欢迎来到麦多课文档分享! | 帮助中心 海量文档,免费浏览,给你所需,享你所想!
麦多课文档分享
全部分类
  • 标准规范>
  • 教学课件>
  • 考试资料>
  • 办公文档>
  • 学术论文>
  • 行业资料>
  • 易语言源码>
  • ImageVerifierCode 换一换
    首页 麦多课文档分享 > 资源分类 > PDF文档下载
    分享到微信 分享到微博 分享到QQ空间

    SAE AS 7949B-2004 Bearings Ball Airframe Antifriction General Standard for《飞机机架抗摩擦滚珠轴承的一般标准》.pdf

    • 资源ID:1025344       资源大小:246.56KB        全文页数:24页
    • 资源格式: PDF        下载积分:10000积分
    快捷下载 游客一键下载
    账号登录下载
    微信登录下载
    二维码
    微信扫一扫登录
    下载资源需要10000积分(如需开发票,请勿充值!)
    邮箱/手机:
    温馨提示:
    如需开发票,请勿充值!快捷下载时,用户名和密码都是您填写的邮箱或者手机号,方便查询和重复下载(系统自动生成)。
    如需开发票,请勿充值!如填写123,账号就是123,密码也是123。
    支付方式: 支付宝扫码支付    微信扫码支付   
    验证码:   换一换

    加入VIP,交流精品资源
     
    账号:
    密码:
    验证码:   换一换
      忘记密码?
        
    友情提示
    2、PDF文件下载后,可能会被浏览器默认打开,此种情况可以点击浏览器菜单,保存网页到桌面,就可以正常下载了。
    3、本站不支持迅雷下载,请使用电脑自带的IE浏览器,或者360浏览器、谷歌浏览器下载即可。
    4、本站资源下载后的文档和图纸-无水印,预览文档经过压缩,下载后原文更清晰。
    5、试题试卷类文档,如果标题没有明确说明有答案则都视为没有答案,请知晓。

    SAE AS 7949B-2004 Bearings Ball Airframe Antifriction General Standard for《飞机机架抗摩擦滚珠轴承的一般标准》.pdf

    1、 AEROSPACE STANDARD (R) Bearings, Ball, Airframe, Antifriction, General Standard for 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

    2、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.

    3、Copyright 2004 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. TO PLACE A DOCUME

    4、NT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: 724-776-4970 (outside USA) Fax: 724-776-0790 Email: custsvcsae.org SAE WEB ADDRESS: http:/www.sae.org Issued 1998-04 Revised 2004-08 Superseding AS7949A AS7949 REV.B NOTICE This document includes cadmium as a plating material. The use of cadmi

    5、um has been restricted and/or banned for use in many countries due to environmental and health concerns. The user should consult with local officials on applicable health and environmental regulations regarding its use. 1. SCOPE: This standard covers ball bearings in the -65 to +350 F temperature ra

    6、nge as specified on the applicable drawing standards. 2. APPLICABLE DOCUMENTS: The following publications form a part of this document to the extent specified herein. The latest issue of SAE publications shall apply. The applicable issue of other publications shall be the issue in effect on the date

    7、 of the purchase order. In the event of conflict between the text of this document and references cited herein, the text of this document takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained. Copyright SAE Inter

    8、national Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE AS7949 Revision B - 2 - 2.1 SAE Publications: Available from SAE, 400 Commonwealth Drive, Warrendale, PA 15096-0001. AMS 2417 Plating, Zinc-Nickel Alloy AMS 3652 Poly

    9、tetrafluoroethylene (PTFE) Film Non-Critical Grade AMS 3666 Polytetrafluoroethylene (PTFE) Sheet, Glass Cloth Reinforced AMS 6440 Steel, Bars, Forgings, and Tubing 1.45cr (0.98-1.10c) (SAE 52100) Premium Aircraft-Quality, Consumable Electrode Vacuum Melted AMS 6444 Steel Bars, Forgings, and Tubing,

