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

    AECMA PREN 4673-003-2009 Aerospace series Inserts UNJ threads self-locking with self-broaching keys Part 003 Technical specification Edition P 1《航空航天系列.带自拉孔键的自锁UNJ螺纹插件.第003部分 技术规范..pdf

    • 资源ID:421591       资源大小:192.18KB        全文页数:24页
    • 资源格式: PDF        下载积分:5000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5000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。

    AECMA PREN 4673-003-2009 Aerospace series Inserts UNJ threads self-locking with self-broaching keys Part 003 Technical specification Edition P 1《航空航天系列.带自拉孔键的自锁UNJ螺纹插件.第003部分 技术规范..pdf

    1、ASD STANDARD NORME ASD ASD NORM prEN 4673-003 Edition P 1 December 2009 PUBLISHED BY THE AEROSPACE AND DEFENCE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATIONAvenue de Tervuren, 270 - B-1150 Brussels - Tel. 32 2 775 8126 - Fax. 32 2 775 8131 - www.asd-stan.orgICS: Descriptors: ENGLISH VERSION Aer

    2、ospace series Inserts, UNJ threads, self-locking, with self-broaching keys Part 003: Technical specification Srie arospatiale Douilles filetes, filetage UNJ, freinage interne, clavettes autobrochantes Partie 003 : Spcification technique Luft- und Raumfahrt Gewindeeinstze, UNJ-Gewinden, selbstsichern

    3、d, mit selbstrumenden Stiften Teil 003: Technische Lieferbedingungen This “Aerospace Series“ Prestandard has been drawn up under the responsibility of ASD-STAN (The AeroSpace and Defence Industries Association of Europe - Standardization). It is published for the needs of the European Aerospace Indu

    4、stry. It has been technically approved by the experts of the concerned Domain following member comments. Subsequent to the publication of this Prestandard, the technical content shall not be changed to an extent that interchangeability is affected, physically or functionally, without re-identificati

    5、on of the standard. After examination and review by users and formal agreement of ASD-STAN, it will be submitted as a draft European Standard (prEN) to CEN (European Committee for Standardization) for formal vote and transformation to full European Standard (EN). The CEN national members have then t

    6、o implement the EN at national level by giving the EN the status of a national standard and by withdrawing any national standards conflicting with the EN. Edition approved for publication 15 December 2009 Comments should be sent within six months after the date of publication to ASD-STAN Mechanical

    7、Domain Copyright 2009 by ASD-STAN Copyright ASD-STAN Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4673-003:2009 (E) 2 Contents Page Foreword2 1 Scope 3 2 Normative references 3 3 Terms and definitions .4 4 Quality as

    8、surance6 5 Requirements.7 Annex A (normative) Definition of test block 17 Annex B (normative) Assembly for rotational resistance test 18 Annex C (normative) Axial tensile strength test. 19 Annex D (normative) Assembly for reusability test 21 Annex E (normative) “GO“ gauge for inspection of the posit

    9、ion of the keys 23 Foreword This standard was reviewed by the Domain Technical Coordinator of ASD-STANs Mechanical Domain. After inquiries and votes carried out in accordance with the rules of ASD-STAN defined in ASD-STANs General Process Manual, this standard has received approval for Publication.

    10、Copyright ASD-STAN Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4673-003:2009 (E) 3 1 Scope This standard specifies the characteristics, qualification and acceptance requirements for self-locking inserts, self-broach

    11、ing keys with UNJ threads, for aerospace applications. It is applicable whenever referenced. 2 Normative references The following referenced documents are indispensable for the application of this document. For dated references, only the edition cited applies. For undated references, the latest edit

    12、ion of the referenced document (including any amendments) applies. EN 2638, Aerospace series Aluminium alloy 2024-T3 Extruded bar and section 1,2 mm (a or D) 150 mm with coarse peripheral grain control 1)EN 4673-001, Aerospace series Inserts, UNJ threads, self-locking, self-broaching keys Part 001:

    13、Installation and removal procedure 1)EN 4673-002, Aerospace series Inserts, UNJ threads, self-locking, self-broaching keys Part 002: Design standard 1)EN 9133, Aerospace series Quality management systems Qualification Procedure for Aerospace Standard Parts ISO 2859-1, Sampling procedures for inspect

    14、ion by attributes Part 1: Sampling schemes indexed by acceptance quality limit (AQL) for lot-by-Iot inspection ISO 3161, UNJ threads General requirements and limit dimensions ISO 3452, Non-destructive testing Penetrant inspection General principles ISO 4288, Geometrical Product Specifications (GPS)

