SAE AS 93E-2013 Cones Rear Propeller Hub《螺旋桨毂后锥体》.pdf

上传人:fuellot230 文档编号:1025862 上传时间:2019-03-21 格式:PDF 页数:2 大小:314.30KB
下载 相关 举报
SAE AS 93E-2013 Cones Rear Propeller Hub《螺旋桨毂后锥体》.pdf_第1页
第1页 / 共2页
SAE AS 93E-2013 Cones Rear Propeller Hub《螺旋桨毂后锥体》.pdf_第2页
第2页 / 共2页
亲,该文档总共2页,全部预览完了,如果喜欢就下载吧!
资源描述

1、 AEROSPACE STANDARD CONES, REAR, PROPELLER HUB AS93Copyright 2013 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

2、 prior written permission of SAE. TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: +1 724-776-4970 (outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org ISSUED 1943-01REVISED 1953-01 NONCURRENT 1984-02 REAFFIRMEDNONCURRENT 2006-05 S

3、TABILIZED 2013-03THIRD ANGLE PROJECTION CUSTODIAN: E-25 REV.E FEDERAL SUPPLY CLASS AS93 REV. E PROCUREMENT SPECIFICATION: NONESAE Technical Standards Board Rules provide that: “This report ispublishedby SAE toadvance thestate of technicalandengineering sciences. Theuse ofthis report is entirely volu

4、ntary, andits applicability and suitability forany particular use,including any patent infringement arising therefrom, isthe soleresponsibilityofthe user.”SAE reviews eachtechnicalreport at least every five years at which time itmay berevised, reaffirmed, stabilized, orcancelled. SAE invites yourwri

5、ttencomments andsuggestions. SAE values your input. To provide feedbackon this Technical Report, please visit http:/www.sae.org/technical/standards/AS93E RATIONALE THIS NONCURRENT STANDARD HAS BEEN STABILIZED. STABILIZED NOTICE THIS DOCUMENT HAS BEEN DECLARED “STABILIZED“ BY THE SAE E-25 GENERAL STA

6、NDARDS FOR AEROSPACE AND PROPULSION SYSTEMS COMMITTEE AND WILL NO LONGER BE SUBJECTED TO PERIODIC REVIEWS FOR CURRENCY. USERS ARE RESPONSIBLE FOR VERIFYING REFERENCES AND CONTINUED SUITABILITY OF TECHNICAL REQUIREMENTS. NEWER TECHNOLOGY MAY EXIST. Copyright SAE International Provided by IHS under li

7、cense with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AEROSPACE STANDARD AS93 SHEET 1 OF 1 REV. E CONES, REAR, PROPELLER HUB Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-

