SAE AMS 4979F-2008
AMS磁编码器产品简介完整版前期
绝对编码器
• 绝对编码器是直接输出数字量的传感器,在它的圆形码盘上沿径向有 若干同心码道,每条道上由透光和不透光的扇形区相间组成,相邻码 道的扇区数目是双倍关系,码盘上的码道数就是它的二进制数码的位 数,在码盘的一侧是光源,另一侧对应每一码道有一光敏元件;当码 盘处于不同位置时,各光敏元件根据受光照与否转换出相应的电平信 号,形成二进制数。这种编码器的特点是不要计数器,在转轴的任意 位置都可 读出一个固定的与位置相对应的数字码。显然,码道越多, 分辨率就越高,对于一个具有 N位二进制分辨率的编码器,其码盘必 须有N条码道。 • 绝对式编码器是利用自然二进制或循环二进制(格雷码)方式进行光 电转换的。绝对式编码器与增量式编码器不同之处在于圆盘上透光、 不透光的线条图形,绝对编码器可有若干编码,根据读出码盘上的编 码,检测绝对位置。编码的设计可采用二进制码、循环码、二进制补 码等。它的特点是: • 可以直接读出角度坐标的绝对值、没有累积误差、电源切除后位置信 息不会丢失。 • 但是分辨率是由二进制的位数来决定的,也就是说精度取决于位数, 目前有10位、14位等多种。
AMS磁编码器产品名词解释及实用公式
名词解释
• 分辨率:
指的是磁编码器每圈的步长数。(如10位磁编 码器AS5040,其分辨率为0.35o,即每圈1024个位 置) • A/B正交两路及Index输出: A、B两路相位差90o脉冲信号,通过通道A的相 位超前通道B或通道B的相位超前通道A便可方便地 判断出旋转方向,每圈A/B各路输出的脉冲数为磁 编码数每圈步长数/4;Index指示绝对值零位,每 经过零点将产生一个脉冲。
增量式编码器
• 增量式编码器是直接利用光电转换原理输出三组 方波脉冲A、B和Z相;A、B两组脉冲相位差90o, 通过通道A的相位超前通道B或通道B的相位超前通 道A便可方便地判断出旋转方向;Z相为每转一个 脉冲,用于基准点定位。 • 优点:原理构造简单,机械平均寿命可在几万小 时以上,抗干扰能力强,可靠性高,适合于长距 离传输。 • 缺点:无法输出轴转动的绝对位置信息。
EMI产品手册08版
目录交流单相通用滤波器 (2)交流单相高性能滤波器 (5)交流单相超高性能滤波器 (7)交流三相三线滤波器 (10)交流三相四线滤波器 (12)变频器输入端专用型滤波器 (14)变频器输出端专用型滤波器 (16)直流滤波器 (18)PCB交流插针型滤波器 (21)IEC标准插座形滤波器 (22)军用交流单相高性能滤波器 (24)军用交流三相滤波器 (27)军用直流滤波器 (30)屏蔽室电源滤波器双线系列 (33)屏蔽室电源滤波器单线系列 (34)电快速瞬变脉冲群抑制器 (36)浪涌抑制器 (37)滤波器基础知识介绍 (39)产品特点▲ 对差模和共模干扰具有良好的抑制特性。
▲ 泄漏电流小。
▲ 体积小,重量轻,性能可靠、价格低廉。
Features▲ General purpose filters with a good suppression tocommon-mode and differential-mode interference.▲ Lower leakage current.▲ Compact, light weight, reliable and low cost技术指标额定电压Rated V oltage 115/250V AC 额定电流Rated Current 3A—300A 工作频率Operating Frequency 50/60Hz 耐压测试(一分钟) 1450VDC (line/line ) Test V oltage (1min ) 1500V AC (line/ground ) 泄漏电流Leakage Current : <0.5mA(250V AC/50Hz) 温度范围Temperature Range -25℃/+85℃ 端接方式Connections应用场合开关电源、UPS 电源、医疗设备、仪器仪表等电力电子设备。
ApplicationSwitching-mode power supply ,UPS ,medical equipments and electronic instruments etc. 电路原理图Electrical Schematics【 A 】 【 B 】插入损耗(dB ) 共模/差模 (CM/DM )额定 电流 外形尺寸原理 电路 测试频率(MHz)型 号 (A) 图号图号 06 07 080.010.050.100.150.5 1.0 5.0 10 20 30F-FAB1-03-?? 3 B1 A 0811/523/1029/1532/1937/2941/3649/53 52/55 55/5450/52F-FAB1-06-?? 6 B1 A 085/4 13/919/1522/1831/2835/3349/55 52/57 56/5658/52F-FAB2-03-?? 3 B2 A 0811/523/1029/1532/1937/2941/3649/53 52/55 55/5450/52F-FAB2-06-?? 6 B2 A 085/4 13/919/1522/1831/2835/3349/55 52/57 56/5658/52F-LAB1-02-?? 2 B1 A 0821/728/1530/2031/2136/5342/5357/63 69/69 62/6862/68F-LAB1-03-?? 3 B1 A 0818/625/1527/1929/2133/4839/5053/63 63/69 69/6568/68F-LAB2-02-?? 2 B2 A 0821/728/1530/2031/2136/5342/5357/63 69/69 62/6862/68F-LAB2-03-?? 3 B2 A 0818/625/1527/1929/2133/4839/5053/63 63/69 69/6568/68F-FAC1-03-?? 3 C1 A 07 0816/629/1135/1639/1945/3147/4352/51 53/55 52/5652/56交流单相通用型滤波器General Purpose Filters交流单相通用滤波器参数表General Purpose Filter Parameter ListFTF EMI电源滤波器插入损耗(dB)共模/差模(CM/DM)测试频率(MHz)型号额定电流(A)外形尺寸图号原理电路类型06 07 080.010.050.100.150.5 1.0 5.0 10 20 30 F-FAC1-06-?? 6 C1 A 07 085/4 13/919/1522/1831/2835/3349/55 52/57 56/5658/52 F-FAC2-03-?? 3 C2 A 07 0816/629/1135/1639/1945/3147/4352/51 53/55 52/5652/56 F-FAC2-06-?? 6 C2 A 07 085/4 13/919/1522/1831/2835/3349/55 52/57 56/5658/52 F-LAC1-03-?? 3 C1 A 07 0826/637/1038/1641/1945/3050/4057/63 60/60 58/6055/62 F-LAC1-06-?? 6 C1 A 07 0820/630/1132/1634/1938/2942/3646/55 50/53 52/5452/58 F-LAC2-03-?? 3 C2 A 07 0826/637/1038/1641/1945/3050/4057/63 60/60 58/6055/62 F-LAC2-06-?? 6 C2 A 07 0820/630/1132/1634/1938/2942/3646/55 50/53 52/5452/58 F-FBD1-06-?? 6 D1 B 06 07 11/723/1830/2132/2237/5042/5353/63 53/63 68/6562/68 F-FBD1-10-?? 10 D1 B 06 07 4/5 16/1722/2124/2530/4434/4746/53 53/63 68/6562/64 F-FBD2-06-?? 6 D2 B 06 07 11/723/1830/2132/2237/5042/5353/63 53/63 68/6562/68 F-FBD2-10-?? 10 D2 B 06 07 4/5 16/1722/2124/2530/4434/4746/53 53/63 68/6562/64 F-LBD1-06-?? 6 D1 B 06 07 21/833/1836/2438/2542/5647/5859/69 59/63 68/6062/65 F-LBD1-10-?? 10 D1 B 06 07 20/825/1928/2429/2533/4738/5053/59 57/63 62/6362/65 F-LBE2-15-?? 15 E2 B 06 07 20/825/1928/2429/2533/4738/5053/59 57/63 62/6362/65 F-LBE2-20-?? 20 E2 B 06 07 20/825/1928/2429/2533/4738/5053/59 57/63 62/6362/65 F-FBE2-30-?? 30 E2 B 06 07 3/8 13/2018/2520/2525/3528/3740/45 43/51 50/5362/66 F-LBE2-30-?? 30 E2 B 06 07 10/815/1918/2020/3123/4230/4350/57 57/63 68/6870/70 F-FBF2-40-?? 40 F2 B 06 3/8 13/2018/2520/2525/3528/3740/45 43/51 50/5362/66 F-LBF2-40-?? 40 F2 B 06 10/815/1918/2020/3123/4230/4350/57 57/63 68/6870/70 F-FBG2-60-?? 60 G2 B 06 3/8 13/2018/2520/2525/3528/3740/45 43/51 50/5362/66 F-LBG2-60-?? 60 G2 B 06 10/815/1918/2020/3123/4230/4350/57 57/63 68/6870/70 F-FBH2-100-?? 100 H2 B 06 3/8 13/2018/2520/2525/3528/3740/45 43/51 50/5362/66 F-LBH2-100-?? 100 H2 B 06 10/815/1918/2020/3123/4230/4350/57 57/63 68/6870/70 F-FBH2-150-?? 150 H2 B 06 3/8 13/2018/2520/2525/3528/3740/45 43/51 50/5362/66 F-LBH2-150-?? 150 H2 B 06 10/815/1918/2020/3123/4230/4350/57 57/63 68/6870/70 F-LBZ2-300-?? 300 Z2 B 06 10/815/1918/2020/3123/4230/4350/57 57/63 68/6870/70 F-LBP1-10-?? 10 P1 B 06 07 23/828/1930/2231/2436/5041/6060/64 63/69 68/7068/68 F-LBP1-20-?? 20 P1 B 06 07 18/825/1826/2328/2632/4738/5053/63 60/68 68/7062/62 F-FAM1-03-?? 3 M1 A 06 07 0811/523/1029/1532/1937/2941/3649/53 52/55 55/5450/52【图B1】【图B2】【图C1】【图C2】外形尺寸交流单相通用滤波器参数表General Purpose Filter Parameter List【图D1】 【图E2】 【图F2】【图G2】 【图H2】【图Z2】 【图P1】68【图M1】外形尺寸产品特点▲双级共模、一级共模一级差模滤波电路,具有良好的共模和差模干扰抑制特性。
SAE AS 403A-2008失速告警器
SAE AS403A 失速告警器免责声明翻译稿忠实原文,准确反映原文内容。
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特此声明。
中国航空综合技术研究所二〇一九《国际自动机工程师学会(SAE )技术标准委员会章程》规定:“本报告由SAE 发布,用以促进技术与工程科学的发展水平。
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国际自动机工程师学会2008年版权所有保留所有权利。
未获SAE 的书面许可前,不允许该出版物的任何部分被复制、存储于检索系统或被以任何形式任何途径,电子、手抄、照片、录音或其他方式等传播。
订购方式: 电话: 877-606-7323(美国和加拿大境内)电话: 724-776-4970(美国境外) 传真: 724-776-0790 邮箱: CustomerService@SAE 网址: 航空航天标准AS403A失速告警器发布日期: 1952-10 修订日期: 1958-07 非现行有效: 1993-05 再次确定非现行有效: 2008-021. 目的:本标准为飞机失速告警器规定了最低要求,失速告警器应能在3.3节规定的环境条件下工作。
2. 范围:A )本标准认为失速是在飞行中由机翼周围气流产生的升力不足以保持或控制飞机飞行的状态。
B )本标准有两类失速告警传感器,都是用来向飞行员指示飞机即将失速用的。
I 类——单点类传感器。
II 类——连续类传感器。
3. 一般要求 3.1 材料和制造工艺3.1.1 材料:材料质量应可靠,且通过使用经验或试验证明其适用于飞机仪表。
3.1.2 制造工艺:制造工艺应符合高级飞机仪表制造规范。
3.2 标记:下列信息应清晰持久地标记或贴在仪表上:(a) 仪表名称(b) AS403A ,类型(I 类或II 类) (c) 额定值(电气、真空度等) (d) 制造商的零件号(e) 制造商的批号或制造日期 (f)制造商名称和/或商标3.3 环境条件:下列条件仅作为设计标准。
全国最全焊条型号、用途对照表
1、Ⅰ类材料
1
15#
J422、H08A+HJ431
2
20#+20g
TIG-J50/J427
3
20#+20g
J427
4
20g
J427
5
20g
TIG-J50/J427
6
20g
H08A+HJ431
7
20g
TIG-J50/J427
8
20R
J427
9
20R
TIG-J50/J427
119
16MnDR+0Cr18Ni9
H1Cr24Ni13、A302
120
16MnDR+16MnR
H10Mn2+E5015-G
121
16MnR+0Cr13
H1Cr24Ni13、A302
122
16MnR+12Cr2Mo
TIG-J50+J507
123
16MnR+14Cr1MoR
J057
124
16MnR+1Cr18Ni9Ti
131
20R/405+奥18-8
A132、A302
132
20R+15CrMoR
16
15CrMo+P11
H13CrMoA+R307
17
P11
H13CrMoA+R307
18
P22
TIG-R40
19
P22
TIG-R40,R407
20
P22+12Cr1MoV
H08CrMoVA/R317
艾特顿燃流熔断器系列产品介绍说明书
Eaton’s Bussmann series of radial fuses offer solutions for space-limited applicationsProduct descriptionEaton provides a diverse offering of radial fuses that include fast-acting and time-delay versions. These radial fuses carry global IEC and UL certifications to provide design options thatmeet today’s various worldwide electronic design requirements. The SS-5H and SR-5H provide protection up to 300 Vac with an interrupting rating of 100 A – ideal for electronic lighting ballasts.Eaton radial fuses have IEC and/or UL certifications across the entire amp range, including the higher 5 to10 A ratings. The higher wattage requirements of today’s end products means these higher amp rated fuses are specified more and more.Round SR-5 radial fuses offer equivalent product performance to typical 5 mm glass fuses with a 60% footprint reduction. The rectangular SS-5 fuses offer an additional 33% reduction to the SR-5 footprint.Through hole mounted radial fuses do not require theadded expense of axial leads, clips or a holder for PC board mounting. This results in a cost effective alternative to traditional electronic ferrule fuses.Eaton offers a variety ofpackaging options to support high volume production via ammo pack and bulk packordering options, with the bulk packaging available in short or long leads Fuse accessoriesFor applications requiring fuse replacement, order the BK-PCS radial fuse holder.ApplicationsPower supplies, power adapters and battery chargers play a critical role in the operation of virtually all consumer electronic devices. These power supplies or battery chargers typically convert high ac voltage from the load side to lower dcvoltage used to operate today’s electronics.Applications include:• Notebook computers and monitors• Consumer electronics • High definition televisions • Household and kitchen appliances• Mobile devices • Set top boxesBecause these products are plugged into the wall, they require primary circuit protection, as the device can be exposed to dangerous overcurrent events.Eaton’s family of rectangular and round body radial leaded fuses provide cost effective primary circuit protection without sacrificing performance inspace constrained power supply applications. The IEC designs have approvals through 6.3 A,and UL designs through 10 A.Radial fuse product aidEaton is a registered trademark.All other trademarks are property of their respective owners.EatonElectronics Division 1000 Eaton Boulevard Cleveland, OH 44122United States/electronics© 2020 EatonAll Rights Reserved Printed in USAPublication No. 4032 BU-MC20100June 2020Radial fuse accessory reference guideFuse sizeCircuit board mount fuse holdersRadialBK-PCS- mmSR-5, SR-5F 7.6mm SR-5H 8.6mm SR-5, SR-5F 35.0mm SR-5H 36.0mm8.4mm4.3mm5.08mm0.6M0.5 Min.9.0mm 18.0mm12.7mm15.0mm optionallead form7.5Tape Packaging*35.0mmSS-5, SS-5F 8.4mm 8.6mm4.3mm0.6M 0.5 Min.9.0mm 18.0mm12.7mm15.0mm optional lead form7.54.3mmSS-5H 7.85mmSS-5 / SS-5F / SS-5HTape Packaging**Bulk and ammo -pack available.SR-5 / SR-5F / SR-5HRadial fuse family overview and quick cross referenceDimensions - mmFollow us on social media to get the latest product and support information.。
SAE AMS 4982D-2007
SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising therefrom, is the sole responsibility of the user.”SAE reviews each technical report at least every five years at which time it may be reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions. Copyright © 2007 SAE InternationalAll rights reserved. No part of this publication may be reproduced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording, or otherwise, without the prior written permission of SAE. TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: 724-776-4970 (outside USA) Fax: 724-776-0790Email: custsvc@ SAE WEB ADDRESS:h ttp://AMS 4982DAEROSPACE MATERIALSPECIFICATIONIssued DEC 1974 Revised JUN 2007Superseding AMS 4982CTitanium Alloy Wire44.5 Cb(Composition similar to UNS R58450)RATIONALEAMS 4982D results from a Five Year Review and update of this specification.1. SCOPE 1.1 FormThe specification covers a titanium alloy in the form of wire. 1.2 ApplicationThis wire has been used typically for parts, such as fasteners, where cold formability is desirable or necessary and whichrequires a high strength-to-weight ratio up to 800 °F (427 °C), but usage is not restricted to such applications. 1.3 ClassificationThis specification covers two types of wire based upon condition supplied, as follows: Type 1: Annealed Type 2: As drawn 1.3.1Type 1 shall be supplied unless Type 2 is specified.2. APPLICABLE DOCUMENTSThe issue of the following documents in effect on the date of the purchase order forms a part of this specification to the extent specified herein. The supplier may work to a subsequent revision of a document unless a specific document issue is specified. When the referenced document has been cancelled and no superseding document has been specified, the last published issue of that document shall apply.Publications2.1 SAEAvailable from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (insideUSA and Canada) or 724-776-4970 (outside USA), .AMS 2241 Tolerances, Corrosion and Heat Resistant Steel, Iron Alloy, Titanium, and Titanium Alloy Bars and WireAMS 2249 Chemical Check Analysis Limits, Titanium and Titanium AlloysAMS 2809 Identification, Titanium and Titanium Alloy Wrought ProductsPublications2.2 ASTMAvailable from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959,Tel: 610-832-9585, .ASTM E 8 Tension Testing of Metallic MaterialsASTM E 112 Determining Average Grain SizeASTM E 1409 Determination of Oxygen and Nitrogen in Titanium and Titanium Alloys by the Inert Gas Fusion TechniqueASTM E 1447 Determination of Hydrogen in Titanium and Titanium Alloys by the Inert Gas Fusion ThermalConductivity/Infrared Detection MethodASTM E 1941 Determination of Carbon in Refractory and Reactive Metals and Their AlloysASTM E 2371 Analysis of Titanium and Titanium Alloys by Atomic Emission Plasma Spectrometry3. TECHNICAL REQUIREMENTS3.1 CompositionShall conform to the percentages by weight shown in Table 1; carbon shall be determined in accordance with ASTM E1941, hydrogen in accordance with ASTM E 1447, oxygen and nitrogen in accordance with ASTM E 1409, and otherelements in accordance with ASTM E 2371. Other analytical methods may be used if acceptable to the purchaser.TABLE 1 - COMPOSITIONElement minmax47.00Columbium 42.000.16Oxygen --Carbon --0.04Silicon --0.03 --`,`,,`,,````,`,,,,`,```,`,,,-`-`,,`,,`,`,,`---ppm)0.03(300 Nitrogen --0.03Iron --Chromium --0.02Magnesium --0.010.01Manganese --Hydrogen (3.1.2) -- 0.0035( 35 ppm)Other Elements, total (3.1.1) -- 0.40Titanium remainder3.1.1 Determination not required for routine acceptance.3.1.2 When ASTM E 1447 is used, sample size may be as large as 0.35 gram.3.1.3 CheckAnalysisComposition variations shall meet the applicable requirements of AMS 2249. Check analysis limits for columbium shall bewithin the limits of Table 1.3.2 MeltingPracticeAlloy shall be multiple melted. Melting cycle(s) prior to the final melting cycle shall be made using vacuum consumable electrode, nonconsumable electrode, electron beam cold hearth, or plasma arc cold hearth melting practice. The final melting cycle shall be made under vacuum using vacuum arc remelting (VAR) practice with no alloy additions permitted.3.2.1 The atmosphere for nonconsumable electrode melting shall be vacuum or shall be argon and/or helium at anabsolute pressure not higher than 1000 mm of mercury.3.2.2 The electrode tip for nonconsumable electrode melting shall be water-cooled copper.3.3 Condition3.3.1 Type 1 WireCold finished and annealed.3.3.2 Type 2 WireCold finished, with drawing lubricant removed, unless otherwise specified by purchaser.Treatment3.4 HeatType 1 wire shall be annealed by heating in vacuum (less than 0.1 µm mercury) to a temperature within the range 1450 to 1600 °F (788 to 871 °C), holding at heat for sufficient time to produce a recrystallized structure that will meet the requirements of 3.5, and cooling as required.3.5 PropertiesWire shall conform to the following requirements:3.5.1 Type 1 Annealed WireProperties3.5.1.1 TensileShall be as shown in Table 2, determined in accordance with ASTM E 8 as applicable, with the rate of strain maintained at 0.003 to 0.007 inch/inch per minute (0.003 to 0.007 mm/mm per minute) through the yield strength and then increased so as to produce failure in approximately one additional minute. When a dispute occurs between purchaser and vendor over the yield strength values, a referee test shall be performed on a machine having a strain rate pacer using a rate of 0.005 inch/inch per minute (0.005 mm/mm per minute) through the yield strength and a minimum cross-head speed of 0.10 inch per minute (0.04 mm/s) above the yield strength.TABLE 2 - MINIMUM TENSILE PROPERTIESProperties ValueTensile Strength 65.0 ksi (448 MPa)Yield Strength at 0.2% Offset 60.0 ksi (414 MPa)Elongation in 2 Inches (50.8 mm) or 4D 10%Reduction of Area 50%3.5.1.1.1 Yield strength and reduction of area requirements do not apply to wire under 0.125 inch (3.18 mm) indiameter.3.5.1.2 Average Grain SizeShall be ASTM No. 5 or finer, determined by comparison of a polished and etched sample with the chart in ASTM E 112.3.5.2Type 2 As-Drawn WireShall be as agreed upon by purchaser and vendor except that Type 2 wire annealed as in 3.4 shall also meet the requirements of 3.5.1.1 and 3.5.1.2. 3.6 QualityWire, as received by purchaser, shall be uniform in quality and condition, sound, and free from foreign materials and from imperfections detrimental to usage of the wire. 3.7 TolerancesShall conform to all applicable requirements of AMS 2241. 4. QUALITY ASSURANCE PROVISIONS 4.1Responsibility for InspectionThe vendor of wire shall supply all samples for vendor's tests and shall be responsible for the performance of all required tests. Purchaser reserves the right to sample and to perform any confirmatory testing deemed necessary to ensure that the wire conforms to specified requirements.4.2 Classification of Tests4.2.1 Acceptance TestsTests for the following requirements are acceptance tests and shall be performed on each heat or lot as applicable: 4.2.1.1 Type 1 4.2.1.1.1 Composition (3.1) of each heat.4.2.1.1.2Hydrogen content (3.1), tensile properties (3.5.1), grain size (3.5.2) and tolerances (3.7) of each lot.4.2.1.2 Type 2 4.2.1.2.1 Composition (3.1) of each heat. 4.2.1.2.2Tolerances (3.7) of each lot.4.2.2 Periodic TestsTests of Type 2 wire to demonstrate ability to develop required properties (3.5.2) are periodic tests and shall be performed at a frequency selected by the vendor unless frequency of testing is specified by purchaser.--`,`,,`,,````,`,,,,`,```,`,,,-`-`,,`,,`,`,,`---4.3 Sampling and TestingShall be in accordance with the following; a lot shall be all wire of the same nominal size from the same heat processed at the same time:4.3.1 For Acceptance Tests4.3.1.1 Type14.3.1.1.1 CompositionOne or more samples from each heat, except that for hydrogen determinations, one sample from each lot obtained after thermal and chemical processing is completed.4.3.1.1.2 Tensile Properties and Grain SizeAt least one sample from each lot.24.3.1.2 Type4.3.1.2.1 CompositionOne sample from each heat (see 8.2).4.4 ReportsMaterials:4.4.1 RawThe vendor shall provide a copy of the original material manufacturer’s report (material certification), including: producer name, product form, mill produced size, and country where the metal was melted (i.e., final melt in the case of metal processed by multiple melting operations). The vendor of the wire shall furnish with each shipment a report showing the results of tests for composition of each heat and for the hydrogen content, tensile properties and grain size of each lot of Type 1 wire, and stating that the wire conforms to the other technical requirements. This report shall include the purchase order number, heat and lot numbers, AMS 4982D, condition, size, specific annealing treatment used on Type 1 wire, and quantity.Parts:4.4.2 FabricatedA copy of the original manufacturer’s report (material certification) shall be provided by the vendor to the purchaser when the purchase order specifies AMS 4982.4.5 Resampling and RetestingIf any specimen used in the above tests fails to meet the specified requirements, disposition of the wire may be based on the results of testing three additional specimens for each original nonconforming specimen. Failure of any retest specimen to meet the specified requirements shall be cause for rejection of the wire represented. Results of all tests shall be reported.5. PREPARATION FOR DELIVERY5.1 IdentificationShall be in accordance with AMS 2809.--`,`,,`,,````,`,,,,`,```,`,,,-`-`,,`,,`,`,,`---SAE AMS 4982D - 6 - 5.2 PackagingWire shall be prepared for shipment in accordance with commercial practice and in compliance with applicable rules and regulations pertaining to the handling, packaging, and transportation of the wire to ensure carrier acceptance and safe delivery.6. ACKNOWLEDGEMENTA vendor shall mention this specification number and its revision letter in all quotations and when acknowledging purchase orders.7. REJECTIONSWire not conforming to this specification, or to modifications authorized by purchaser, will be subject to rejection.8. NOTES8.1 A change bar (|) located in the left margin is for the convenience of the user in locating areas where technicalrevisions, not editorial changes, have been made to the previous issue of this specification. An (R) symbol to the left of the document title indicates a complete revision of the specification, including technical revisions. Change bars and (R) are not used in original publications, nor in specifications that contain editorial changes only.8.2 When Type 2 wire is purchased for making fasteners, the procurement specification for the fasteners should specifythe maximum hydrogen level.8.3 Terms used in AMS are clarified in ARP1917.8.4 Dimensions and properties in inch/pound units and the Fahrenheit temperatures are primary; dimensions andproperties in SI units and the Celsius temperatures are shown as the approximate equivalents of the primary units and are presented only for information.8.5 Purchase documents should specify not less than the following:AMS 4982DType number and size of wire desiredQuantity of wire desired.PREPARED BY AMS COMMITTEE "G"。