    10、1.45cr (0.98 1.10c) for Bearing Applications AMS-QQ-P-416 Plating, Cadmium (Electro deposited) AS21428 Bearing, Ball, Airframe, Anti-friction, Extra Light Duty, Precision AS21443 Bearing, Ball, Airframe, Anti-friction, Pulley Type AS27640 Bearing, Ball, Airframe, Anti-friction, Heavy Duty AS27641 Be

    11、aring, Ball, Airframe, Anti-friction, Intermediate Duty AS27642 Bearing, Ball, Airframe, Extra Light Duty AS27643 Bearing, Ball, Airframe, Anti-friction, Self-aligning, Double Row, Heavy Duty AS27644 Bearing, Ball, Airframe, Anti-friction, Double Row, Heavy Duty AS27645 Bearing, Ball, Airframe, Anti

    12、-friction, Self-aligning, Light and Heavy Duty AS27646 Bearing, Ball, Airframe, Anti-friction, Extra Light Duty AS27647 Bearing, Ball, Airframe, Anti-friction, Extra Wide, Double Row, Intermediate Duty AS27648 Bearing, Ball, Airframe, Anti-friction, Externally Self-aligning, Extra Light Duty AS27649

    13、 Bearing, Ball, Airframe, Anti-friction, Intermediate Duty Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE AS7949 Revision B - 3 - 2.2 ASTM Publications: Available from ASTM, 100 Barr Harbor, Wes

    14、t Conshohocken, PA 19428-2959. ASTM E 1444 Standard Practice for Magnetic Particle Inspection ASTM F 2215 Standard Specification for Balls, Bearings, Ferrous and Nonferrous for Use in Bearings, Valves, and Bearing Applications 2.3 ASME Publications: Available from ASME, 22 Law Drive, Box 2900, Fairf

    15、ield, NJ 07007-2900. ASME B46.1 Surface Texture (Surface Roughness, Waviness and Lay) ANSI/ABMA STD 4 Gauging/Tolerancing Practices 2.4 ISO Publications: Available from ANSI, 25 West 43rd Street, New York, NY 10036-8002. ISO 12103-1 Arizona Road Dust 2.5 U.S. Government Publications: Available from

    16、Standardization Documents Order Desk, Building 4D, 700 Robbins Avenue, Philadelphia, PA 19111-5094. Electronic copies may be obtained from http:/assist.daps.mil/quicksearch MIL-DTL-197 Packaging of Bearings, Antifriction, Associated Parts and Subassemblies MIL-PRF-23827 Grease, Aircraft and Instrume

    17、nt, Gear and Actuator Screw MIL-PRF-81322 Grease, Aircraft, General Purpose, Wide Temperature Range MIL-STD-129 Standard Practice for Military Marking MIL-STD-130 Identification Marking of U.S. Military Property MIL-STD-2073-1 DoD Standard Practice for Military Packaging Copyright SAE International

    18、Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE AS7949 Revision B - 4 - 3. REQUIREMENTS: 3.1 Drawing Standards: The individual item requirements shall be as specified herein and in accordance with the applicable drawing sta

    19、ndards (see 2.1). In the event of any conflict between the requirements of this general standard and the drawing standards, the latter shall govern. 3.2 Qualification: The bearings furnished under this standard shall be products that are authorized by the qualifying activity for listing on the appli

    20、cable Qualified Products List (QPL-AS7949) before contract award (see 4.3 and 6.3). 3.2.1 Product Change: Any change in product design, including raceway geometry or dimensions, nominal rolling element dimensions, rolling element quantity, seals, materials, or plant location shall be reported to the

    21、 qualifying activity and may require re-qualification of the product to an extent determined by the qualifying activity. Any other specific changes that must be brought to the qualifying activitys attention shall be identified in the qualification notification letter. 3.2.2 Product Manufacture: The

    22、bearing manufacturer shall be capable of performing the preponderance of manufacturing operations in-house, but may subcontract these operations at its option. Component inspection shall be performed at the plant listed on the QPL. If manufacturing operations are performed in more than one plant, th

