BS EN 3302-2017 Aerospace series Bolts in heat resisting steel FE-PM1708 (FV535) Classification 1 000 MPa 550 C Technical specification《航空航天系列 FE-PM1708(FV535)型耐热钢制螺栓 等级 1000MPa 55.pdf

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BS EN 3302-2017 Aerospace series Bolts in heat resisting steel FE-PM1708 (FV535) Classification 1 000 MPa 550 C Technical specification《航空航天系列 FE-PM1708(FV535)型耐热钢制螺栓 等级 1000MPa 55.pdf_第1页
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1、Aerospace series - Bolts in heat resisting steel FE-PM1708 (FV535) - Classification: 1 000 MPa/550 C - Technical specification BS EN 3302:2017 BSI Standards Publication WB11885_BSI_StandardCovs_2013_AW.indd 1 15/05/2013 15:06 EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 3302 July 2017 ICS 49

2、.030.20 Supersedes EN 3302:2007 English Version Aerospace series - Bolts in heat resisting steel FE-PM1708 (FV535) - Classification: 1 000 MPa/550 C - Technical specification Srie arospatiale - Vis en acier rsistant chaud FE- PM1708 (FV535) - Classification : 1 000 MPa/550 C - Spcification technique

3、 Luft- und Raumfahrt - Schrauben aus hochwarmfestem Stahl FE-PM1708 (FV535) - Klasse: 1 000 MPa/550 C - Technische Lieferbedingungen This European Standard was approved by CEN on 10 April 2017. CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions f

4、or 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 CEN-CENELEC Management Centre or to any CEN member. This European Standard exists in thr

5、ee official 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 CEN-CENELEC Management Centre has the same status as the official versions. CEN members are the national standards bo

6、dies of Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Serbia, Slovakia, Sl

7、ovenia, Spain, Sweden, Switzerland, Turkey and United Kingdom. EUROPEAN COMMITTEE FOR STANDARDIZATION COMIT EUROPEN DE NORMALISATION EUROPISCHES KOMITEE FR NORMUNG CEN-CENELEC Management Centre: Avenue Marnix 17, B-1000 Brussels 2017 CEN All rights of exploitation in any form and by any means reserv

8、ed worldwide for CEN national Members. Ref. No. EN 3302:2017 E National foreword This British Standard is the UK implementation of EN 3302:2017. It supersedes BS EN 3302:2007, which is withdrawn. The UK participation in its preparation was entrusted to Technical Committee ACE/12, Aerospace fasteners

9、 and fastening systems. A list of organizations represented on this committee can be obtained on request to its secretary. This publication does not purport to include all the necessary provisions of a contract. Users are responsible for its correct application. The British Standards Institution 201

10、7 Published by BSI Standards Limited 2017 ISBN 978 0 580 96841 9 ICS 49.030.20 Compliance with a British Standard cannot confer immunity from legal obligations. This British Standard was published under the authority of the Standards Policy and Strategy Committee on 31 August 2017. Amendments/corrig

11、enda issued since publication Date Text affected BRITISH STANDARD BS EN 3302:2017 EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 3302 July 2017 ICS 49.030.20 Supersedes EN 3302:2007 English Version Aerospace series - Bolts in heat resisting steel FE-PM1708 (FV535) - Classification: 1 000 MPa/5

12、50 C - Technical specification Srie arospatiale - Vis en acier rsistant chaud FE- PM1708 (FV535) - Classification : 1 000 MPa/550 C - Spcification technique Luft- und Raumfahrt - Schrauben aus hochwarmfestem Stahl FE-PM1708 (FV535) - Klasse: 1 000 MPa/550 C - Technische Lieferbedingungen This Europe

13、an Standard was approved by CEN on 10 April 2017. CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this European Standard the status of a national standard without any alteration. Up-to-date lists and bibliographical references conce

14、rning such national standards may be obtained on application to the CEN-CENELEC Management Centre or to any CEN member. This European Standard exists in three official versions (English, French, German). A version in any other language made by translation under the responsibility of a CEN member int

15、o its own language and notified to the CEN-CENELEC Management Centre has the same status as the official versions. CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, G