AEM代理PTC自恢复 FUSE一次性保险丝 ESD TVS静电抑制器全系选型表
MF2410 Surface Mount Fuses "Series: AirMatrix® 中空贴片保险丝AirMatrix® MF Series产品特点:极小体积、贴片式、250V交流应用环氧树脂基体""铜端头镀镍和锡100%无铅使用温度范围:-55℃~+125℃符合IEC60127-4标准尺寸:1210和2410产品应用:照明:LED电源驱动电源:充电器、适配器、电源板医疗设备白色家电"Related Product AirMatrix® AF Series Related DocumentsQF1206F SeriesSeries: 车用系列保险丝Automotive QF F-Series产品特点尺寸涵盖0603/1206/2410,包括快断、慢断6个系列产品。
符合AEC Q200测试标准,经过高温、震动等多项严格的可靠性测试。
100% 无铅,无卤素,完全符合环境要求。
拥有全套TS16949的认证资料。
安全性高。
该系列产品全部采用熔丝内置式设计,避免熔断时能量外泄。
Related ProductAutomotive QA F-SeriesAutomotive QF H-SeriesElectrical CharacteristicsRelated DocumentsQF1206F SeriesSeries: 车用系列保险丝Automotive QF F-Series产品特点尺寸涵盖0603/1206/2410,包括快断、慢断6个系列产品。
符合AEC Q200测试标准,经过高温、震动等多项严格的可靠性测试。
100% 无铅,无卤素,完全符合环境要求。
拥有全套TS16949的认证资料。
安全性高。
该系列产品全部采用熔丝内置式设计,避免熔断时能量外泄。
Related ProductAutomotive QF F-SeriesAutomotive QA F-SeriesElectrical CharacteristicsRelated DocumentsQA2410F SeriesSeries: 车用系列保险丝Automotive QA F-Series产品特点尺寸涵盖0603/1206/2410,包括快断、慢断6个系列产品。
雅宝温度保险丝系列产品规格书
● ● ● ● ●●●
尺寸:(mm)
a 9.0±0.5
b 38±3
(P-F 系列)
c
d
Φ0.54±0.05 Φ2.5±0.1
e 3.3 or below
型号
A0-3A-F A1-3A-F A2-3A-F A3-3A-F A4-3A-F A5-3A-F A7-3A-F A8-3A-F
额定动 作温度
84℃ 102℃ 115℃ 125℃ 130℃ 135℃ 138℃ 150℃
保持 温度
45℃ 51℃ 58℃ 66℃ 71℃ 79℃ 84℃ 92℃ 94℃ 104℃ 114℃ 127℃ 144℃ 159℃ 170℃ 191℃ 200℃ 200℃
AUPO BF 系列
极限 温度
额定 电流
150℃
10A
150℃
10A
150℃
10A
150℃
10A
150℃
10A
150℃
10A
150℃
保持 温度
76℃ 85℃ 97℃ 102℃ 105℃ 108℃ 120℃
A-1A-F 系列
极限 温度
额定 电流
额定 电压
180℃ 180℃ 180℃ 180℃ 180℃ 180℃ 180℃
1A 250Vac 1A 250Vac 1A 250Vac 1A 250Vac 1A 250Vac 1A 250Vac 1A 250Vac
实测动 作温度
82±2℃ 112±3℃ 120±3℃ 126±2℃ 131±3℃ 135±2℃ 145±3℃
保持 温度
55℃ 75℃ 85℃ 90℃ 90℃ 95℃ 105℃
P-3A-F 系列
极限 温度
2008年Ford自动变速箱组件目录说明书
1622008 AUTOMATIC TRANSMISSION KIT & COMPONENTS CATALOG ©2008 PARKER HANNIFIN CORP. ALL RIGHTS RESERVED3790103008397797405R55N / 5R55S / 5R55WRWD 5 SpeedA544510034070670Input ShaftO.Dr. Ring GearO.Dr. CenterShaft783Center SupportInterm. BandDirect DrumForward ClutchForward PlanetReverse BandReverse DrumLow Sprag310037179520036178530311914363912911913910896904896437490996V.B.Parts741E414494765-6370Case313321320Valve Body917747765746322420002OHK Kit004Master L/Steels Kit 006Master 030External Seal Kit1632008 AUTOMATIC TRANSMISSION KIT & COMPONENTS CATALOG ©2008 PARKER HANNIFIN CORP . ALL RIGHTS RESERVEDRWD 5 Speed5R55N / 5R55S / 5R55W862981971961560961971985879565126106146861*229964974877564285872962972104124552894Intermediate Sprag690074266Park Gear264847Park Pawl Assy995-1995-2995-3995916-2916-3919922915916-2916-3919922916263EDA181554770Ext. Hsg.781493305678Output ShaftO.Dr. Band StrutInterm. Band Strut268841Internal Linkage991-2991-3994799991-4761P-4991072410992Yoke1642008 AUTOMATIC TRANSMISSION KIT & COMPONENTS CATALOG©2008 PARKER HANNIFIN CORP. ALL RIGHTS RESERVED*Prefix Letter ‘T’ denotes Toledo-Trans Kit (TTK) Brand Transmission Kits *Prefix Letter ‘B’ denotes Bryco Brand Transmission Kits002.............T16002AP......Overhaul Kit, 5R55N (With Bonded Pistons) 1999-Up ..............................................................1..........002.............T16002GP......Overhaul Kit, 5R55S/5R55W (With Bonded Pistons) 2002-Up..................................................1..........004.............T16004AP......Master L/Steels Kit, 5R55N (With Bonded Pistons) 1999-Up ....................................................1..........004.............T16004GP......Master L/Steels Kit, 5R55S/5R55W (With Bonded Pistons) 2002-Up .......................................1..........006.............T16006AP......Master W/Steels Kit, 5R55N (With Bonded Pistons) 1999-Up...................................................1..........006.............T16006GP......Master W/Steels Kit, 5R55S/5R55W (With Bonded Pistons) 2002-Up ......................................1..........E300...........45019............Gasket, 5R55N Bottom Pan (Plastic With Silicon Bead) OE Style (With Large Holes) 1999-Up 1..........XW4Z-7A191CA D305...........45097668......Gasket, 5R55N/5R55S/5R55W Extension Housing To Case 1999-Up......................................1..........XW4Z-7086-AA A309..........41217............Gasket, 5R55N/5R55S/5R55W Pump Bolt Washer...................................................................AR ........A310..........45097667......Gasket, 5R55N/5R55S/5R55W Pump 1999-Up..........................................................................1..........XW4Z-7A136AB A311...........1988096........O-Ring, 5R55N/5R55S/5R55W Pump Cover 1999-Up ...............................................................1..........XW4Z-7A248AA A313..........1994747........O-Ring, 5R55N Inner Pump Gear 1999-Up.................................................................................1..........F77Z-7L323AA E320...........45097692......Gasket, 5R55N Valve Body Separator Plate To Case 1999-Up ................................................1..........XW4Z-7D100-BF E320...........45097738......Gasket, 5R55S/5R55W Valve Body Separator Plate To Case (Upper) 2002-Up......................1..........1L2Z-7Z490AB-1A070..........70243V..........Seal, 5R55N/5R55S/5R55W Front (No Flange) (Rubber Coated) 1999-Up ..............................1..........F77Z-7A248AA D072...........70083............Seal, 5R55N Linkage 1999-Up ..................................................................................................1..........D5AZ-7B498A D074...........70283............Seal, 5R55N Rear 2WD 2000-Up ...............................................................................................1..........XW4Z-7052AA D074...........70205............Seal, 5R55S/5R55W Rear (W/Long Boot) 2WD 2002-Up .........................................................1..........F6UZ-7052A D074...........70282............Seal, 5R55S/5R55W Extension Housing 4X4 2002-Up .............................................................1..........1L2Z-7052BA175.............6358..............Ring Kit, 5R55N/5R55S/5R55W (2 Metal 4PTFE 2 Torlon Rings) 1999-Up ...............................1..........A178..........45060279......Ring, 5R55N, 5R55W, 5R55S Pump Support (Lock-Up) 1999-Up .............................................1..........B181...........TAW- 2212....Ring, 5R55N, 5R55W, 5R55S Forward Clutch Cylinder 1999-Up .............................................2..........D184...........45060265......Ring, 5R55N, 5R55W, 5R55S Output Shaft 1999-Up.................................................................1..........A179..........30308............Ring, 5R55N, 5R55W, 5R55S Overdrive Brake Drum 1999-Up.................................................2..........B179...........30308P ..........Ring, 5R55N, 5R55W, 5R55S Direct Clutch (Center Support) 1999-Up Torlon .........................2..........119.............45082NR........Friction Module, 5R55N 1999-Up................................................................................................1..........119.............45082LR........Friction Module, 5R55S/5R55W 2002-Up...................................................................................1..........E010...........45040N ..........Filter, 5R55N (3/8” Tall Pick-up Tube) 1999-Up ..........................................................................1..........XW4Z-7A098BB E010...........F-340.............Filter, 5R55S/5R55W (2 1/4” Tall Pick-Up Tube) 2002-Up..........................................................1..........1L2Z-7A098AC5R55N / 5R55S / 5R55WRWD 5 Speed1652008 AUTOMATIC TRANSMISSION KIT & COMPONENTS CATALOG ©2008 PARKER HANNIFIN CORP. ALL RIGHTS RESERVEDB022...........45090............Band, 5R55N Overdrive/Intermediate (Hi-Energy) 1999-Up......................................................2..........XW4Z-7D034BA 030.............45030G..........Bushing Kit, 5R55N/5R55S/5R55W 1999-Up.............................................................................1..........A034..........31530............Bushing, 5R55N/5R55S/5R55W Pump Cover 1999-Up .............................................................1..........A036..........31531............Bushing, 5R55N/5R55S/5R55W Overdrive Sun Gear 1999-Up................................................1..........A036..........45039............Bushing, 5R55N/5R55S/5R55W Stator (Front) 1999-Up ...........................................................1..........A037..........31532............Bushing, 5R55N/5R55S/5R55W Stator (Rear) 1999-Up............................................................1..........A046..........31533............Bushing, 5R55N/5R55S/5R55W Coast Clutch Drum e 56036A................................................................................................................................1..........B211...........45176A..........Washer, 5R55N/5R55S/5R55W Pump To Coast Clutch Drum .063" (Plastic) 1999-Up.............1..........F7TZ-7D014TA B211...........45176B ..........Washer, 5R55N/5R55S/5R55W Pump To Coast Clutch Drum .071" (Plastic) 1999-Up.............1..........F7TZ-7D014MA B211...........45176C ..........Washer, 5R55N/5R55S/5R55W Pump To Coast Clutch Drum .075" (Plastic) 1999-Up.............1..........F7TZ-7D014NA B211...........45176D ..........Washer, 5R55N/5R55S/5R55W Pump To Coast Clutch Drum .079" (Plastic) 1999-Up.............1..........F7TZ-7D014PA B211...........45176E ..........Washer, 5R55N/5R55S/5R55W Pump To Coast Clutch Drum .083" (Plastic) 1999-Up.............1..........F7TZ-7D014RA B211...........45176F ..........Washer, 5R55N/5R55S/5R55W Pump To Coast Clutch Drum .087" (Plastic) 1999-Up.............1..........F7TZ-7D014SA C232...........45145............Washer, 5R55N/5R55S/5R55W Bearing to Forward Hub (Solid Bronze) 1999-Up .................1..........FOTZ-7D090A D263...........45077............Washer, 5R55N/5R55S/5R55W Parking Gear To Case 1999-Up ..............................................1..........D4ZZ-7B368-AD410...........D56955J ........Switch, 5R55N Neutral Safety (12 Prong Connector) 1999-Up ...............................................1..........XW4Z-7F293AA E922...........33991............Nut, 5R55N/S/W Band 1999-Up .................................................................................................2..........380850-SRWD 5 Speed5R55N / 5R55S / 5R55W。
