EN 4322-2004 en Aerospace series - Bolts double hexagon head with lockwire holes relieved shank long thread in titanium alloy TI-P64001 anodized MoS2 coated - Strength class 1 100 .pdf

1、BRITISH STANDARD AEROSPACE SERIES BS EN 4322:2004 Bolts, double hexagon head with lockwire holes, relieved shank, long thread, in titanium alloy TI-P64001, anodized, MoS 2coated Strength class: 1 100 MPa (at ambient temperature) The European Standard EN 4322:2004 has the status of a British Standard

2、 ICS 49.030.20 BS EN 4322:2004 This British Standard, was published under the authority of the Standards Policy and Strategy Committee on 15 December 2004 BSI 15 December 2004 ISBN 0 580 45094 5 National foreword This British Standard is the official English language version of EN 4322:2004. It supe

3、rsedes BS EN 4322:2003 which is withdrawn. 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 secretar

4、y. Cross-references The British Standards 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

5、 or of British Standards Online. This publication 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 t

6、ext; present to the responsible international/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 c

7、over, an inside front cover, the EN title page, pages 2 to 9 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 4322 Novembe

8、r 2004 ICS 49.030.20 Supersedes EN 4322:2003 English version Aerospace series - Bolts, double hexagon head with lockwire holes, relieved shank, long thread, in titanium alloy TI-P64001, anodized, MoS2 coated - Strength class: 1 100 MPa (at ambient temperature) Srie arospatiale - Vis tte bihexagonale

9、 avec trous de fil frein, ft dgag, filetage long, en alliage de titane TI- P64001, anodises, revtues MoS2 - Classe de rsistance : 1 100 MPa ( temprature ambiante) Luft- und Raumfahrt - Zwlfkantschrauben mit Lcher fr Sicherungsdraft, Dnnschaft, langes Gewinde, aus Titanlegierung TI-P64001, anodisiert

10、, MoS2 beschichtet - Festigkeitsklasse: 1 100 MPa (bei Raumtemperatur) 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 for giving this European Standard the status of a national

11、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 versions (English, French, German). A version in any oth

12、er 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, Belgium, Cyprus, Czech Republic, Denmark, Estonia, Finland, F

13、rance, 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 COMIT EUROPEN DE NORMALISATION EUROPISCHES KOMITEE FR NORMU

14、NG 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 4322:2004: EEN 4322:2004 (E) 2 Contents Page Foreword3 1 Scope 4 2 Normative references 4 3 Required characteristics.4 4

15、 Designation 9 5 Marking .9 6 Technical specification .9 EN 4322:2004 (E) 3 Foreword This document (EN 4322:2004) has been prepared by the European Association of Aerospace Manufacturers - Standardization (AECMA-STAN). After enquiries and votes carried out in accordance with the rules of this Associ

16、ation, 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 of an identical text or by endorsem

17、ent, at the latest by May 2005, and conflicting national standards shall be withdrawn at the latest by May 2005. This document supersedes EN 4322:2003. According to the CEN/CENELEC Internal Regulations, the national standards organizations of the following countries are bound to implement this Europ

18、ean 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, Switzerland and the United Kingdom. EN 4322:20

19、04 (E) 4 1 Scope This standard specifies the characteristics of double hexagon headed bolts with lockwire holes, relieved shank and long thread, in TI-P64001, anodized, MoS 2coated, for aerospace applications. Strength class: 1 100 MPa 1)2 Normative references The following referenced documents are

20、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 3353-1, Aerospace Lead and runout threads Part 1: Rolled external threads ISO 4095,

21、Aerospace Bihexagonal drives Wrenching configuration Metric series ISO 5855-2, Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts EN 2424, Aerospace series Marking of aerospace products EN 2491, Aerospace series Molybdenum disulphide dry lubricants Coating methods EN 3813, Aerospace se

22、ries Titanium alloy TI-P64001 Annealed Bar and wire for forged fasteners D e 25 mm 2)EN 3818, Aerospace series Bolts, MJ threads, in titanium alloy TI-P64001 Strength class: 1 100 MPa (at ambient temperature) Technical specification 3 Required characteristics 3.1 Configuration Dimensions Tolerances

23、Masses See Figure 1 and Tables 1 and 2. Dimensions and tolerances are in millimetres. They apply after anodizing but before MoS 2coating. 3.2 Materials EN 3813 3.3 Surface treatment EN 2491 1) Minimum tensile strength of the material at ambient temperature 2) Published as AECMA Prestandard at the da

24、te of publication of this standard EN 4322:2004 (E) 5 Key 1 rolled 2 values apply before MoS 2 coating. 3 remove sharp edges 0,1 to 0,4. 4 pitch diameter 5 thread 6 marking 7 conforms to ISO 3353-1. 8 shape in this area at manufacturers option 9 four holes M deburred aWhen the length of the shank is

25、 less than one times the nominal value of the shank diameter D, the run-out is measured at a distance equal to half the actual shank length. bFor bolts having a shank length less than one times the nominal value of the shank diameter D, and for those threaded to head, the pitch diameter axis shall b

