1、BRITISH STANDARD AEROSPACE SERIES BS EN 2364:1989 Specification for Pins, shear headed, close tolerance This European Standard EN2364 has the status of a British Standard. UDC 621.882.6 0.34.14:629.7BS EN2364:1989 This British Standard, having been prepared under the directionof the Aerospace Standa
2、rds Policy Committee,waspublished underthe authority of the BoardofBSI on 30November1989 BSI 01-2000 The following BSI references relate to the work on this standard: Committee referenceACE/14 Draft for comment 88/72214 DC ISBN 0 580 17928 1 Cooperating organizations The European Committee for Stand
3、ardization, under whose supervision this European Standard was prepared, comprises the national standards organizations of the following Western European countries. Austria Oesterreichisches Normungsinstitut Belgium Institut belge de normalisation Denmark Dansk Standardiseringsraad Finland Suomen St
4、andardisoimisliito, r.y. France Association franaise de normalisation Germany Deutsches Institut fr Normung e.V. Greece Hellenic Organization for Standardization Iceland Icelandic Council for Standardization Ireland National Standards Authority of Ireland Italy Ente Nazionale Italiano di Unificazion
5、e Luxemburg Inspection des travails et des mines Netherlands Nederlands Normalisatie-instituut Norway Norges Standardiseringsforbund Portugal Instituto Portugus da Qualidade Spain Instituto Espaol de Normalizacin Sweden Standardiseringskommissionen i Sverige Switzerland Association suisse de normali
6、sation United Kingdom British Standards Institution Amendments issued since publication Amd. No. Date of issue CommentsBS EN2364:1989 BSI 01-2000 i Contents Page Cooperating organizations Inside front cover National foreword ii Brief history 2 Text of EN2364 3 National appendix A Inside back cover N
7、ational appendix B Inside back coverBS EN2364:1989 ii BSI 01-2000 National foreword This British Standard has been prepared under the direction of the Aerospace Standards Policy Committee and is the English language version of EN2364 “Aerospace series. Pins, shear headed, close tolerance” published
8、by the European Committee for Standardization (CEN). EN2364 was produced as a result of international discussion in which the UK took an active part. A British Standard does not purport to include all the necessary provisions of a contract. Users of British Standards are responsible for their correc
9、t application. Compliance with a British Standard does not of itself confer immunity from legal obligations. Summary of pages This document comprises a front cover, an inside front cover, pagesi andii, theEN title page, pages2to6, an inside back cover and a back cover. This standard has been updated
10、 (see copyright date) and may have had amendments incorporated. This will be indicated in the amendment table on the inside front cover.EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 2364 March 1989 UDC: 621.882.6-034.14:629.7 Key words: Aircraft industry Pins Tolerance Specifications Designat
11、ion Dimensions English version Aerospace series Pins, shear, headed, close tolerance Srie arospatiale Axes lisses tte et tolrances serres Luft- und Raumfahrt Pabolzen mit Kopf This European Standard was accepted by CEN on1988-05-26. CEN members are bound to comply with the requirements of CEN Intern
12、al 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 concerning such national standards may be obtained on application to the CEN Central Secretariat or to any CEN mem
13、ber. 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 into its own language and notified to CEN Central Secretariat has the same status as the official versions. CEN member
14、s are the national standards organizations of Austria, Belgium, Denmark, Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxemburg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and UnitedKingdom. CEN European Committee for Standardization Comit Europen de Normalisation Europi
15、sches Komitee fr Normung Central Secretariat: rue de Stassart 36, B-1050 Brussels CEN 1989 Copyright reserved to all CEN members Ref. No. EN 2364:1989EEN2364:1989 BSI 01-2000 2 Brief history This European Standard has been prepared by the European Association of Aerospace Manufacturers (AECMA). Afte
16、r enquiries and votes carried out in accordance with the rules of this Association, this Standard has successively received the approval of the National Associations and the Official Services of the member countries of AECMA, prior to its presentation to CEN. According to the Common CEN/CENELEC Rule
17、s, following countries are bound to implement this European Standard: Austria, Belgium, Denmark, Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxemburg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and the UnitedKingdom. Contents Page Brief history 2 1 Scope and field of a