AMS 4928Q
宇航材料规范 AMS 4979D
宇航材料规范AMS 4979D 固溶及沉淀热处理1970年3月发布6AL-6V-2Sn1998年10月修订钛合金棒材丝材锻件及环材代替AMS4979C1范围1.1品种本规范适用钛合金棒材、丝材、锻件、闪光焊环及用于锻件或闪光焊环的坯料。
1.2应用这些产品一般用于要求达750℉(399℃)具有更高比强度的部件,但不限于该用途。
1.2.1加工工艺和工作环境可能会引起这些产品易受应力腐蚀来裂,ARP982推荐了一些减小这些开裂的方法。
2 适用文件下列出版物在规定的范围内构成本规范的一部分,应该使用最新版本的SAE出版物其它出版物的适用版本应是该购货单生效之日有效版本。
2.1SAE刊物:从美国机动车工程师学会获得(SAE)。
地址:400Commonweal th Drive, Warrendale PA 15096-0001 AMS2241 耐蚀和耐热钢、铁合金、钛及钛合金棒和丝材的尺寸公差。
AMS2241 耐蚀和耐热钢、铁合金、钛及钛合金棒和丝材的尺寸公差。
(米制)AMS 2249 钛及钛合金化学成分检查分析误差范围。
AMS2368 加工钛原材料的取样和试验,除锻件和锻坯AMS 2750 高温测定方法AMS 2808 锻件的标记AMS 2809 钛及钛合金加工产品的标识。
AMS4798钛及钛合金闪光焊环ARP982 加工钛合金产品的最小应力腐蚀裂纹。
2.2 ASTM出版物从美国材料和试验协会获得。
地址:100 Barr Harbor Drive West Conshohocken PA 19428-2959ASTM E8 金属材料拉伸试验ASTM E8M金属材料拉伸试验(米制)ASTM E120 钛及钛合金的化学分析ASTM E1409 钛及钛合金中氧的测定采用惰性气体熔融技术。
ASTM E1447 钛及钛合金H的测定采用惰性气体熔融电量法。
3技术要求3.1 成分应符合表1中的重量百分比;氧含量应按ASTM E 1409测定,氢含量应按ASTM E1447测定,其它元素应按ASTM E120 用湿法化学分析方法、光谱化学法或用由买方批准的其它分析方法测定。
航空发动机试验测试技术发展探讨
航空发动机试验测试技术发展探讨王振华;王亮【摘要】强调了航空发动机试验测试技术在发动机研制过程中的重要性.简述了航空发动机试验测试技术的特点及国内外发展现状,分析了其试验测试技术发展需求,提出了发展设想.为适应新1代航空发动机研制的需求,必须积极推进其试验测试技术的快速发展,应及时开展其研制试验所需测试仪器的研究和开发,组织开展其试验测试技术研究,加强专业间交流和协同,进一步提高试验测试结果的准确度,建立和完善试验测试技术标准规范.【期刊名称】《航空发动机》【年(卷),期】2014(040)006【总页数】5页(P47-51)【关键词】测试技术;试验;测试仪器;航空发动机【作者】王振华;王亮【作者单位】中航工业沈阳发动机设计研究所,沈阳110015;中航工业沈阳发动机设计研究所,沈阳110015【正文语种】中文【中图分类】V23航空发动机是1个复杂的动力装置,主要由进气道、压气机、燃烧室、涡轮、加力燃烧室、尾喷管、附件传动装置与附属系统等组成。
其内部的气动、热力和结构特性非常复杂,因此对其工况尚不能从计算上给予详尽准确地描述,必须依靠试验来获得相关数值。
在进行发动机装配前,需要确认每个部件的性能均满足设计指标,同时,需要在试车台上进行试验测试(如压气机的增压比、空气流量、喘振点,燃烧室的燃烧效率、出口温度分布等),获得整机的推力、单位耗油量等性能数据,用于评价其是否满足设计使用要求。
发动机研制中要进行大量的材料、零部件、整机试验测试才能确认其性能、可适用性、环境条件、完整性、战斗生存力等是否满足发动机使用要求。
据统计,一型航空发动机研制工作一般需要进行10万h的部件试验,4万h的材料试验,1万h的整机试车。
试验测试技术是发展先进航空发动机的关键技术之一,试验测试结果既是验证和修改发动机设计的重要依据,也是评价发动机部件和整机性能的重要判定条件。
“航空发动机是试出来的”已成为行业共识。
本文简述了航空发动机试验测试技术国内外发展现状,并分析了其发展需求,提出了发展设想。
SAE AMS 4943H-2008
SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising therefrom, is the sole responsibility of the user.”SAE reviews each technical report at least every five years at which time it may be reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions. Copyright © 2008 SAE InternationalAll rights reserved. No part of this publication may be reproduced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording, or otherwise, without the prior written permission of SAE.TO PLACE A DOCUMENT ORDER:Tel: 877-606-7323 (inside USA and Canada)Tel: 724-776-4970 (outside USA)Fax: 724-776-0790 Email: CustomerService@A AEROSPACE MATERIALSPECIFICATIONIssued 1971-11 Revised 2008-02 Superseding AMS 4943GTitanium Alloy, Hydraulic, Seamless Tubing3.0Al - 2.5VAnnealed (Composition similar to R56320)RATIONALEAMS 4943H results from a Five Year Review and update of this specification.1. SCOPE1.1 FormThis specification covers a titanium alloy in the form of seamless tubing.1.2 ApplicationThis tubing has been used typically for parts, such as hydraulic lines, requiring strength and oxidation resistance up to 600 °F (316 °C) and weldability, but usage is not limited to such applications.2. APPLICABLE DOCUMENTSThe issue of the following documents in effect on the date of the purchase order forms a part of this specification to the extent specified herein. The supplier may work to a subsequent revision of a document unless a specific document issue is specified. When the referenced document has been cancelled and no superseding document has been specified, the last published issue of that document shall apply.2.1 SAE PublicationsAvailable from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or 724-776-4970 (outside USA), .AMS 2244Tolerances, Titanium and Titanium Alloy Tubing AMS 2249Chemical Check Analysis Limits, Titanium and Titanium Alloys AMS 2634Ultrasonic Inspection, Thin Wall Metal Tubing AMS 2750Pyrometry AMS 2809 Identification, Titanium and Titanium Alloy Wrought Products2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, .ASTM E 8Tension Testing of Metallic Materials ASTM E 1409Determination of Oxygen and Nitrogen in Titanium and Titanium Alloys by the Inert Gas Fusion Technique ASTM E 1447Determination of Hydrogen in Titanium and Titanium Alloys by the Inert Gas Fusion Thermal Conductivity/Infrared Detection Method ASTM E 1941Determination of Carbon in Refractory and Reactive Metals and Their Alloys ASTM E 2371 Analysis of Titanium and Titanium Alloys by Atomic Emission Plasma Spectrometry2.3 ASME PublicationsAvailable from American Society of Mechanical Engineers, 22 Law Drive, P.O. Box 2900, Fairfield, NJ 07007-2900, Tel: 973-882-1170, .ASME B46.1 S urface Texture (Surface Roughness, Waviness, and Lay)3. TECHNICAL REQUIREMENTS3.1 CompositionShall conform to the percentages by weight shown in Table 1; carbon shall be determined in accordance with ASTM E 1941, hydrogen in accordance with ASTM E 1447, oxygen and nitrogen in accordance with ASTM E 1409, and other elements in accordance with ASTM E 2371. Other analytical methods may be used if acceptable to the purchaserTABLE 1 - COMPOSITIONElement min maxAluminumVanadiumIronOxygenCarbonNitrogenHydrogen (3.1.1)Yttrium (3.1.2)Other Elements, each (3.1.2)Other Elements, total (3.1.2)Titanium2.50 2.00 -- -- -- -- -- -- -- -- remainder3.50 3.00 0.30 0.12 0.050 0.020 0.015 0.005 0.10 0.40 (200 ppm) (150 ppm) ( 50 ppm) 3.1.1Sample size when using ASTM E 1447 may be as large as 0.35 gram. 3.1.2 Determination not required for routine acceptance.3.1.3 Check AnalysisComposition variations shall meet the applicable requirements of AMS 2249.3.2 Melting PracticeAlloy shall be multiple melted. Melting cycle(s) prior to the final melting cycle shall be made using vacuum consumable electrode, nonconsumable electrode, electron beam cold hearth, or plasma arc cold hearth melting practice(s). The finalmelting cycle shall be made under vacuum using vacuum arc remelting (VAR) practice with no alloy additions permitted.3.2.1 The atmosphere for nonconsumable electrode melting shall be vacuum or shall be argon and/or helium at anabsolute pressure not higher than 1000 mm of mercury.3.2.2 The electrode tip for nonconsumable electrode melting shall be water-cooled copper.3.3 ConditionCold reduced, annealed by heating to a temperature within the range 1100 to 1450 °F (593 to 788 °C), holding at the selected temperature within ±25 °F (±14 °C) for not less than 30 minutes, cooling at a rate equivalent to an air cool or slower, and descaled. Pyrometry shall be in accordance with AMS 2750.3.4 PropertiesTubing shall conform to the following requirements:3.4.1 Tensile PropertiesShall be as shown in Table 2, determined in accordance with ASTM E 8 with the rate of strain maintained at 0.003 to 0.007 inch/inch/minute (0.003 to 0.007 mm/mm/minute) through the yield strength and then increased so as to produce failure in approximately one additional minute. When a dispute occurs between purchaser and vendor over the yield strength value, a referee test shall be performed on a machine having a strain rate pacer, using a rate of 0.005 inch/inch/minute (0.005 mm/mm/minute) through the yield strength and a minimum cross head speed of 0.10 inch per minute (0.04 mm/s) above the yield strength.TABLE 2 - MINIMUM TENSILE PROPERTIES Property ValueTensile Strength Yield Strength at 0.2% Offset Elongation in 2 Inches (50.8 mm) 90 ksi (621 MPa)75 ksi (517 MPa) 15%3.4.2 FlarabilitySpecimens as in 4.3.4.1 shall withstand flaring at room temperature, without formation of cracks or other visible defects, by being forced axially, with steady pressure, over a hardened and polished tapered steel pin having a 74-degree included angle to produce a flare having a permanent expanded OD not less than 1.30 times the original nominal OD.3.4.3 Pressure TestingTubing shall show no bulges, leaks, pin holes, cracks, or other defects when subjected to an internal hydrostatic pressure (P) sufficient to cause a tensile stress of 75 ksi (517 MPa) in the tubing wall, except that a diametric permanent set of 0.002 inch/inch (0.002 mm/mm) of diameter is acceptable. The hydrostatic pressure (P) shall be determined using Equation 1.P S D 2d 2–D 2d 2+------------------= (Eq. 1)where:P = T est pressure in ksi (MPa)S = 75 ksi (517 MPa)D = N ominal ODd = N ominal ID3.4.4 BendingTubing shall not develop cracks, tears, breaks, or other flaws when bent at ambient temperature 180 degrees around a suitable bend die having a centerline radius equal to three times the nominal OD of the tubing. A solid rod or ball-type retractable mandrel inserted to the tangent of the bend shall be used to support the inside of the tube during bending.3.4.5 FlatteningSpecimens as in 4.3.5 shall show no cracks, tears, breaks, opened die marks, or opened polishing marks when a half-section of a tube is flattened between parallel plates until the distance between plates is essentially equal to the wall thickness of the tube. The flattened sample shall be examined under a binocular microscope at 20 to 35X magnification.3.4.5.1 As an alternate flattening test method, the half-tube sample may be placed between mandrels and pressedtogether to produce a flat surface approximately 3/8 inch (9.5 mm) wide on the tubing ID. The mandrel or mandrels shall be positioned so that the width of the flattened area will be parallel to the length of the half-section of tubing.3.4.6 MicrostructureShall be that structure resulting from processing within the alpha-beta phase field. Microstructure shall conform to 3.4.6.1 or 3.4.6.2.3.4.6.1 Equiaxed and/or elongated primary alpha in a transformed beta matrix with no continuous network of alpha atprior beta grain boundaries.3.4.6.2 Essentially complete field of equiaxed and/or elongated alpha with or without intergranular beta and with nocontinuous network of alpha at prior beta