    15、Surface texture: Profile method Rules and procedures for the assessment of surface texture ASTM-E112-96, Standard Test Methods for Determining Average Grain Size 2)1) Published as ASD-STAN Prestandard at the date of publication of this standard. 2) Published by: American Society for Testing and Mate

    16、rials (ASTM), 1916, Race Street, Philadelphia, PA 19103, USA. Copyright ASD-STAN Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4673-003:2009 (E) 4 3 Terms and definitions For the purposes of this European Standard, th

    17、e following terms and definitions apply. 3.1 batch quantity of finished parts, of the same type and same diameter, produced from the same material obtained from the same melt, manufactured in the course of the same production cycle, following the same manufacturing route and having undergone all the

    18、 relevant heat treatments and surface treatments 3.2 Surface discontinuities 3.2.1 crack rupture in the material which may extend in any direction and which may be intercrystalline or transcrystalline in character 3.2.2 seam open surface defect 3.2.3 lap surface defect caused by folding over metal f

    19、ins or sharp corners and then rolling or forging them into the surface 3.2.4 inclusions metallic or non-metallic particles originating from the manufacturing process. These particles may be isolated or arranged in strings. 3.2.5 test temperature ambient temperature, unless otherwise specified 3.2.6

    20、simple random sampling the taking of n items from a population of N items in such a way that all possible combinations of n items have the same probability of being chosen 3.2.7 critical defect a defect that, according to judgement and experience, is likely to result in hazardous or unsafe condition

    21、s for individuals using, maintaining, or depending upon the considered product, or that is likely to prevent performance of the function of a major end item 3.2.8 major defect a defect other than critical, that is likely to result in a failure or to reduce materially the usability of the considered

    22、product for its intended purpose Copyright ASD-STAN Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4673-003:2009 (E) 5 3.2.9 minor defect a defect that is not likely to reduce materially the usability of the considered

    23、 product for its intended purpose, or that is a departure from established specification having little bearing on the effective use or operation of this product 3.2.10 sampling plan a plan according to which one or more samples are taken in order to obtain information and possibly to reach 3.2.11 li

    24、miting quality (LQ10) in a sampling plan, the quality limit which corresponds to a specified 10 % probability of acceptance NOTE 1 It is the limiting lot quality characteristic that the consumer is willing to accept with a low probability that a lot of this quality would occur. NOTE 2 For the purpos

    25、es of this Standard, the limiting quality quoted in Table 4 corresponds to a probability of acceptance of 10 %. 3.2.12 acceptance quality limit (AQL) a quality limit which in a sampling plan corresponds to a specified but relatively high probability of acceptance NOTE It is the maximum per cent defe

    26、ctive (or the maximum number of defects per hundred units) that, for purposes of sampling inspection can be considered satisfactory as a process average. 3.2.13 finished insert an insert ready for use, inclusive of any possible treatments and/or surface coatings, as specified in the definition docum

    27、ent 3.2.14 definition document document specifying all the requirements for finished inserts 3.2.15 self-locking torque the torque to be applied to the associated bolt to maintain movement of rotation in relation to the part, the assembly being under no axial load and the insert locking zone being c

    28、ompletely engaged with the bolt (minimum protrusion of two pitches, including the end chamfer) 3.2.16 seating torque the tightening torque to be applied to the insert or bolt to introduce or to increase the axial load in the assembly 3.2.17 unseating torque the untightening torque to be applied to t

    29、he insert or bolt to reduce or remove the axial load in the assembly Copyright ASD-STAN Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4673-003:2009 (E) 6 3.2.18 breakaway torque the torque required to start unscrewing

    30、 the insert or the bolt from the associated part, with the insert locking device still fully engaged on the bolt, but after the axial load in the assembly has been removed by unscrewing half a turn followed by a halt in rotational movement 4 Quality assurance 4.1 Qualification EN 9133 Qualification

    31、inspections and tests (requirements, methods, numbers of inserts with self-broaching keys) are specified in Table 1. They shall be carried out on: each type and diameter of inserts; 39 inserts selected from a single batch by simple random sampling. The test programme may possibly be reduced, or the

    32、qualification be granted without inspection or testing: Any such decision shall be based on the results obtained on similar types and diameters of inserts provided that the design and manufacturing conditions are identical. Table 2 indicates the allocation of insert samples for the inspections and t

    33、ests. 4.2 Acceptance 4.2.1 Purpose The purpose of acceptance inspections and tests is to check, as simply as possible, by a method representative of actual use conditions, with the uncertainty inherent to statistical sampling, that the inserts constituting the batch satisfy the requirements of this