18、pplication 3 2 References 3 3 Required characteristics 3 4 Designation 6 5 Marking 6 6 Technical specification 6 Figure Configuration 4 Table 1 Dimensions 4 Table 2 Lengths and masses (kg/1000pieces) 5EN2364:1989 BSI 01-2000 3 1 Scope and field of application This standard specifies the characterist
19、ics of close tolerance headed shear pins in steel: cadmium plated, for use in aerospace at temperatures below235 C. These shear pins are intended for use as a connecting part in conjunction with collars EN2365 and split pins EN2367. 2 References EN 2133, Cadmium plating of steels with maximum specif
20、ied tensile strength equal to or less than1450MPa, and copper and copper alloys Aerospace series. EN 2236, Aerospace series Pins, shear, headed, close tolerance Technical specification 1) . EN 2365, Aerospace series Collars, aluminium alloy. EN 2367, Aerospace series Split pins in steel EN2573. EN 2
21、424, Aerospace series Identification marking of standard fasteners. EN 2450, Steel FE-PL73 1230MPak R m k 1420MPa BarsD e k 40mm Aerospace series. EN 2451, Steel FE-PL73 1230MPak R m k 1420MPa Forgings D e k 40mm Aerospace series. 3 Required characteristics 3.1 Configuration Dimensions Tolerances Co
22、nfiguration shall correspond with the Figure. Dimensions and tolerances shall correspond with the Figure andTable 1 andTable 2. These values apply after cadmium plating. 3.2 Surface roughness R a =3,24m except where stated otherwise. These values apply prior to cadmium plating. 3.3 Material Steel EN
23、2450 ouEN2451 3.4 Surface treatment Cadmium plating EN2133, 7to104m 1) In preparationEN2364:1989 4 BSI 01-2000 Table 1 Dimensions Figure Configuration Dimensions in millimetres Diameter code D E F G H M N P max. min. min. max. min. max. min. max. min. H13 h11 030 2,99 2,965 5,3 5 4,88 1,8 1,6 0,3 0,
24、2 1,1 0,15 6 040 3,99 3,965 6,5 6 5,88 2 1,8 0,3 0,2 1,5 0,2 7 050 4,99 4,965 7,6 7 6,85 2,2 2 0,3 0,2 1,9 0,25 8 060 5,99 5,965 8,7 8 7,85 2,2 2 0,3 0,2 1,9 0,3 9 070 6,987 6,962 10,9 10 9,78 2,5 2,2 0,5 0,4 2,4 0,35 11 080 7,987 7,962 12 11 10,73 2,8 2,5 0,5 0,4 2,4 0,4 12 100 9,987 9,962 14,3 13
25、12,73 2,8 2,5 0,5 0,4 3 0,5 13EN 2364:1989 BSI 01-2000 5 Table 2 Lengths and masses (kg/1000pieces) Dimensions in millimetres Length Diameter code Code L 030 040 050 060 070 080 100 K Mass K Mass K Mass K Mass K Mass K Mass K Mass 007 7,0 3,85 0,67 008 8,0 4,85 0,72 4,6 1,24 009 9,0 5,85 0,78 5,6 1,
26、34 010 10,0 6,85 0,83 6,6 1,43 6,35 2,22 012 12,0 8,85 0,94 8,6 1,63 8,35 2,53 8,35 3,55 014 14,0 10,85 1,05 10,6 1,82 10,35 2,84 10,35 3,99 016 16,0 12,85 1,16 12,6 2,02 12,35 3,14 12,35 4,43 12,1 6,37 12,1 8,41 018 18,0 14,85 1,27 14,6 2,21 14,35 3,45 14,35 4,88 14,1 6,97 14,1 9,19 020 20,0 16,85
27、1,38 16,6 2,41 16,35 3,75 16,35 5,32 16,1 7,57 16,1 9,98 022 22,0 18,85 1,49 18,6 2,60 18,35 4,06 18,35 5,76 18,1 8,17 18,1 10,76 17,85 16,48 025 25,0 21,85 1,65 21,6 2,90 21,35 4,52 21,35 6,42 21,1 9,07 21,1 11,94 20,85 18,33 030 30,0 26,85 1,92 26,6 3,39 26,35 5,28 26,35 7,52 26,1 10,57 26,1 13,90
28、 25,85 21,40 035 35,0 31,85 2,20 31,6 3,87 31,35 6,04 31,35 8,62 31,1 12,07 31,1 15,86 30,85 24,46 040 40,0 36,85 2,47 36,6 4,36 36,35 6,81 36,35 9,72 36,1 13,57 36,1 17,83 35,85 27,53 045 45,0 41,35 7,57 41,35 10,83 41,1 15,07 41,1 19,77 40,85 30,60 050 50,0 46,35 8,34 46,35 11,93 46,1 16,58 46,1 2
29、1,75 45,85 33,67 055 55,0 51,1 18,08 51,1 23,71 50,85 36,74 060 60,0 56,1 19,58 56,1 25,67 55,85 39,81 065 65,0 61,1 21,08 61,1 27,64 60,85 42,88 070 70,0 66,1 22,58 66,1 29,60 65,85 45,95 075 75,0 70,85 49,02 080 80,0 75,85 52,08 +0,25 0EN2364:1989 6 BSI 01-2000 4 Designation Each pin shall only be
30、 designated as in the following example: NOTEIf necessary the originator codeS9005 may be introduced between the description block and the identity block. 5 Marking Each pin shall be marked in the positions shown in the Figure in accordance with the marking style shown inTable3 as defined by EN2424
31、6 Technical specification Pins supplied to this standard shall conform with the requirements of EN2236 Diameter code Marking style 030to040 D 050 to 100 ABSEN2364:1989 BSI 01-2000 National appendix A The United Kingdom participation in the preparation of this European Standard was entrusted by the A
32、erospace Standards Policy Committee (ACE/-) to Technical Committee ACE/14 upon which the following bodies were represented: British Independent Steel Producers Association Civil Aviation Authority (Airworthiness Division) Federation of Wire Rope Manufacturers of Great Britain Ministry of Defence Soc
33、iety of British Aerospace Companies Limited Stainless Steel Wire Export Group National appendix B The British Standards corresponding to the European Standards referred to in the text are identical in number and title with those given in clause2.BS EN 2364:1989 BSI 389 Chiswick High Road London W4 4
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