grain boundaries3.4.7 The tubing shall be free of any oxygen-rich layer, such as alpha case (See 8.2), or other surface contamination,determined by microscopic examination at not lower than 400X magnification or by other method acceptable to purchaser.3.5 QualityTubing, as received by purchaser, shall be uniform in quality and condition and shall have a finish conforming to the best practice for high quality aircraft tubing. It shall be smooth and free from heavy scale or oxide, burrs, seams, tears, cracks, grooves, laminations, slivers, pits, and other imperfections detrimental to usage of the tubing. Surface imperfections, such as handling marks, straightening marks, light mandrel and die marks, shallow pits, and scale pattern will not be considered injurious if the imperfections are removable within the tolerances specified for wall thickness but removal of such imperfections is not required.3.5.1 Each tube shall be ultrasonically inspected in accordance with AMS 2634 and shall conform to Class AA.Condition3.5.2 SurfaceSurface3.5.2.1 ODShall show a uniformly acid-pickled surface finish; not less than 0.0005 inch (12.7 µm) shall have been chemically removed from the wall thickness as a finishing operation. Soft belt polishing prior to the pickling operation is permissible but traces of polishing marks shall be removed by the pickling operation. Centerless grinding or other mechanical sizing operations are not permitted.Surface3.5.2.2 IDShall show a uniform matte finish, produced by abrasive blasting with grit not larger than 100 mesh (150 µm) followed by acid pickling to remove not less than 0.0005 inch (12.7 µm) from the wall thickness.3.5.2.3 SurfaceTextureShall be not greater than 63 microinches (1.6 µm) on the ID and be not greater than 32 microinches (0.8 µm) on the OD, determined in accordance with ASME B46.1.3.5.3 SurfaceCleanlinessThe ID and OD surfaces of the tubing shall be free from grease and other foreign matter. Metallic flakes or particles shall not be collected by a clean, white cloth drawn through the bore of a sample tube. Discoloration of the cloth, without the presence of metallic flakes or particles, is acceptable.3.6 TolerancesShall conform to all applicable requirements of AMS 2244 for special tolerances.4. QUALITY ASSURANCE PROVISIONS4.1 Responsibility for InspectionThe vendor of tubing shall supply all samples for vendor's tests and shall be responsible for the performance of all required tests. Purchaser reserves the right to sample and to perform any confirmatory testing deemed necessary to ensure that the tubing conforms to specified requirements.4.2 Classification of TestsAll technical requirements are acceptance tests and preproduction tests and shall be performed prior to or on the initial shipment of tubing to a purchaser, on each heat or lot as applicable, when a change in material and/or processing requires reapproval as in 4.4, and when purchaser deems confirmatory testing to be required.4.3 Sampling and TestingShall be in accordance with the following; a lot shall be all tubing of the same nominal size, from the same heat, processed at the same time, and annealed in the same furnace charge:4.3.1 CompositionOne sample from each heat; for hydrogen determination, one sample from each lot obtained after thermal and chemical processing is completed.Properties4.3.2 TensileOne sample from each 1000 feet (305 m) or three samples from each lot, whichever is greater.4.3.3 MicrostructureOne sample from each lot.4.3.4 Pressure, Bend, and Flarability TestsThree samples from each lot:4.3.4.1 Specimens for the flarability test (3.4.2) shall be full tubes or sections cut from a tube. The end of the specimento be flared shall be cut square, with the cut end smooth and free from burrs, but not rounded.Test4.3.5 FlatteningOne sample from each 135 feet (41 m) of tubing or 10 samples from each lot, whichever is less. Each specimen shall be approximately 3 inches (76 mm) long, cut in half, with the cuts being parallel to the axis of the tube.Tests4.3.6 UltrasonicEach tube.4.3.7 Surface Condition and TolerancesEach tube, except that ID surface inspection need only be made on each sample selected for the flattening test.4.4 ApprovalSample tubing or process sheets showing the process control factors for producing the tubing shall be approved by the cognizant engineering organization before tubing for production use is supplied, unless such approval is waived by purchaser.4.4.1 Vendor shall establish parameters for the process control factors which will produce tubing meeting specifiedrequirements. If necessary to make any change in parameters for the process control factors, vendor shall submit, for reapproval, revised process sheets and, when requested, sample tubing. Tubing incorporating the revised operations shall not be shipped prior to receipt of reapproval.4.4.1.1 Control factors for producing tubing include, but are not limited to, the following:Acceptance criteria for tube hollowsConditioning practice for tube hollowsCold working proceduresAnnealing proceduresTube ID and OD finishing operationsFinal inspection procedures4.4.1.2 Any of the process control factors for which parameters are considered proprietary by the vendor may beassigned a code designation. Each variation in such parameters shall be assigned a modified code designation.4.5 ReportsThe vendor shall provide a copy of the original material manufacturer’s report (material certification) including: producer name, product form, mill produced size, and country where the metal was melted (i.e., final melt in the case of metal processed by multiple melting operations). The vendor of tubing shall furnish with each shipment a report showing the results of tests for composition of each heat and for the hydrogen content, tensile properties, pressure test, bend test, and flattening requirements of each lot, and stating that the tubing conforms to the other technical requirements. This report shall include the purchase order number, heat and lot numbers, AMS 4943H, size, and quantity.4.6 Resampling and RetestingIf any specimen used in the above tests fails to meet specified requirements, disposition of the tubing may be based on the results of testing three additional specimens for each original nonconforming specimen. Failure of any retest specimen to meet specified requirements shall be cause for rejection of the tubing represented. Results of all tests shall be reported.5. PREPARATION FOR DELIVERY5.1 IdentificationShall be in accordance with AMS 2809.5.2 PackagingTubing shall be prepared for shipment in accordance with commercial practice and in compliance with applicable rules and regulations pertaining to the handling, packaging, and transportation of the tubing to ensure carrier acceptance and safe delivery.6. ACKNOWLEDGMENTA vendor shall include this specification number and its revision letter in all quotations and when acknowledging purchase orders.7. REJECTIONSTubing not conforming to this specification, or to modifications authorized by purchaser, will be subject to rejection.8. NOTES8.1 A change bar (|) located in the left margin is for the convenience of the user in locating areas where technicalrevisions, not editorial changes, have been made to the previous issue of this document. An (R) symbol to the left of the document title indicates a complete revision of the document, including technical revisions. Change bars and (R) are not used in original publications, nor in documents that contain editorial changes only.8.2 Terms used in AMS are clarified in ARP1917 and as follows.8.2.1 An oxygen rich layer, such as alpha case, is hard and brittle and results in marked lowering of fatigue properties.8.2.2 Terminology relating to titanium microstructures is presented in AS1814.8.3 Dimensions and properties in inch/pound units and the Fahrenheit temperatures are primary; dimensions andproperties in SI units and the Celsius temperatures are shown as the approximate equivalents of the primary units and are presented only for information.8.4 Purchase documents should specify not less than the following:AMS 4943HSize of tubing desiredQuantity of tubing desired.PREPARED BY AMS COMMITTEE “G”。
SAE AMS 5596K-2007 Nickel Alloy UNS N07718
SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising therefrom, is the sole responsibility of the user.”SAE reviews each technical report at least every five years at which time it may be reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions. Copyright © 2007 SAE InternationalAll rights reserved. No part of this publication may be reproduced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording, or otherwise, without the prior written permission of SAE. TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: 724-776-4970 (outside USA) Fax: 724-776-0790Email: CustomerService@ SAE WEB ADDRESS:h ttp://AMS 5596KAEROSPACE MATERIALSPECIFICATIONIssued JAN 1964 Revised MAY 2007 Superseding AMS 5596JNickel Alloy, Corrosion and Heat-Resistant, Sheet, Strip, Foil and Plate52.5Ni - 19Cr - 3.0Mo - 5.1Cb (Nb) - 0.90Ti - 0.50Al - 18Fe Consumable Electrode Remelted or Vacuum Induction Melted1775 °F (968 °C) Solution Heat Treated(Composition similar to UNS N07718)RATIONALEAMS 5596K is a Five Year Review and update of this specification.1. SCOPE 1.1 FormThis specification covers a corrosion and heat-resistant nickel alloy in the form of sheet, strip, foil, and plate. 1.2 ApplicationThese products have been used typically for parts requiring resistance to creep and stress-rupture up to 1300 °F (704 °C) and oxidation resistance up to 1800 °F (982 °C), particularly those parts which are formed or welded and then heat treated to develop desired properties, but usage is not limited to such applications. 2. APPLICABLE DOCUMENTSThe issue of the following documents in effect on the date of the purchase order forms a part of this specification to the extent specified herein. The supplier may work to a subsequent revision of a document unless a specific document issue is specified. When the referenced document has been cancelled and no superseding document has been specified, the last published issue of that document shall apply. 