    34、standard. 4.2.2 Conditions Acceptance inspections and tests (requirements, methods, numbers of inserts) are specified in Table 1. They shall be carried out on each batch. Inserts from the batch to be tested shall be selected by simple random sampling. Each insert may be submitted to several inspecti

    35、ons or tests. If a more stringent inspection is deemed necessary, all or part of the qualification inspections and tests may be performed during the acceptance inspections and tests. In this case, the number of inserts submitted to these inspections and tests is the same as that submitted for qualif

    36、ication inspection and tests. 4.2.3 Responsibility Acceptance inspections and tests shall be carried out by the manufacturer, or under his responsibility. 4.2.4 Inspection and test report A test report showing actual numerical values shall be provided if specified in the purchase order. Copyright AS

    37、D-STAN Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4673-003:2009 (E) 7 5 Requirements See Table 1. Table 1 Technical requirements and test methods Clause Characteristic Requirement Inspection and test method Q/A aSa

    38、mple size Q 5.1 Material In accordance with the definition document. Chemical analysis or certificate of conformity issued by the manufacturer of the semi-finished product. A Q 39 5.2 Dimensions, tolerances and tolerances of form and position In accordance with the definition document. A “GO” inspec

    39、tion gauge is to be fitted on the insert keys. On completion of this inspection, the keys must neither be bent nor moved. Standard gauging. See Annex E. A Tables 3 and 4 5.3 Manufacturing 5.3.1 Process Insert threads may be produced by machining or forming. Manufacturing method shall be indicated on

    40、 test report. The heat treatment medium or atmosphere shall not cause any surface contamination. Calibration of the heat treatment equipment shall be confirmed. Any scale which will not be removed by subsequent machining shall be removed by abrasive blasting with an appropriate equipment. Visual exa

    41、mination. 5.3.2 Heat treatment The material shall be heat treated in accordance with the material specification defined in the definition document. Examination of the heat treatment specification. continued Copyright ASD-STAN Provided by IHS under license with AECMA Not for ResaleNo reproduction or

    42、networking permitted without license from IHS-,-,-prEN 4673-003:2009 (E) 8 Table 1 (continued) Clause Characteristic Requirement Inspection and test method Q/A aSample size 5.3.3 Q 39 Thread deformation (form out-of round) Threads in the locking zone may be deformed in any manner provided that the i

    43、nsert meets the requirements of this standard. The finished inserts shall allow the “GO“ thread plug gauge to enter a minimum of three turns, when gauged from the installation side before engagement in the locking zone. Standard gauging. A Tables 3 and 4 Q 3 5.3.4 Surface roughness In accordance wit

    44、h the definition document. ISO 4288. A Tables 3 and 4 Q 36 A Tables 3 and 4 5.3.5 Surface coating In accordance with the definition document. See applicable coating standard. A Table 6 5.4 Mechanical properties Q 5 5.4.1 Installation requirement The screwing of insert shall be possible freely by han

    45、d. After testing, the inserts shall show no signs of: buckling and/or incomplete fitting of the keys, deformation of the internal thread of the insert caused by keys installation. Inserts shall be installed into test block (see Annex A, normative) in accordance with EN 4673-001. Use a tool specified

    46、 in accordance with EN 4673-001. Visual examination at a suitable magnification of 10 to 20. The recorded hardness of the test blocks must be indicated in the test report. A Table 5 5.4.1.1 into test block in aluminium See 5.4.1. See 5.4.1. Q 14 5.4.1.2 into test block in corrosion resisting steel S

    47、ee 5.4.1. See 5.4.1. Q 16 5.4.1.3 into test block in titanium alloy See 5.4.1. See 5.4.1. Q 6 continued Copyright ASD-STAN Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4673-003:2009 (E) 9 Table 1 (continued) Clause C

    48、haracteristic Requirement Inspection and test method Q/A aSample size 5.4.2 Rotational resistance Q 5 5.4.2.1 into test block in aluminium alloy Inserts shall withstand the torque specified in Table B.1 without rotation. Inserts shall be installed in accordance with 5.4.1.1. The installed inserts shall be tested in a counter clockwise direction as shown in Annex B (normative). Q 5 5.4.2.2 into test block in corrosion resisting steel dSee 5.4.2.1. Inserts shall be installed into test block in corrosion resisting steel (see Annex A). Test method, see 5.4.2.1. Q 6 c5.4.3 Axial loadbInse


    注意事项

    本文(AECMA PREN 4673-003-2009 Aerospace series Inserts UNJ threads self-locking with self-broaching keys Part 003 Technical specification Edition P 1《航空航天系列.带自拉孔键的自锁UNJ螺纹插件.第003部分 技术规范..pdf)为本站会员(eventdump275)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