    23、e manufacturers additional plant(s) shall be reported to the qualifying activity. The manufacturer is responsible for meeting all requirements of the specification and for the quality of the end product, whether it is manufactured totally in-house or some of the operations are performed by a subcont

    24、ractor. Inherent in the responsibility for the end product is the responsibility to verify that the subcontractors processes meet specification requirements. A change in subcontractor need not be reported to the qualifying activity unless specifically identified in the qualification notification let

    25、ter. NOTE: Bearings partly or completely manufactured in foreign countries shall be subject to the laws and procurement regulations pertaining to acquisition of foreign-made products. 3.3 Materials: Material used to manufacture the bearing and its components shall conform to the applicable drawing s

    26、tandard. The lubricant used shall be qualified to the applicable grease specification (see 3.12). Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE AS7949 Revision B - 5 - 3.4 Bearing Assembly: The

    27、 bearing assembly shall be as specified in the applicable drawing standard, but the details of the working parts shall be optional. Only factory-new bearings shall be furnished. 3.4.1 Out-of-Roundness: The maximum and minimum bore and outside diameter readings shall be within the out-of-roundness li

    28、mits specified on the applicable drawing standard. The average bore and outer diameter measurements shall be within the tolerances specified for dimensions “B“ and “D“ of the applicable drawing standard. Bearings shall be tested in accordance with 4.5.1.1. 3.4.2 Seals: Seals shall prevent the entran

    29、ce of contaminants and retain the lubricant. Seals shall be securely attached to the outer ring. All relative motion shall be between the seal and the inner ring. Removable design seals, which could lead to unintended bearing disassembly, shall not be permitted on internal self-aligned bearings. 3.4

    30、.2.1 Seal Test (Grease Retention): The seals shall be capable of withstanding the test requirements as specified in 4.5.2.1 without failure. Grease conforming to MIL-PRF-81322 shall be injected into the bearing. The amount of grease shall be measured by weight and shall be at least 80% of the minimu

    31、m theoretical volume within the bearing. Not less than 25% of the bearing lubricant by weight shall be retained in the bearing at the end of the test. 3.4.2.2 Dust Test: After completion of the dust test specified in 4.5.2.2, the tested bearings shall meet the following requirements: a. Radial clear

    32、ance shall not increase more than 50% or 0.0002 in over the pretest value, whichever is greater. b. Starting torque shall not increase more than 100% or 2 in-oz over the pretest value, whichever is greater. 3.4.2.3 Seal Retention: For bearings of internal self-aligning design, the seal retention sha

    33、ll be tested in accordance with 4.5.2.3. The seals shall meet the minimum torque to dislodge the seal as specified on the applicable drawing standard. Any seal that is damaged or dislodged prior to achieving the minimum torque value shall be considered to have failed. 3.5 Interchangeability: All par

    34、ts having the same MS part number shall be functionally and dimensionally interchangeable. Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE AS7949 Revision B - 6 - 3.6 Strength Performance: 3.6.1

    35、Radial Strength: 3.6.1.1 Radial Limit Load: The bearings shall meet the radial limit loads specified on the applicable drawing standard when tested in accordance with 4.5.3.1. If the smoothness of operation of the bearings has lessened perceptibly, they shall be considered to have failed. 3.6.1.2 Ra

    36、dial Static Ultimate Load: The minimum radial static ultimate strength shall be 1.5 times the radial limit load value specified on the applicable drawing standard when tested in accordance with 4.5.3.2. Bearings shall be capable of being turned by hand and shall not have broken or cracked parts afte

    37、r applying 1.5 times the applicable radial limit load. After the test, all rings and balls shall pass a magnetic particle inspection per ASTM E 1444. 3.6.1.3 Radial Dynamic Load: The bearing shall have a radial dynamic load rating of not less than the value specified on the applicable drawing standa

    38、rd when tested in accordance with 4.5.3.3. The bearing shall have an L50life of 10,000 cycles, except for bearings covered by AS21443 which shall have an L10of 3,500 cycles. A bearing shall be considered to have failed when there is any evidence of the following defects: (1) wear of the outer racewa