2.1 SAE PublicationsAvailable from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or 724-776-4970 (outside USA), or . AMS 2262 Tolerances, Nickel, Nickel Alloy, and Cobalt Alloy Sheet, Strip, and Plate AMS 2269 Chemical Check Analysis Limits, NIckel, Nickel Alloys, and Cobalt AlloysAMS 2371 Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant Steels and Alloys, Wrought Products and Forging StockAMS 2807 Identification, Carbon and Low-Alloy Steels, Corrosion and Heat-Resistant Steels and Alloys, Sheet, Strip, Plate, and Aircraft TubingAS4194Sheet and Strip Surface Finish Nomenclature--`,`,,`,,````,`,,,,`,```,`,,,-`-`,,`,,`,`,,`-----`,`,,`,,````,`,,,,`,```,`,,,-`-`,,`,,`,`,,`---SAE AMS 5596K - 2 - 2.2 ASTMPublicationsAvailable from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, or .ASTM A 480/A 480M Flat-Rolled Stainless and Heat-Resisting Steel Plate, Sheet, and StripASTM E 3 Preparation of Metallographic SpecimensASTM E 8 Tension Testing of Metallic MaterialsASTM E 8M Tension Testing of Metallic Materials (Metric)ASTM E 18 Rockwell Hardness and Rockwell Superficial Hardness of Metallic MaterialsASTM E 21 Elevated Temperature Tension Tests for Metallic MaterialsASTM E 112 Determining Average Grain SizeASTM E 139 Conducting Creep, Creep-Rupture, and Stress-Rupture Tests of Metallic MaterialsASTM E 290 Bend Test for Ductility of Metallic MaterialsASTM E 354 Chemical Analysis of High-Temperature, Electrical, Magnetic, and Other Similar Iron, Nickel, and Cobalt AlloysASTM E 384 Microindentation Hardness of Materials3. TECHNICAL REQUIREMENTS3.1 CompositionShall conform to the percentages by weight shown in Table 1, determined by wet chemical methods in accordance with ASTM E 354, by spectrochemical methods, or by other analytical methods acceptable to purchaser.Element minmaxCarbon --0.080.35Manganese --0.35Silicon --0.015Phosphorus --Sulfur --0.01521.00Chromium 17.0055.00Nickel 50.00Molybdenum 2.803.30Columbium (Niobium) 4.75 5.501.15Titanium 0.650.80Aluminum 0.20Cobalt --1.00Tantalum -- 0.05Boron --0.0060.30Copper --Iron remainder3.1.1 CheckAnalysisComposition variations shall meet the applicable requirements of AMS 2269.3.2 MeltingPracticeAlloy shall be multiple melted using consumable electrode practice in the remelt cycle or shall be induction melted undervacuum. If consumable electrode remelting is not performed in vacuum, electrodes which have been produced by vacuum induction melting shall be used for remelting.3.3 ConditionThe product shall be supplied in the following condition:3.3.1 Sheet, Strip, and FoilHot or cold rolled, solution heat treated, and, unless solution heat treatment is performed in an atmosphere yielding a bright finish, descaled having a surface appearance in accordance with ASTM A 480/A 480M and AS4194 comparable to 3.3.1.1 and 3.3.1.2, as applicable, except that product 0.010 inch (0.25 mm) and under in nominal thickness shall have a surface appearance comparable to No. 2B finish.3.3.1.1 SheetNo. 2D finish.3.3.1.2 StripNo. 1 strip finish.3.3.2 PlateHot rolled, solution heat treated, and, unless solution heat treatment is performed in an atmosphere yielding a bright finish, descaled.3.4 Solution Heat Treatment3.4.1 Product 0.050 Inch (1.27 mm) and Over in ThicknessHeat to a temperature within the range 1725 to 1825 °F (941 to 996 °C), hold at the selected temperature within ±25 °F (±14 °C) for a time commensurate with product thickness, and cool at a rate equivalent to an air cool or faster.3.4.2 Product under 0.050 Inch (1.27 mm) in ThicknessNo specific heat treating instructions are specified, but it is recommended that the product be solution heat treated by heating in a suitable protective atmosphere, preferably in hydrogen or argon (See 3.4.4) or in vacuum (10-4 Torr or less), to a temperature within the range 1725 to 1825 °F (941 to 996 °C), holding at the selected temperature within ±25 °F (±14 °C) for a time commensurate with product thickness, and cooling at a rate equivalent to an air cool or faster.3.4.3 The use of dissociated ammonia as protective atmosphere is not recommended.3.4.4 For product 0.010 inch (0.25 mm) and under in nominal thickness, a dew point of -60 °F (-50 °C) or lower ispreferable when using hydrogen or argon atmosphere.--`,`,,`,,````,`,,,,`,```,`,,,-`-`,,`,,`,`,,`---3.5 PropertiesProduct, 1.00 inch (25.4 mm) and under in nominal thickness, shall conform to the following requirements: 3.5.1 As Solution Heat Treated3.5.1.1 TensilePropertiesShall be as shown in Table 2, determined in accordance with ASTM E 8 or ASTM E 8M.TABLE 2A - TENSILE PROPERTIES, INCH/POUND UNITSNominal ThicknessInchTensileStrengthksi, maxYield Strengthat 0.2% Offsetksi, maxElongation in2 Inches or 4D%, minUp to 0.010, incl 140 80.0 report Over 0.010 to 0.1874, incl 140 80.0 30 Over 0.1874 to 1.00, incl 150 105 30 TABLE 2B - TENSILE PROPERTIES, SI UNITSNominal Thickness MillimetersTensileStrengthMPa, maxYield Strengthat 0.2% OffsetMPa, maxElongation in50.8 mm or 4D%, minUp to 0.25, incl 965 552 reportOver 0.25 to 4.760, incl 965 552 30Over 4.760 to 25.4, incl 1034 724 303.5.1.2 HardnessShall be not higher than shown in Table 3, or equivalent (See 8.2), determined in accordance with ASTM E 18; for thin gages, where superficial hardness testing is impractical, microhardness testing in accordance with ASTM E 384 may be used. Product shall not be rejected on the basis of hardness if the tensile properties of 3.5.1.1 are acceptable, determined on specimens taken from the same sample as that with nonconforming hardness or from another sample with similar nonconforming hardness.TABLE 3 - MAXIMUM HARDNESSNominal ThicknessInch Nominal ThicknessMillimeters HardnessUp to 0.1874, incl Up to 4.760, incl 102 HRBOver 0.1874 to 1.00, incl Over 4.760 to 25.4, incl 25 HRC3.5.1.3 BendingProduct 0.1874 inch (4.760 mm) and under in nominal thickness shall be tested in accordance with ASTM E 290 using a sample prepared nominally 0.75 inch (19.0 mm) in width with its axis of bending parallel to the direction of rolling and shall withstand without cracking bending at room temperature through an angle of 180 degrees around a diameter equal to the bend factor shown in Table 4 times the nominal thickness of the product.TABLE 4 - BENDING PARAMETERSNominal ThicknessInch Nominal ThicknessMillimetersBendFactorUp to 0.050, incl Up to 1.27, incl 1 Over 0.050 to 0.1874, incl Over 1.27 to 4.760, incl 2--`,`,,`,,````,`,,,,`,```,`,,,-`-`,,`,,`,`,,`---3.5.1.4 Average Grain SizeShall be as follows, determined in accordance with ASTM E 112:3.5.1.4.1 For Product 0.010 inch (0.25 mm) and Under in Nominal ThicknessASTM No. 8 or finer.3.5.1.4.2 For Product Over 0.010 to 0.250 inch (0.25 to 6.35 mm), Inclusive, in Nominal ThicknessASTM No. 6 or finer.3.5.1.4.3 For Product Over 0.250 inch (6.35 mm) in Nominal ThicknessASTM No. 4 or finer.3.5.1.5 SurfaceMicrostructureMetallographic examination on the unetched and etched specimen cross-section of product 0.125 inch (3.18 mm) and under in thickness, shall disclose no alloy depleted surface layer (See 8.3.1), intergranular attack, or other detrimental surface conditions greater than 0.0005 inch (0.013 mm) for product 0.060 inch (1.52 mm) and under in nominal thickness, or greater than 0.001 inch (0.025 mm) for product over 0.060 inch (1.52 mm) in nominal thickness. Other standards for acceptance or limits for product over 0.125 inch (3.18 mm) in thickness may be established by purchaser. Each specimen shall be prepared according to ASTM E 3 and evaluated at 500X magnification.3.5.2 After Precipitation Heat TreatmentThe product shall have the following properties after being precipitation heat treated by heating to 1325 °F ± 15 (718 °C ± 8), holding at heat for 8 hours ± 0.5, cooling at a rate of 100 F ± 15 (56 C ± 8) degrees per hour to 1150 °F ± 15 (621 °C ± 8), holding at 1150 °F ± 15 (621 °C ± 8) for 8 hours ± 0.5, and cooling in air. Instead of the 100 F ± 15 (56 C ± 8) degrees per hour cooling rate to 1150 °F ± 15 (621 °C ± 8), product may be furnace cooled at any rate provided the time at 1150 °F ± 15 (621 °C ± 8) is adjusted to give a total precipitation heat treatment time of 18 hours. The product shall also meet the requirements of 3.5.2.1, 3.5.2.2, and 3.5.2.3 after being re-solution heat treated by heating to 1750 °F ± 25 (954 °C ± 14), holding at heat for 60 minutes ± 5, and cooling at a rate equivalent to an air cool or faster and precipitation heat treated as above.3.5.2.1 TensileProperties3.5.2.1.1 At Room TemperatureShall be as shown in Table 5, determined in accordance with ASTM E 8 or ASTM E 8M.TABLE 5A - MINIMUM ROOM TEMPERATURE TENSILE PROPERTIES, INCH/POUND UNITSNominal ThicknessInchTensileStrengthksiYield Strengthat 0.2% OffsetksiElongation in2 Inches or 4D%Up to 0.010, incl 180 150 report Over 0.010 to 1.00, incl 180 150 12TABLE 5B - MINIMUM ROOM TEMPERATURE TENSILE PROPERTIES, SI UNITSNominal Thickness MillimetersTensileStrengthMPaYield Strengthat 0.2% OffsetMPaElongation in50.8 mm or 4D%Up to 0.25, incl 1241 1034 report Over 0.25 to 25.4, incl 1241 1034 12 --`,`,,`,,````,`,,,,`,```,`,,,-`-`,,`,,`,`,,`---3.5.2.1.2 At 1200 °F (649 °C)Shall be as shown in Table 6, determined in accordance with ASTM E 21 on specimens heated to 1200 °F ± 5 (649 °C ± 3), held at heat for not less than 20 minutes before testing, and tested at 1200 °F ± 5 (649 °C ± 3).TABLE 6A - MINIMUM ELEVATED TEMPERATURE TENSILE PROPERTIES, INCH/POUND UNITSNominal ThicknessInchTensileStrengthksiYield Strengthat 0.2% OffsetksiElongation in2 Inches or 4D%Up to 0.025, incl 140 115 5 Over 0.025 to 1.00, incl 145 120 5TABLE 6B - MINIMUM ELEVATED TEMPERATURE TENSILE PROPERTIES, SI UNITSNominal Thickness MillimetersTensileStrengthMPaYield Strengthat 0.2% OffsetMPaElongation in50.8 mm or 4D%Up to 0.64, incl 965 793 5Over 0.64 to 25.4, incl 1000 827 53.5.2.1.2.1 For product 0.010 inch (0.25 mm) and under in nominal thickness, properties may be established using asample up to 0.025 inch (0.64 mm) in nominal thickness from the same master coil and heat. The supplier’scertification of test shall indicate the thickness at which the elevated temperature tensile test was performed.Properties do not apply to product 0.010 inch (0.25 mm) and under, but product shall be produced fromproduct under 