26、e used as the datum. Figure 1 EN 4322:2004 (E) 6 Table 1 Thread aD E F G H K M P Q R 1 S bT U V X Y Z Code Designation 0,13 max. min. min. min. max. min. H13 0,5 max. min. min. max. min. max. min. 050 MJ50,8-4h6h 4,48 9,1 8,3 6,8 1 5,65 5,35 4,2 3,4 0,5 0,3 7 2 2,9 2,5 3,7 3,2 0,13 060 MJ61-4h6h 5,3

27、5 10,6 9,8 7,8 1,2 6,15 5,85 4,6 4,2 8 2,3 3,2 2,8 4,6 4,1 0,12 0,15 070 MJ71-4h6h 6,35 12,1 11,3 8,8 1,4 6,65 6,35 5,1 5,2 9 2,6 3,7 3,3 5,4 4,9 0,18 080 MJ81-4h6h 7,35 13,6 12,8 9,8 1,6 7,15 6,85 5,5 6,2 0,7 0,5 10 2,8 4,1 3,7 5,7 5,2 0,003 0,2 100 MJ101,25-4h6h 9,19 16,7 15,7 11,8 2 8,15 7,85 6,4

28、 7,9 0,8 12 3,1 5,1 4,7 7,2 6,7 0,15 0,25 120 MJ121,25-4h6h 11,19 19,9 18,8 13,7 2,4 9,35 9,05 1,2 7,4 9,8 0,9 0,6 14 3,5 6 5,6 8,5 8 0,0025 0,18 0,3 aIn accordance with ISO 5855-2 b Bihexagonal wrenching configuration in conformity with ISO 4095 over length T min. EN 4322:2004 (E) 7 Table 2 Thread

29、code 050 060 070 080 100 120 W Mass aW Mass a W Mass a W Mass a W Mass a W Mass aLength code N 0,3 max. min. max. min. max. min. max. min. max. min. max. min. 008 8 1,76 010 10 1,90 2,72 3,84 5,14 012 12 2,04 2,92 4,12 5,51 014 14 2,17 3,12 4,40 5,89 9,53 016 16 2,31 3,32 4,68 6,26 10,12 15,87 018 1

30、8 2,1 1,7 2,46 3,52 4,96 6,64 10,71 16,74 020 20 4 2,5 2,60 2,7 2,2 3,72 5,24 7,02 11,30 17,61 022 22 6 4,5 2,74 4 2,5 3,92 2,7 2,2 5,52 7,39 11,88 18,48 024 24 8 6,5 2,88 6 4,5 4,12 4 2,5 5,80 2,7 2,2 7,77 12,46 19,35 026 26 10 8,5 3,02 8 6,5 4,32 6 4,5 6,08 4 2,5 8,14 13,05 20,22 028 28 12 10,5 3,

31、16 10 8,5 4,52 8 6,5 6,36 6 4,5 8,52 3,3 2,7 13,64 21,09 030 30 14 12,5 3,30 12 10,5 4,72 10 8,5 6,65 8 6,5 8,90 4 2,7 14,23 21,96 032 32 16 14,5 3,44 14 12,5 4,92 12 10,5 6,93 10 8,5 9,27 6 4,5 14,82 3,4 2,8 22,83 034 34 18 16,5 3,58 16 14,5 5,12 14 12,5 7,21 12 10,5 9,65 8 6,5 15,40 4 2,8 23,71 03

32、6 36 20 18,5 3,71 18 16,5 5,32 16 14,5 7,49 14 12,5 10,03 10 8,5 15,99 6 4,5 24,58 038 38 22 20,5 3,85 20 18,5 5,52 18 16,5 7,77 16 14,5 10,41 12 10,5 16,58 8 6,5 25,45 040 40 24 22,5 3,99 22 20,5 5,71 20 18,5 8,05 18 16,5 10,78 14 12,5 17,16 10 8,5 26,32 042 42 26 24,5 4,13 24 22,5 5,91 22 20,5 8,3

33、3 20 18,5 11,16 16 14,5 17,75 12 10,5 27,19 044 44 28 26,5 4,27 26 24,5 6,12 24 22,5 8,61 22 20,5 11,53 18 16,5 18,34 14 12,5 28,06 046 46 30 28,5 4,41 28 26,5 6,31 26 24,5 8,89 24 22,5 11,91 20 18,5 18,93 16 14,5 28,94 048 48 32 30,5 4,55 30 28,5 6,51 28 26,5 9,17 26 24,5 12,29 22 20,5 19,52 18 16,

34、5 29,80 050 50 34 32,5 4,69 32 30,5 6,71 30 28,5 9,45 28 26,5 12,66 24 22,5 20,10 20 18,5 30,68 052 52 36 34,5 4,83 34 32,5 6,91 32 30,5 9,73 30 28,5 13,04 26 24,5 20,69 22 20,5 31,54 054 54 38 36,5 4,97 36 34,5 7,11 34 32,5 10,02 32 30,5 13,41 28 26,5 21,27 24 22,5 32,42 056 56 40 38,5 5,11 38 36,5

