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本文(EN 3005-2004 en Aerospace series - Nuts self-locking MJ threads in heat resisting nickel base alloy NI-PH1302 (Waspaloy) silver plated or uncoated - Classification 1 210 MPa (at am.pdf)为本站会员(ownview251)主动上传,麦多课文库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库(发送邮件至master@mydoc123.com或直接QQ联系客服),我们立即给予删除!

EN 3005-2004 en Aerospace series - Nuts self-locking MJ threads in heat resisting nickel base alloy NI-PH1302 (Waspaloy) silver plated or uncoated - Classification 1 210 MPa (at am.pdf

1、BRITISH STANDARD AEROSPACE SERIES BS EN 3005:2004 Nuts, self-locking, MJ threads, in heat resisting nickel base alloy NI-PH1302 (Waspaloy), silver plated or uncoated Classification: 1210MPa (at ambient temperature)/730 C Technical specification The European Standard EN 3005:2004 has the status of a

2、British Standard ICS 49.030.30 BS EN 3005:2004 This British Standard was published under the authority of the Standards Policy and Strategy Committee on 6 January 2005 BSI 6 January 2005 ISBN 0 580 45186 0 National foreword This British Standard is the official English language version of EN 3005:20

3、04. The UK participation in its preparation was entrusted to Technical Committee ACE/12, Aerospace fasteners and fastening systems, which has the responsibility to: A list of organizations represented on this committee can be obtained on request to its secretary. Cross-references The British Standar

4、ds which implement international or European publications referred to in this document may be found in the BSI Catalogue under the section entitled “International Standards Correspondence Index”, or by using the “Search” facility of the BSI Electronic Catalogue or of British Standards Online. This p

5、ublication does not purport to include all the necessary provisions of a contract. Users are responsible for its correct application. Compliance with a British Standard does not of itself confer immunity from legal obligations. aid enquirers to understand the text; present to the responsible interna

6、tional/European committee any enquiries on the interpretation, or proposals for change, and keep the UK interests informed; monitor related international and European developments and promulgate them in the UK. Summary of pages This document comprises a front cover, an inside front cover, the EN tit

7、le page, pages 2 to 18, an inside back cover and a back cover. The BSI copyright notice displayed in this document indicates when the document was last issued. Amendments issued since publication Amd. No. Date Comments EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 3005 November 2004 ICS 49.03

8、0.30 Supersedes EN 3005:2003 English version Aerospace series - Nuts, self-locking, MJ threads, in heat resisting nickel base alloy NI-PH1302 (Waspaloy), silver plated or uncoated - Classification: 1 210 MPa (at ambient temperature) / 730 C - Technical specification Srie arospatiale - crous, freinag

9、e interne, filetage MJ, en alliage rsistant chaud base de nickel NI- PH1302 (Waspaloy), argents ou non revtus - Classification : 1 210 MPa ( temprature ambiante) / 730 C - Spcification technique Luft- und Raumfahrt - Muttern, selbstsichernd, MJ- Gewinde, aus hochwarmfester Nickelbasislegierung NI- P

10、H1302 (Waspaloy), versilbert oder unbeschichtet - Klasse: 1 210 MPa (bei Raumtemperatur) / 730 C - Technische Lieferbedingungen This European Standard was approved by CEN on 11 September 2003. CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions fo

11、r giving this European Standard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning such national standards may be obtained on application to the Central Secretariat or to any CEN member. This European Standard exists in three official

12、 versions (English, French, German). A version in any other language made by translation under the responsibility of a CEN member into its own language and notified to the Central Secretariat has the same status as the official versions. CEN members are the national standards bodies of Austria, Belg

13、ium, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom. EUROPEAN COMMITTEE FOR STANDARDIZATION CO

14、MIT EUROPEN DE NORMALISATION EUROPISCHES KOMITEE FR NORMUNG Management Centre: rue de Stassart, 36 B-1050 Brussels 2004 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 3005:2004: E EN 3005:2004 (E) 2 Contents Page Foreword3 1 Scope

15、 4 2 Normative references 4 3 Terms and definitions .4 4 Quality assurance6 5 Requirements.7 EN 3005:2004 (E) 3 Foreword This document (EN 3005:2004) has been prepared by the European Association of Aerospace Manufacturers - Standardization (AECMA-STAN). After enquiries and votes carried out in acco