0.025 inch (0.64 mm) that has met property requirements.3.5.2.2 HardnessShall be not lower than 36 HRC, or equivalent (See 8.2), determined in accordance with ASTM E 18; for thin gages, where superficial hardness testing is impractical, microhardness testing in accordance with ASTM E 384 may be used. Product shall not be rejected on the basis of hardness if the tensile properties of 3.5.2.1.1 are acceptable, determined on specimens taken from the same sample as that with nonconforming hardness or from another sample with similar nonconforming hardness.3.5.2.3 Stress-Rupture Properties at 1200 °F (649 °C)A tensile specimen, maintained at 1200 °F ± 3 (649 °C ± 2) while a load sufficient to product the initial axial stress shown in Table 7 or higher stress is applied continuously, shall not rupture in less than 23 hours. The test shall be continued to rupture without change of load. Elongation after rupture, measured at room temperature, shall be not less than specified in Table 7. Tests shall be conducted in accordance with ASTM E 139.TABLE 7A - STRESS-RUPTURE PROPERTIES, INCH/POUND UNITSNominal ThicknessInch Initial AxialStress, ksiElongation in2 Inches or 4D%Up to 0.015, incl 95 - Over 0.015 to 0.025, incl 95 4 Over 0.025 to 1.00, incl 100 4 TABLE 7B - STRESS-RUPTURE PROPERTIES, SI UNITSNominal Thickness MillimetersInitial AxialStress, MPaElongation in50.8 mm or 4D%Up to 0.38, incl 655 - Over 0.38 to 0.64, incl 655 4 Over 0.64 to 25.4, incl 689 4 --` , ` , , ` , , ` ` ` ` , ` , , , , ` , ` ` ` , ` , , , -` -` , , ` , , ` , ` , , ` ---3.5.2.3.1 For product 0.010 inch (0.25 mm) and under in nominal thickness, stress-rupture properties may beestablished using a sample up to 0.025 inch (0.64 mm) in nominal thickness from the same master coil andheat. The supplier’s certification of test shall indicate the thickness at which the stress-rupture test wasperformed. Properties do not apply to product 0.010 inch (0.25 mm) and under, but product shall be producedfrom product under 0.025 inch (0.64 mm) that has met property requirements.3.5.2.3.2 The test of 3.5.2.3 may be conducted using incremental loading. In such case, the load required to producethe initial axial stress shown in Table 7 shall be used to rupture or for 23 hours, whichever occurs first. Afterthe 23 hours and at intervals of 8 hours minimum thereafter, the stress shall be increased in increments of 5.0ksi (34.5 MPa). Time to rupture and elongation requirements shall be as specified in 3.5.2.3.3.6 QualityThe product, as received by purchaser, shall be uniform in quality and condition, sound, and free from foreign materials and from imperfections detrimental to usage of the product.3.7 TolerancesShall conform to all applicable requirements of AMS 2262.4. QUALITY ASSURANCE PROVISIONS4.1 Responsibility for InspectionThe vendor of the product shall supply all samples for vendor’s tests and shall be responsible for the performance of allrequired tests. Purchaser reserves the right to sample and to perform any confirmatory testing deemed necessary to --`,`,,`,,````,`,,,,`,```,`,,,-`-`,,`,,`,`,,`---ensure that the product conforms to specified requirements.4.2 Classification of Tests4.2.1 AcceptanceTestsThe following requirements are acceptance tests and shall be performed on each heat or lot as applicable.4.2.1.1 Composition (3.1) of each heat and tolerances (3.7) of each lot.4.2.1.2 Tensile properties (3.5.1.1), hardness (3.5.1.2), bending (3.5.1.3), average grain size (3.5.1.4) and surfacemicrostructure (3.5.1.5) of each lot as solution heat treated.4.2.1.3 Room temperature tensile properties (3.5.2.1.1) and hardness (3.5.2.2) of each lot after precipitation heattreatment.4.2.2 PeriodicTestsThe following requirements are periodic tests and shall be performed at a frequency selected by the vendor unless frequency of testing is specified by purchaser.4.2.2.1 Tensile properties at 1200 °F (649 °C) (3.5.2.1.2) and stress-rupture properties (3.5.2.3) after precipitation heattreatment.4.2.2.2 Tensile properties (3.5.2.1.1 and 3.5.2.1.2), hardness (3.5.2.2), and stress-rupture properties (3.5.2.3) after re-solution and precipitation heat treatment as in 3.5.2.4.3 Sampling and TestingShall be in accordance with AMS 2371.4.4 ReportsThe vendor of the product shall furnish with each shipment a report showing the results of tests for composition of each heat and the results of tests for tensile properties, hardness, bending, average grain size and surface microstructure as solution heat treated, and for room temperature tensile properties and hardness after precipitation heat treatment of each lot, and stating that the product conforms to the other technical requirements. This report shall include the purchase order number, heat and lot numbers, AMS 5596K, size and quantity.4.5 Resampling and RetestingShall be in accordance with AMS 2371.5. PREPARATION FOR DELIVERY5.1 IdentificationShall be in accordance with AMS 2807.5.2 PackagingThe product shall be prepared for shipment in accordance with commercial practice and in compliance with applicable rules and regulations pertaining to the handling, packaging and transportation of the product to ensure carrier acceptance and safe delivery.6. ACKNOWLEDGMENTA vendor shall mention this specification number and its revision letter in all quotations and when acknowledging purchase orders.7. REJECTIONSProduct not conforming to this specification, or to modifications authorized by purchaser, will be subject to rejection.8. NOTES--`,`,,`,,````,`,,,,`,```,`,,,-`-`,,`,,`,`,,`---8.1 A change bar (|) located in the left margin is for the convenience of the user in locating areas where technicalrevisions, not editorial changes, have been made to the previous issue of a specification. An (R) symbol to the left of the document title indicates a complete revision of the specification, including technical revision. Change bars and (R) are not used in original publications, nor in specifications that contain editorial changes only.8.2 Hardness conversion tables for metals are presented in ASTM E 140.8.3 Terms used in AMS are clarified in ARP1917 and as follows:8.3.1 An alloy-depleted layer is defined as a loss of alloying elements at the surface sufficient to affect a near-surfacemicrostructure difference, using a suitable etchant.8.4 Dimensions and properties in inch/pound units and the Fahrenheit temperatures are primary; dimensions andproperties in SI units and the Celsius temperatures are shown as the approximate equivalents of the primary units and are presented only for information.8.5 Purchase documents should specify not less than the following:AMS 5596KForm and size of product desiredQuantity of product desiredStandards for acceptance of surface microstructure (See 3.5.1.5).PREPARED BY AMS COMMITTEE “F”。
SAE ARP 490F-2008电液伺服阀(修订版)
SAE ARP490F电液伺服阀(修订版)航空航天ARP490F推荐惯例基本情况SAE ARP490文件本修订版经过定期有效性审核推出。
其包括了SAE A-6小组和委员会成员建议的修改。
《国际自动机工程师学会(SAE)技术标准委员会章程》规定:“本报告由SAE发布,用以促进技术与工程科学的发展水平。
使用本报告完全出于自愿,本报告对于任何特殊用途的可行性和适用性,包括由此引起的任何专利侵权问题,均由使用者个人承担责任。
”SAE至少每五年对各技术报告审查一次,届时会重申、修订或废除这些报告。
SAE欢迎您提出书面意见和建议。
国际自动机工程师学会2008年版权所有。
保留所有权利。
未经SAE事先书面许可,不允许该出版物的任何部分被复制、存储于检索系统或被以任何形式或任何途径,包括电子、手抄、照片、录音或其他方式等传播。
订购方式:电话:877-606-7323(美国和加拿大境内)电话:+1 724-776-4970(美国境外)传真:724-776-0790邮箱:CustomerService@SAE网址:SAE ARP490 F版-3 -1. 范围本SAE航空航天推荐惯例(ARP)提供了定义和背景信息,用于理解电液流量伺服阀物理性能和试验程序。
这份推荐惯例包括接口定义和输入/输出特性,它不限制或试图定义伺服阀的内部特性。
由于这个原因,这份推荐惯例也适用于具有不同的内部功能、不同等级、不同物理尺寸的阀以及使用不同流体的阀。
在某些情况下,为保持互换性,建议统一阀门设计标准,例如阀的极性、固定螺栓和出液口位置。
这份推荐惯例在制定采购规范和功能试验方面也提供了广泛的指导。
附录A提供了采购规范的样本。
这份推荐惯例主要关注的是四通阀,三通阀很少讨论。
压力控制阀的术语见附录B。
这份推荐惯例适用于所有类型飞行器的流体动力系统,而且适用于军用、民用和航天设计/鉴定标准,对于特定的控制系统,需要另外的规范或专用的试验程序规定特定的要求。
赛米控丹佛斯电子 Board_93_GB_SKYPER_42_R 数据表
®Adaptor boardIGBT Driver CoreBoard 93 GB SKYPER 42 R Preliminary Data Features•Two output channels •Gold nickel finish •Failure managementTypical Applications*•Adaptor board for SKYPER 42 IGBT drivers in bridge circuits for industrial applications •PCB with gold plating •DC bus up to 1200VFootnotesIsolation test voltage with external high voltage diodeThe isolation test is not performed as a series test at SEMIKRONThe driver power can be expanded to 50µC with external boost capacitorsIsolation coordination in compliance with EN50178 PD2Operating temperature is real ambient temperature around the driver core Degree of protection: IP00This is an electrostatic discharge sensitive device (ESDS), international standard IEC 60747-1, Chapter IX* The specifications of our components may not be considered as an assurance of component characteristics. Components have to be tested for the respective application. Adjustments may be necessary. The use of SEMIKRON products in life support appliances and systems is subject to prior specification and written approval by SEMIKRON. We therefore strongly recommend prior consultation of our staff.Absolute Maximum Ratings SymbolConditionsValuesUnitV s Supply voltage primary 16V Iout PEAK Output peak current 30A Iout AVmax Output average current 150mA f max Max. switching frequency100kHz V CECollector emitter voltage sense across the IGBT1700V V isol IO Isolation test voltage input - output (AC, rms, 2s)4000V V isolPD Partial discharge extinction voltage, rms, Q PD ≤ 10pC1500V V isol12Isolation test voltage output 1 - output 2 (AC, rms, 2s)1500V R Gon min Minimum rating for external R Gon 0.8ΩR Goff min Minimum rating for external R Goff 0.8ΩT op Operating temperature -40...85°C T stgStorage temperature-40 (85)°CCharacteristics SymbolConditionsmin.typ.max.UnitV s Supply voltage primary side 14.41515.6V V i Input signal voltage on / off 15 / 0V V IT+Input treshold voltage HIGH 12.3V V IT-Input threshold voltage (LOW) 4.6V V G(on)Turn on output voltage 15V V G(off)Turn off output voltage-8V t d(on)IO Input-output turn-on propagation time 1.1µs t d(off)IOInput-output turn-on propagation time1.1µsAdaptor Board 93 SKYPER® 42 RTechnical ExplanationsRevision 04------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ This Technical Explanation is valid for the following parts:Related documents:Prepared by: Johannes Krapp------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ ContentApplication and Handling Instructions (2)Further application support (2)General Description (2)Dimensions (3)PIN Array (3)Setting Dynamic Short Circuit Protection (4)Collector Series Resistance (4)Adaptation Gate Resistors (5)Boost Capacitors (6)Environmental conditions (6)Mounting Notes (6)Please note:All values in this technical explanation are typical values. Typical values are the average values expected in large quantities and are provided for information purposes only. These values can and do vary in different applications. All operating parameters should be validated by user’s technical experts for each application.Application and Handling Instructions▪Please provide for static discharge protection during handling. As long as the hybrid driver is not completely assembled, the input terminals have to be short-circuited. Persons working with devices have to wear a grounded bracelet. Any synthetic floor coverings must not be statically chargeable. Even during transportation the input terminals have to be short-circuited using, for example, conductive rubber. Worktables have to be grounded. The same safety requirements apply to MOSFET- and IGBT-modules.