展开阅读全文
相关资源
猜你喜欢
  • SAE AMS 4574F-2017 Nickel-Copper Alloy Corrosion Resistant Tubing Seamless 67Ni - 31Cu Annealed (UNS N04400).pdf SAE AMS 4574F-2017 Nickel-Copper Alloy Corrosion Resistant Tubing Seamless 67Ni - 31Cu Annealed (UNS N04400).pdf
  • SAE AMS 4590C-2009 Extrusions Nickel-Aluminum Bronze Martensitic 78 5Cu C 10 5Al C 5 1Ni C 4 8Fe Quenched and Tempered (TQ50) (UNS C63020)《78 5Cu-10 5Al-5 1Ni-4 8Fe溶液热处理和淬火(TQ50)镍铝.pdf SAE AMS 4590C-2009 Extrusions Nickel-Aluminum Bronze Martensitic 78 5Cu C 10 5Al C 5 1Ni C 4 8Fe Quenched and Tempered (TQ50) (UNS C63020)《78 5Cu-10 5Al-5 1Ni-4 8Fe溶液热处理和淬火(TQ50)镍铝.pdf
  • SAE AMS 4595-2011 Copper Nickel Tin Alloy Plate 77Cu C 15Ni C 8Sn Solution Annealed and Spinodal Hardened (TX 00) (UNS C72900)《固溶退火和亚稳态硬化工艺制备的77Cu-15Ni-8Sn铜镍锡合金板(TX 00)》.pdf SAE AMS 4595-2011 Copper Nickel Tin Alloy Plate 77Cu C 15Ni C 8Sn Solution Annealed and Spinodal Hardened (TX 00) (UNS C72900)《固溶退火和亚稳态硬化工艺制备的77Cu-15Ni-8Sn铜镍锡合金板(TX 00)》.pdf
  • SAE AMS 4596B-2010 Copper Nickel Tin Alloy Bars and Rods 77Cu C 15Ni C 8Sn Solution Annealed and Spinodal Hardened (TX 00) (UNS C72900)《固溶煅烧和调幅硬化(TX00)的77Cu15Ni8Sn铜镍锡合金条材 棒材和管材》.pdf SAE AMS 4596B-2010 Copper Nickel Tin Alloy Bars and Rods 77Cu C 15Ni C 8Sn Solution Annealed and Spinodal Hardened (TX 00) (UNS C72900)《固溶煅烧和调幅硬化(TX00)的77Cu15Ni8Sn铜镍锡合金条材 棒材和管材》.pdf
  • SAE AMS 4597A-2011 Copper-Nickel-Tin Alloy Bars and Rods 77Cu - 15Ni - 8Sn Solution Annealed Cold Finished and Spinodal Hardened (TX TS) (UNS C72900)《固溶退火 冷加工和亚稳界线淬硬(TX TS)的含77Cu 1.pdf SAE AMS 4597A-2011 Copper-Nickel-Tin Alloy Bars and Rods 77Cu - 15Ni - 8Sn Solution Annealed Cold Finished and Spinodal Hardened (TX TS) (UNS C72900)《固溶退火 冷加工和亚稳界线淬硬(TX TS)的含77Cu 1.pdf
  • SAE AMS 4598A-2012 Copper Nickel Tin Alloy Mechanical Tube 77Cu - 15Ni - 8Sn Solution Annealed and Spinodal Hardened (TX 00) (UNS C72900)《固溶退火和旋接线硬化(TX 00)77Cu 15Ni 8Sn铜镍矿锡合金机械管》.pdf SAE AMS 4598A-2012 Copper Nickel Tin Alloy Mechanical Tube 77Cu - 15Ni - 8Sn Solution Annealed and Spinodal Hardened (TX 00) (UNS C72900)《固溶退火和旋接线硬化(TX 00)77Cu 15Ni 8Sn铜镍矿锡合金机械管》.pdf
  • SAE AMS 4599-2011 Aluminum Alloy Sheet and Plate 6 3Cu - 0 30Mn - 0 06Ti - 0 10V - 0 18Zr Solution and Precipitation Heat Treated (2219 -T81 -T851)《溶解沉淀热处理工艺制备的6 3Cu-0 30Mn-0 06Ti-.pdf SAE AMS 4599-2011 Aluminum Alloy Sheet and Plate 6 3Cu - 0 30Mn - 0 06Ti - 0 10V - 0 18Zr Solution and Precipitation Heat Treated (2219 -T81 -T851)《溶解沉淀热处理工艺制备的6 3Cu-0 30Mn-0 06Ti-.pdf
  • SAE AMS 4599A-2017 Aluminum Alloy Sheet and Plate 6 3Cu - 0 30Mn - 0 06Ti - 0 10V - 0 18Zr Solution and Precipitation Heat Treated (2219 -T81 -T851) (UNS A92219).pdf SAE AMS 4599A-2017 Aluminum Alloy Sheet and Plate 6 3Cu - 0 30Mn - 0 06Ti - 0 10V - 0 18Zr Solution and Precipitation Heat Treated (2219 -T81 -T851) (UNS A92219).pdf
  • SAE AMS 4600-2011 Aluminum Alloy Sheet and Plate 6 3Cu - 0 30Mn - 0 06Ti - 0 10V - 0 18Zr Solution Heat Treated Cold Worked (8%) and Naturally Aged (2219 -T37) (UNS A92219)《固溶热处理 冷.pdf SAE AMS 4600-2011 Aluminum Alloy Sheet and Plate 6 3Cu - 0 30Mn - 0 06Ti - 0 10V - 0 18Zr Solution Heat Treated Cold Worked (8%) and Naturally Aged (2219 -T37) (UNS A92219)《固溶热处理 冷.pdf
  • 相关搜索

    当前位置:首页 > 标准规范 > 国际标准 > 其他

    copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
    备案/许可证编号:苏ICP备17064731号-1