16、rdance with the rules of this Association, this Standard has received the approval of the National Associations and the Official Services of the member countries of AECMA, prior to its presentation to CEN. This European Standard shall be given the status of a national standard, either by publication

17、 of an identical text or by endorsement, at the latest by May 2005, and conflicting national standards shall be withdrawn at the latest by May 2005. This document supersedes EN 3005:2003. According to the CEN/CENELEC Internal Regulations, the national standards organizations of the following countri

18、es are bound to implement this European Standard: Austria, Belgium, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Slovakia, Slovenia, Spain, Sweden, Switzerlan

19、d and United Kingdom. EN 3005:2004 (E) 4 1 Scope This standard specifies the characteristics, qualification and acceptance requirements for self-locking nuts with MJ threads in NI-PH1302, silver plated or uncoated for aerospace applications. Classification: 1 210 MPa 1)/ 730 C 2)It is applicable whe

20、never 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 edition of the referenced document (including any amendments) applies. ISO 2859

21、-1, Sampling procedures for inspection by attributes Part 1: Sampling schemes indexed by acceptance quality limit (AQL) for lot-by-lot inspection ISO 3452, Non-destructive testing Penetrant inspection General principles ISO 4288, Geometrical Product Specifications (GPS) Surface texture: Profile meth

22、od Rules and procedures for the assessment of surface texture ISO 8642, Aerospace Self-locking nuts with maximum operating temperature greater than 425 C Test methods EN 2786, Aerospace series Electrolytic silver plating of fasteners 3)EN 9133, Aerospace series Quality management systems Qualificati

23、on procedure for aerospace standard parts 3)ASTM E 112-96, Standard Test Methods for Determining Average Grain Size 4)3 Terms and definitions For the purposes of this standard, the following terms and definitions apply. 3.1 batch quantity of finished nuts, of the same type and same diameter, produce

24、d 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 relevant heat treatments and surface treatments 3.2 inspection lot quantity of nuts from a single production batch with t

25、he same part number which completely defines the nut 1) Correspond to the minimum tensile stress which the nut is able to withstand at ambient temperature without breaking or cracking when tested with a bolt of a higher strength class. 2) Maximum test temperature of the parts 3) Published as AECMA P

26、restandard at the date of publication of this standard 4) Published by: American Society for Testing and Materials (ASTM), 1916, Race Street, Philadelphia, PA 19103, USA EN 3005:2004 (E) 5 3.3 Surface discontinuities 3.3.1 crack rupture in the material which may extend in any direction and which may

27、 be intercrystalline or transcrystalline in character 3.3.2 seam open surface defect 3.3.3 lap surface defect caused by folding over metal fins or sharp corners and then rolling or forging them into the surface 3.3.4 inclusions non-metallic particles originating from the material manufacturing proce

28、ss. These particles may be isolated or arranged in strings. 3.4 test temperature ambient temperature unless otherwise specified 3.5 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 cho

29、sen 3.6 critical defect a defect that, according to judgement and experience, is likely to result in hazardous or unsafe conditions 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 3.7 major def

30、ect a defect other than critical, that is likely to result in a failure or to reduce materially the usability of the considered product for its intended purpose 3.8 minor defect a defect that is not likely to reduce materially the usability of the considered product for its intended purpose, or that

31、 is a departure from established specification having little bearing on the effective use or operation of this product 3.9 sampling plan a plan according to which one or more samples are taken in order to obtain information and possibly to reach a decision 3.10 limiting quality (LQ 10 ) in a samplin

32、g plan, the quality limit which corresponds to a specified 10 % probability of acceptance EN 3005:2004 (E) 6 3.11 acceptance quality limit (AQL) a quality limit which in a sampling plan corresponds to a specified but relatively high probability of acceptance It is the maximum per cent defective (or

33、the maximum number of defects per hundred units) that, for purposes of sampling inspection can be considered satisfactory as a process average. 3.12 finished nut a nut ready for use, inclusive of any possible treatments and/or surface coatings, as specified in the product standard or definition docu