35、 7,31 36 34,5 10,30 34 32,5 13,79 30 28,5 21,86 26 24,5 33,29 058 58 42 40,5 5,25 40 38,5 7,51 38 36,5 10,58 36 34,5 14,17 32 30,5 22,45 28 26,5 34,16 060 60 44 42,5 5,39 42 40,5 7,71 40 38,5 10,86 38 36,5 14,54 34 32,5 23,01 30 28,5 35,03 062 62 46 44,5 5,53 44 42,5 7,91 42 40,5 11,14 40 38,5 14,92

36、 36 34,5 23,63 32 30,5 35,90 064 64 48 46,5 5,67 46 44,5 8,11 44 42,5 11,42 42 40,5 15,30 38 36,5 24,21 34 32,5 36,77 066 66 50 48,5 5,81 48 46,5 8,31 46 44,5 11,70 44 42,5 15,67 40 38,5 24,80 36 34,5 37,64 068 68 52 50,5 5,95 50 48,5 8,51 48 46,5 11,98 46 44,5 16,05 42 40,5 25,38 38 36,5 38,51 cont

37、inued EN 4322:2004 (E) 8 Table 2 (concluded) Thread code 050 060 070 080 100 120 W Mass aW Mass a W Mass a W Mass a W Mass a W Mass aLength code N 0,3 max. min. max. min. max. min. max. min. max. min. max. min. 070 70 54 52,5 6,09 52 50,58 ,71 50 48,51 2 ,26 48 46,51 6 ,43 44 42,52 5 ,97 40 38,5 39,

38、38 072 72 54 52,5 8,90 52 50,5 12,54 50 48,5 16,80 46 44,5 26,56 42 40,5 40,25 074 74 56 54,5 9,10 54 52,5 12,82 52 50,5 17,18 48 46,5 27,15 44 42,5 41,13 076 76 58 56,5 9,30 56 54,5 13,10 54 52,5 17,56 50 48,5 27,74 46 44,5 41,99 078 78 60 58,5 9,50 58 56,5 13,39 56 54,5 17,93 52 50,5 28,32 48 46,5

39、 42,87 080 80 62 60,5 9,70 60 58,5 13,67 58 56,5 18,31 54 52,5 28,91 50 48,5 43,74 082 82 64 62,5 9,90 62 60,5 13,95 60 58,5 18,69 56 54,5 29,50 52 50,5 44,61 084 84 66 64,5 10,10 64 62,5 14,23 62 60,5 19,06 58 56,6 30,08 54 52,5 45,48 086 86 66 64,5 14,51 64 62,5 19,44 60 58,5 30,67 56 54,5 46,35 0

40、88 88 68 66,5 14,79 66 64,5 19,81 62 60,5 31,26 58 56,5 47,22 090 90 70 68,5 15,08 68 66,5 20,18 64 62,5 31,84 60 58,5 48,09 092 92 72 70,5 15,36 70 68,5 20,56 66 64,5 32,43 62 60,5 48,97 094 94 74 72,5 15,64 72 70,5 20,94 68 66,5 33,02 64 62,5 49,83 096 96 76 74,5 15,92 74 72,5 21,32 70 68,5 33,61

41、66 64,5 50,71 098 98 78 76,5 16,20 76 74,5 21,69 72 70,5 34,19 68 66,5 51,58 100 100 78 76,5 22,07 74 72,5 34,78 70 68,5 52,45 104 104 82 80,5 22,83 78 76,5 35,95 74 72,5 54,19 108 108 86 84,5 23,58 82 80,5 37,13 78 76,5 55,93 112 112 90 88,5 24,33 86 84,5 38,30 82 80,5 57,67 116 116 90 88,5 39,48 8

42、6 84,5 59,42 120 120 94 92,5 40,65 90 88,5 61,16 124 124 98 96,5 41,83 94 92,5 62,90 128 128 102 100,543,00 98 96,5 64,64 132 132 106 104,544,18 102 100,5 66,38 136 136 110 108,545,35 106 104,5 68,12 140 140 114 112,546,53 110 108,5 69,87 144 144 114 112,5 71,60 148 148 118 116,5 73,35 152 152 122 1

43、20,5 75,09 156 156 126 124,5 76,83 160 160 130 128,5 78,57 164 164 134 132,5 80,32 168 168 138 136,5 82,06 aMass quoted in kg/1 000 parts EN 4322:2004 (E) 9 4 Designation EXAMPLE Description block BOLT Identity block EN4322-080060 Number of this standard Thread code (see Table 1) Length code (see Ta

44、ble 2) NOTE If necessary, the code I9005 shall be placed between the description block and the identity block. 5 Marking EN 2424, indicated on Figure 1 and Table 3. Table 3 Thread code Style 050 C 060 to 120 A 6 Technical specification EN 3818 BS EN 4322:2004 BSI 389 Chiswick High Road London W4 4AL

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