秀》节目总导演 2006-2009年《梦圆东方倒计时》《春满东方除夕特别节目》
晚会总导演 2009年《魔法天裁》第二季策划、节目导演 2011年《我心唱响》节目总导演
浙江卫视: 2012年《中国好声音》现场总导演 2011-2012年《中国梦想秀》节目总导演、策划 2012年《越跳越美丽》节目总导演 2011年 ELITE模特大赛真人秀《卧底超模》节目总导演 2012年 雪弗兰 《开心大买卖》、《大红鹰天生我才》、《哇
播出平台
节目名称
湖南卫视 《爸爸去哪儿》第三季
预计播出时间 2015年7月起
2015年,各类明星真人秀
将愈演愈烈,一场没有硝 烟的荧屏大战蓄势待发!
浙江卫视 《中国好声音》第四季 《奔跑吧兄弟》第二季
东方卫视 《花样爷爷》第二季 江苏卫视 《花样年华》第二季
2015年7月起 2015年10月起
2015年6月起 2015年5月起
人在饥饿状态下会激发出怎样的生理本能?
为了证明自己是站在食物链顶端的王者,赌上生命和荣誉的 美食大作战! 是掠食者还是猎物?男神女神组成的美食战队,十三周绕着 美国跑,追寻舌尖上好滋味的终极奥义!展开一场激烈的
月,是一家专业的多媒体内容提供商,致力于为强势媒体平台量身定制品牌节 目,并提供频道运营战略规划、视觉形象创意、推广传播执行以及跨媒体新业 务延伸等服务。
成功运作的节目:
1.
金星脱口秀- 金星撞火星(星空卫视)
2.
中国好声音之酷我真声音(浙江卫视)
3.
梦想合伙人(北京卫视)
4.
梦想下一战(第一财经频道)
5.
股市天天向上(宁夏卫视、第一财经频道)
6.
职场好榜样等(宁夏卫视、第一财经频道)
制作人、导演个人简述
曹申君
台湾金牌电视 制作人、导演
知名节目导演,超过二十年的导演从业经历,创造过无 数个收视佳绩,理性思维缜密,兼具感性色彩,其创意 的节目具有难以言说的平衡之美。认为目不暇接的媒体 主发要展作,品为影视制作提出了新的机遇和挑战