16、ermany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Serbia, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and United Kingdom. EUROPEAN COMMITTEE FOR STANDARDIZATION COMIT EUROPEN DE NORMALISATION EUROPISCHES

17、 KOMITEE FR NORMUNG CEN-CENELEC Management Centre: Avenue Marnix 17, B-1000 Brussels 2017 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 3302:2017 E BS EN 3302:2017EN 3302:2017 (E) 2 Contents Page European foreword 3 1 Scope . 4 2

18、 Normative references . 4 3 Terms and definitions 5 4 Certification and quality assurance . 7 5 Technical requirements and test methods . 8 (informative) Standard evolution form . 25 BS EN 3302:2017EN 3302:2017 (E) 3 European foreword This document (EN 3302:2017) has been prepared by the Aerospace a

19、nd Defence Industries Association of Europe - Standardization (ASD-STAN). After enquiries and votes carried out in accordance 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 ASD, prior to it

20、s presentation to CEN. This European Standard shall be given the status of a national standard, either by publication of an identical text or by endorsement, at the latest by January 2018, and conflicting national standards shall be withdrawn at the latest by January 2018. Attention is drawn to the

21、possibility that some of the elements of this document may be the subject of patent rights. CEN shall not be held responsible for identifying any or all such patent rights. This document supersedes EN 3302:2007. According to the CEN-CENELEC Internal Regulations, the national standards organizations

22、of the following countries are bound to implement this European Standard: Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Ne

23、therlands, Norway, Poland, Portugal, Romania, Serbia, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and the United Kingdom. BS EN 3302:2017EN 3302:2017 (E) 4 1 Scope This European Standard specifies the technical, qualification and quality assurance requirements for bolts in material FE-PM1

24、708 (FV535) of tensile strength class 1 000 MPa at room temperature, maximum test temperature of material 550 C. Primarily for aerospace applications it is applicable to such bolts when referenced on the product standard or drawing. 2 Normative references The following documents, in whole or in part

25、, are normatively referenced in this document and are indispensable for its application. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 2493 1) , Aerospace series Heat resisting steel

26、FE-PM38 1 000 MPa R m 1 140 MPa Bars 2)EN 4244, Aerospace series Heat resisting alloy FE-PM1708 Vacuum arc remelted, hardened and tempered, bar a or D 200 mm, 1 000 MPa R m 1 140 MPa 2)EN 4245, Aerospace series Heat resisting alloy FE-PM1708 Vacuum arc remelted, as forged, forging stock D e 300 mm 2

27、)EN 9100, Quality Management Systems Requirements for Aviation, Space and Defense Organizations EN 9133, Aerospace series Quality management systems Qualification procedure for aerospace standard parts EN ISO 3452-1, Non-destructive testing Penetrant testing Part 1: General principles (ISO 3452-1) E

28、N ISO 4288, Geometrical Product Specifications (GPS) Surface texture: Profile method Rules and procedures for the assessment of surface texture (ISO 4288) ISO 2859-1, Sampling procedures for inspection by attributes Part 1: Sampling schemes indexed by acceptance quality limit (AQL) for lot-by-lot in

29、spection ISO 3534:1977, Statistics Vocabulary and symbols ISO 6508-1, Metallic materials Rockwell hardness test Part 1: Test method ISO 9000, Quality management systems Fundamentals and vocabulary TR 3040-1, Aerospace series Quality Assurance EN aerospace products Part 1: List of approved manufactur

30、ers 3)1)Inactive for new designation, see EN 4244 and EN 4245. 2)Published as ASD-STAN Prestandard at the date of publication of this standard. http:/www.asd-stan.org/ 3) Published as ASD-STAN Technical Report at the date of publication of this standard. http:/www.asd-stan.org/ BS EN 3302:2017EN 330

31、2:2017 (E) 5 3 Terms and definitions For the purposes of this document, the following terms and definitions apply. 3.1 production batch quantity of finished parts fabricated by the same process from a single material cast (single heat of alloy), having the same basic part number and diameter, heat t

32、reated together to the same specified condition and produced as one continuous run 3.2 inspection lot quantity of parts from a single production batch of the same part number which completely defines the part 3.3 Surface discontinuities 3.3.1 crack rupture in the material which may extend in any dir