34、ment 3.13 definition document document specifying all the requirements for finished nuts 3.14 self-locking torque the torque to be applied to the nut or bolt to maintain movement of rotation in relation to the associated part, the assembly being under no axial load and the nut locking system being c

35、ompletely engaged with the bolt (minimum protrusion of two pitches including end chamfer) 3.15 seating torque the tightening torque to be applied to the nut or bolt to introduce or to increase the axial load in the assembly 3.16 unseating torque the untightening torque to be applied to the nut or bo

36、lt to reduce or remove the axial load in the assembly 3.17 breakaway torque the torque required to start unscrewing the nut or bolt with respect to the associated part, with the nut locking device still fully engaged on the bolt, but after the axial load in the assembly has been removed by unscrewin

37、g half a turn followed by a halt in rotational movement 3.18 wrench feature torque the torque to be applied to the wrenching feature of the nut 4 Quality assurance 4.1 Qualification EN 9133 Qualification inspections and tests (requirements, methods, numbers of nuts) are specified in Table 1. They sh

38、all be carried out on: each type and diameter of nut; 46 nuts selected from a single inspection lot by simple random sampling. The test programme may possibly be reduced, or the qualification of a nut be granted without inspection or testing. Any such decision shall be based on the results obtained

39、on similar types and diameters of nuts provided that the design and manufacturing conditions are identical. Table 2 indicates the allocation of nut samples for the inspections and tests. EN 3005:2004 (E) 7 4.2 Acceptance 4.2.1 Purpose The purpose of acceptance inspections and tests is to check, as s

40、imply as possible, by a method representative of actual use conditions, with the uncertainty inherent to statistical sampling, that the nuts constituting the batch satisfy the requirements of this standard. 4.2.2 Conditions Acceptance inspections and tests (requirements, methods, numbers of nuts) ar

41、e specified in Table 1 ; they shall be carried out on each production batch or inspection lot. Nuts from the batch or lot to be tested shall be selected by simple random sampling. Each nut may be submitted to several inspections or tests. If a more stringent inspection is deemed necessary, all or pa

42、rt of the qualification inspections and tests may be performed during the acceptance inspection and testing. In this case, the number of nuts submitted to these inspections and tests is the same as that submitted for qualification inspection and tests. 4.2.3 Responsibility Acceptance inspections and

43、 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. 5 Requirements See Table 1. EN 3005:2004 (E) 8 Table 1 Technical requirements and test me

44、thods Clause Characteristic Requirement Inspection and test method Q/A aSample size Q 5.1 Material In accordance with the product standard or definition document Chemical analysis or certificate of conformity issued by the manufacturer of the semi-finished product A Q 46 5.2 Dimensions, tolerances a

45、nd tolerances of form and position In accordance with the product standard or definition document Standard gauging A Tables 3 and 4 5.3 Manufacturing Q 5.3.1 Forming Nuts shall be formed by a hot or cold forming process. If hot formed, the forming temperature shall not exceed 1 150 C and they shall

46、be air cooled or faster. The equipment shall ensure a uniform temperature throughout the production batch. The method of forming shall be indicated. Q The heat treatment medium or atmosphere shall not cause any surface contamination except as permitted by 5.5.4. Calibration of the heat treatment equ

47、ipment shall be confirmed. Any scale which will not be removed by subsequent machining shall be removed by abrasive blasting with an appropriate equipment. Visual examination 5.3.2 Heat treatment Solution treat at a temperature of 1 010 C to 1 080 C, hold at the selected temperature within 15 C for

48、not less than 1 h and oil quench or equivalent or faster. Stabilization treatment at (850 8) C for 4 h and air cooled or faster. Precipitation treatment at (760 8) C, held at temperature for 16 h 15 min, cooled in air or faster. Examination of the heat treatment specification continued EN 3005:2004

49、(E) 9 Table 1 (continued) Clause Characteristic Requirement Inspection and test method Q/A aSample size 5.3.3 Q 46 Bearing surface perpendicularity In accordance with the product standard or definition document For non-floating plate nuts having a bearing surface exceeding 1,5 the thread nominal diameter, the perpendicularity requirement shall, unless otherwise specified by the product standard or definition document, apply only

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