    39、y greater than 0.002 in; (2) 0.002 in radial displacement during testing; (3) spalling or cracking detected by magnetic particle inspection per ASTM E 1444; or (4) fracture of any component. 3.6.2 Axial Strength: 3.6.2.1 Axial Limit Load: The bearings shall meet the axial limit loads specified on th

    40、e applicable drawing standard when tested in accordance with 4.5.4.1. If the smoothness of operation of the bearings has lessened perceptibly, they shall be considered to have failed. 3.6.2.2 Axial Static Ultimate Load: The axial ultimate strength shall be 1.5 times the axial load value specified on

    41、 the applicable drawing standard when tested in accordance with 4.5.4.2. Bearings shall be capable of being turned by hand and shall have no cracks or broken parts after applying 1.5 times the applicable axial load. After the test, all rings and balls shall pass a magnetic particle inspection per AS

    42、TM E 1444. 3.7 Internal Clearance: Radial and axial internal clearance shall conform to the applicable drawing standard when measured in accordance with 4.5.5. Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from

    43、 IHS-,-,-SAE AS7949 Revision B - 7 - 3.8 Plating (Except for the AS27649 Bearings): When tested in accordance with 4.5.6, all external surfaces of the bearing excluding the inner ring bore and chamfer, seal retainers, and seals, shall be cadmium plated per AMS-QQ-P-416, Type I, Class 2 or zinc-nicke

    44、l plated in accordance with AMS 2417, Type 2. The plating thickness shall be 0.0003 to 0.0006 in. The plating thickness of the bore chamfers shall be a maximum of 0.0006 in. Plating on the ball loading slot is optional. 3.9 Surface Roughness: The surface roughness shall be measured in accordance wit

    45、h 4.5.7, and shall conform to the values on the applicable drawing standard. 3.10 Hardness: The rings and balls shall be tested in accordance with 4.5.8. The hardness shall be in accordance with values on the applicable drawing standard. 3.11 Radial and Lateral Eccentricity: Non-self-aligning bearin

    46、gs shall be tested in accordance with 4.5.9. The eccentricity values shall be in accordance with the limits specified in the applicable drawing standard. 3.12 Lubrication: The bearings shall be packed with grease qualified to MIL-PRF-81322 for -65 to 350 F operating range or MIL-PRF-23827 for -65 to

    47、 250 F operating range. The bearings shall be filled with lubricant not less than 80% by volume, and shall be cleaned before the lubricant is injected into the bearings. Bearings shall not have been lubricated more than 36 months prior to the date of delivery of the bearings under contract or order.

    48、 The bore of all bearings and the outside diameter of the outer ring and the inside diameter of the self-aligning ring of the externally self-aligning bearing shall be coated with the same grease that is packed in the bearing. Inspection of lubricant shall be in accordance with 4.5.10. 3.13 Dimensio

    49、nal Stability: Bearings shall exhibit dimensional stability by not changing more than 0.0001 in per inch diameter from the last reading when tested in accordance with 4.5.11. 3.14 Starting Torque: Starting torque shall be within the allowable values specified in the applicable drawing standard. The amount of torque required to begin rotation of the bearing shall be measured in accordance with 4.5.12. Copyright SAE International Provided by


    注意事项

    本文(SAE AS 7949B-2004 Bearings Ball Airframe Antifriction General Standard for《飞机机架抗摩擦滚珠轴承的一般标准》.pdf)为本站会员(李朗)主动上传,麦多课文档分享仅提供信息存储空间,仅对用户上传内容的表现方式做保护处理,对上载内容本身不做任何修改或编辑。 若此文所含内容侵犯了您的版权或隐私,请立即通知麦多课文档分享(点击联系客服),我们立即给予删除!




    关于我们 - 网站声明 - 网站地图 - 资源地图 - 友情链接 - 网站客服 - 联系我们

    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 

    收起
    展开