33、ection and which may be intercrystalline or transcrystallyne in character 3.3.2 seam longitudinal surface defect in the form of an unwelded open fold in the material 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 in

34、clusion non-metallic particles originating from the material making process Note 1 to entry: They may exist as discrete particles or strings of particles extending longitudinally. 3.4 test temperature ambient temperature, unless otherwise specified 3.5 simple random sampling the taking of n items fr

35、om a population of N items in such a way that all possible combinations of n items have the same probability of being chosen SOURCE: ISO 3534, see definition 3.6 critical defect a defect that according to judgement and experience, is likely to result in hazardous or unsafe conditions for individuals

36、 using, maintaining, or depending upon the considered product, or that is likely to prevent performance of the function of a major end item SOURCE: ISO 3534, see definition 3.7 major defect a defect other than critical, that is likely to result in a failure or to reduce materially the usability of t

37、he considered product for its intended purpose BS EN 3302:2017EN 3302:2017 (E) 6 SOURCE: ISO 3534, see definition 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 is a departure from established specification

38、having little bearing on the effective use or operation of this product SOURCE: ISO 3534, see definition 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 SOURCE: ISO 3534, see definition 3.10 Limiting Quality LQ

39、 10 in a sampling plan, a quality limit which corresponds to a specified and relatively low probability of acceptance in this case 10 % probability of acceptance Note 1 to entry: It is the limiting lot quality characteristic that a lot of this quality would occur. Note 2 to entry: When expressed as

40、a per cent defective, it may be referred to as a lot tolerance per cent defective. SOURCE: ISO 3534, see definition 3.11 Acceptance Quality Limit AQL a quality limit which in a sampling plan corresponds to a specified but relatively high probability of acceptance Note 1 to entry: It is the maximum p

41、er cent defective (or the maximum number of defects per hundred units) that, for purposes of sampling inspection, can be considered satisfactory as a process average. SOURCE: ISO 3534, see definition 3.12 finished bolt a bolt ready for use, inclusive of any possible treatments and/or surface coating

42、s, as specified in the dimensional standard or definition document 3.13 definition document document specifying all the requirements for bolts i.e. metallurgical, geometrical and dimensional, functional (strength and temperature classes). BS EN 3302:2017EN 3302:2017 (E) 7 4 Certification and quality

43、 assurance 4.1 Qualification 4.1.1 Purpose The purpose of qualification tests is to ensure that the bolt design and bolt manufacturing conditions allow the bolt to comply with the requirements of this standard. 4.1.2 Conditions The qualification tests summarized in Table 3 shall be performed on each

44、 type and diameter of bolt. Proposed changes in manufacturing source or procedure shall be subject to the requirements of EN 9133. 25 bolts selected from a single inspection lot by simple random sampling shall be subjected to the qualification tests. The number of bolts to be subjected to each test

45、as well as the method(s) to be used is specified in Table 1. The tests to be applied to each bolt are shown in Table 4. The test programme may possibly be reduced, this decision will be based on the comparison of results obtained from parts of similar design, size and manufacturing conditions. All o

46、r part of these tests may also be performed for production acceptance, when a reinforced inspection seems to be necessary, or to survey bolts that have not proved satisfactory in use. In that case, the sample to be subjected to these tests is the same as that used for production acceptance tests. 4.

47、1.3 Qualification test requirements and procedures The qualification test requirements and procedures shall be to the requirements of EN 9133. 4.1.4 Qualified manufacturers A list of qualified manufacturers for specific standard parts is listed in TR 3040-1. 4.2 Acceptance 4.2.1 Purpose The purpose

48、of acceptance 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 bolts constituting the batch satisfy the requirements of this standard. 4.2.2 Conditions Acceptance tests are summarized in Tab

49、le 3. They shall be performed on each batch. Table 1 specifies, the test method and sampling plan to be used for each test. Bolts from the batch to be tested shall be selected by simple random sampling. Each bolt may be submitted to several tests. The bolts to be subjected to destructive tests may be those on which non-destructive tests have been performed. BS EN 3302:2017EN 3302:2017 (E) 8 4.3 Quality system certification 4.3.1 Purpose The purpose of quality system certification is

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