▪Any parasitic inductances within the DC-link have to be minimised. Over-voltages may be absorbed by C- or RCD-snubber networks between main terminals for PLUS and MINUS of the power module.▪When first operating a newly developed circuit, SEMIKRON recommends to apply low collector voltage and load current in the beginning and to increase these values gradually, observing the turn-off behaviour of the free-wheeling diode and the turn-off voltage spikes generated across the IGBT. An oscillographic control will be necessary. Additionally, the case temperature of the module has to be monitored. When the circuit works correctly under rated operation conditions, short-circuit testing may be done, starting again with low collector voltage.▪It is important to feed any errors back to the control circuit and to switch off the device immediately in failure events.Repeated turn-on of the IGBT into a short circuit with a high frequency may destroy the device.▪The inputs of the hybrid driver are sensitive to over-voltage. Voltages higher than V S +0,3V or below -0,3V may destroy these inputs. Therefore, control signal over-voltages exceeding the above values have to be avoided.▪The connecting leads between hybrid driver and the power module should be as short as possible (max. 20cm), the driver leads should be twisted.Further application supportLatest information is available at . For design support please read the SEMIKRON Application Manual Power Modules available at .General DescriptionThe Board 93 GB SKYPER® 42 is an adaptor board for the IGBT module SKiM® 93 (spring contact). The board is paralleling three channels so the SKiM module can be used in half bridge configuration. The board can be customized allowing adaptation and optimization to the used IGBT module.The switching characteristic of the IGBT can be influenced through user settings, e.g. changing turn-on and turn-off speed by variation of R Gon and R Goff. Furthermore, it is possible to adjust the monitoring level and blanking time for the DSCP (see Technical Explanations SKYPER® 42 R).Please note:This technical explanation is based on the Technical Explanations for SKYPER®42 R. Please read the Technical Explanations SKYPER® 42 R before using the Adaptor Board.Dimensions116 PIN ArraySetting Dynamic Short Circuit ProtectionThe Vce formula for the Vce monitoring is described in the technical explanation of SKYPER 42 R. Collector Series ResistanceDesignation Shape SettingR105 MiniMELF (SMD) R VCE*Factory setting: not equippedTOPR205 MiniMELF (SMD) R VCE *Factory setting: not equippedBOTAdaptation Gate ResistorsBoost CapacitorsEnvironmental conditionsPlease refer to the technical explanation of SKYPER 42 R for the environmental conditions.Mounting NotesDISCLAIMERSEMIKRON reserves the right to make changes withoutfurnished in this document is believed to be accurate and reliable. However, no representation or warranty is given and no liability is assumed with respect to the accuracy or use of such information. SEMIKRON does not assume any liability arising out of the application or use of any product or circuit described herein. Furthermore,。
【CN109883031A】导风组件、空气处理模块及落地式空调室内机【专利】
(19)中华人民共和国国家知识产权局(12)发明专利申请(10)申请公布号 (43)申请公布日 (21)申请号 201910167669.2(22)申请日 2019.03.07(71)申请人 广东美的制冷设备有限公司地址 528311 广东省佛山市顺德区北滘镇林港路(72)发明人 彭代杰 (74)专利代理机构 深圳市世纪恒程知识产权代理事务所 44287代理人 唐文波(51)Int.Cl.F24F 13/10(2006.01)F24F 1/0007(2019.01)(54)发明名称导风组件、空气处理模块及落地式空调室内机(57)摘要本发明公开一种导风组件、空气处理模块及落地式空调室内机,所述导风组件包括导风罩和导风板;所述导风罩设有导风入口和第一导风出口;所述导风板可翻转地安装在所述导风罩上,以打开或遮盖所述第一导风出口;所述导风板包括板主体及位于所述板主体一侧、并与所述导风罩转动连接的边板,所述边板与所述板主体之间形成有拐角。
本发明的导风组件,能够增强导风板的强度,以减少导风板变形或断裂等情况的发生,进而提高用户的使用体验。
权利要求书1页 说明书6页 附图6页CN 109883031 A 2019.06.14C N 109883031A权 利 要 求 书1/1页CN 109883031 A1.一种导风组件,其特征在于,所述导风组件包括:导风罩,所述导风罩设有导风入口和第一导风出口;以及导风板,所述导风板可翻转地安装在所述导风罩上,以打开或遮盖所述第一导风出口;所述导风板包括板主体及位于所述板主体一侧、并与所述导风罩转动连接的边板,所述边板与所述板主体之间形成有拐角。
2.如权利要求1所述的导风组件,其特征在于,所述导风罩还设有第二导风出口,所述导风板位于所述第一导风出口和所述第二导风出口之间,所述导风板还可打开或所述第二导风出口。
3.如权利要求2所述的导风组件,其特征在于,所述导风板可翻转地安装在所述第一导风出口和所述第二导风出口之间的拐角位置。
epeat标准
SAE AS4375是一个涉及到航空航天用流体系统和零部件的标准,主要涉及到接头端的设计和镁合金板材的退火和再结晶。
具体来说,该标准包括以下部分:* SAE AS4375A-1997:接头端 Flareless 设计标准* SAE AS4375-1992:接头端外螺纹无扩口设计标准* SAE AS4375B-2003:接头端 Flareless 设计标准* SAE AMS4375A-1951:镁合金板材和板材 AZ31X 退火* SAE AMS4375D-1962:镁合金板材 AZ31B-0* SAE AMS4375G-1978:镁合金板材 3.0Al 1.0Zn(AZ31B-0)* SAE AMS4375H-1984:镁合金板材和板材 3.0Al 1.0Zn(AZ31B-0)退火和再结晶(UNS M11311)* SAE AMS4375B-1958:镁合金板材 AZ31B-0* SAE AMS4375E-1966:镁合金板材 3.0Al 1.0Zn(AZ31B-0)* SAE AMS4375F-1968:镁合金板材 3.0Al 1.0Zn(AZ31B-0)* SAE AMS4375C-2017:板材和板材镁合金 3.0Al 1.0Zn 0.20Mn(AZ31B-O)退火和再结晶(UNS M11311)* SAE AS4375C-2003:无扩口接头端的设计标准* SAE AMS4375L-2011:退火和再结晶镁合金 3.0Al 1.0Zn 0.20Mn (AZ31B-0)薄片和板* SAE AMS4375J-1991:退火的镁合金薄板和板 3.0Al 1.0Zn 0.20Mn* SAE AMS4375K-2005:退火和重结晶的镁合金薄板和板材3.0Al 1.0Zn 0.20Mn (AZ31B-0)* SAE AMS4375J-1995:板材和板材,镁合金 3.0Al 1.0Zn 020Mn(AZ31B-0)退火和再结晶SAE AS4375是一个关于航空航天领域材料的标准,包括各种接头端设计和镁合金的退火和再结晶处理。
电热设备用云母板标准
电热设备用云母板标准
电热设备通常需要使用云母板来进行绝缘和隔热。
云母板是一种具有优良绝缘性能的材料,适用于高温和高压环境。
以下是一些常见的云母板标准:
1. GB/T 13024-2008《绝缘材料云母板》:该标准规定了云母板的分类、要求、试验方法以及标志、包装、运输和质量认证等内容。
2. IEC 60371-3-3《Insulating materials based on mica - Part 3: Specifications for individual materials - Sheet 3: Rigid mica sheets》:该标准为刚性云母板提供了技术规范,包括分类、尺寸、机械性能、热性能、电气性能等方面的要求。
3. ASTM D709-05《Standard Specification for Laminated Thermosetting Materials》:这是美国材料和试验协会制定的标准,适用于热固性层压材料,包括云母板。
在选择云母板时,可以根据电热设备的工作条件
和要求,参考以上标准,并与供应商进一步沟通,以确保选用合适的云母板。
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2.2 ASTM Publications
Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, .
AMS 2241
AMS 2249 AMS 2368 AMS 2750 AMS 2808 AMS 2809
Tolerances, Corrosion and Heat Resistant Steel, Iron Alloy, Titanium, and Titanium Alloy Bars and Wire Chemical Check Analysis Limits, Titanium and Titanium Alloys Sampling and Testing of Wrought Titanium Raw Materials, Except Forgings and Forging Stock Pyrometry Identification, Forgings Identification, Titanium and Titanium Alloy Wrought Products
Copyright © 2008 SAE International
All rights reserved. No part of this publication may be reproduced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording, or otherwise, without the prior written permission of SAE.
Solution and Precipitation Heat Treated
(Composition similar to R56620)
RATIONALE AMS 4979F results from a Five Year Review and update of this specification.
SAE
AMS 4979F
-2-
AMS 7498
Rings, Flash Welded, Titanium and Titanium Alloys
ARP982
Minimizing Stress-Corrosion Cracking in Wrought Titanium Alloy Products
ASTM E 8 ASTM E 1409
ASTM E 1447
ASTM E 1941 ASTM E 2371
Tension Testing of Metallic Materials Determination of Oxygen and Nitrogen in Titanium and Titanium Alloys by the Inert Gas Fusion Technique Determination of Hydrogen in Titanium and Titanium Alloys by the Inert Gas Fusion Thermal Conductivity/Infrared Detection Method Determination of Carbon in Refractory and Reactive Metals and Their Alloys Analysis of Titanium and Titanium Alloys by Atomic Emission Plasma Spectrometry
2.1 SAE Publications
Available from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or 724-776-4970 (outside USA), .
SAE reviews each technical report at least every five years at which time it may be reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions.
--`,`,````,``,`,,,,`,`,,``,,``-`-`,,`,,`,`,,`---
SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising therefrom, is the sole responsibility of the user.”
min
max
5.00
6.00
5.00
6.00
1.50
2.50
0.35
1.00ቤተ መጻሕፍቲ ባይዱ
0.35
1.00
--
0.05
--
0.20
--
0.04 (400 ppm)
--
0.015 (150 ppm)
--
0.005 ( 50 ppm)
--
0.10
--
0.40
remainder
3.1.1 Determination not required for routine acceptance. 3.1.2 No variation over maximum will be permitted for yttrium. 3.1.3 Check Analysis Composition variations shall meet the applicable requirements of AMS 2249. 3.1.4 When using AMS E 1447 for hydrogen determination, sample size may be as large as 0.35 gram.
1. SCOPE
1.1 Form
This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings, and of stock for forging or flash welded rings.
2. APPLICABLE DOCUMENTS
The issue of the following documents in effect on the date of the purchase order forms a part of this specification to the extent supplied herein. The supplier may work to a subsequent revision of a document unless a specific document issue is specified. When the referenced document has been cancelled and no superseding document has been specified, the last published issue of that document shall apply.
3. TECHNICAL REQUIREMENTS
3.1 Composition
Shall conform to the percentages by weight shown in Table 1; carbon shall be determined in accordance with ASTM E 1941, hydrogen in accordance with ASTM E 1447, oxygen and nitrogen in accordance with ASTM E 1409, and other elements in accordance with ASTM E 2371. Other analytical methods may be used if acceptable to the purchaser.
TABLE 1 - COMPOSITION
Element Aluminum Vanadium Tin Iron Copper Carbon Oxygen Nitrogen Hydrogen Yttrium (3.1.2) Other Elements, each (3.1.1) Other Elements, total (3.1.1) Titanium
1.2.1 Certain processing procedures and service conditions may cause these products to become subject to stresscorrosion cracking; ARP982 recommends practices to minimize such conditions.