EN 4130-2009 en Aerospace series - Bolts normal hexagonal head coarse tolerance normal shank medium length thread in titanium alloy aluminium IVD coated - Classification 1 100 MPa .pdf

1、BS EN 4130:2009ICS 49.030.20NO COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGHT LAWBRITISH STANDARDAerospace series Bolts, normal hexagonal head, coarse tolerance normal shank, medium length thread, in titanium alloy, aluminium IVD coated Classification: 1 100 MPa (at ambient temperat

2、ure) / 425 CIncorporating corrigendumApril 2010National forewordThis British Standard is the UK implementation of EN 4130:2009, incorporating corrigendum April 2010.The UK participation in its preparation was entrusted by Technical Committee ACE/12, Aerospace fasteners and fastening systems.A list o

3、f 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.Compliance with a British Standard cannot confer immunity from legal ob

4、ligations.BS EN 4130:2009This British Standard was published under the authority of the Standards Policy and Strategy Committee on 31 May 2009 BSI 2010Amendments/corrigenda issued since publicationDate Comments 30 June 2010 Implementation of CEN corrigendum April 2010; Figure 1 replacedISBN 978 0 58

5、0 71481 8EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 4130 April 2009 ICS 49.030.20 English Version Aerospace series - Bolts, normal hexagonal head, coarse tolerance normal shank, medium length thread, in titanium alloy, aluminium IVD coated - Classification: 1 100 MPa (at ambient temperatur

6、e) / 425 C Srie arospatiale - Vis tte hexagonale normale, tige normale tolrance large, filetage moyen, en alliage de titane, revtues aluminium IVD - Classification : 1 100 MPa ( temprature ambiante) / 425 C Luft- und Raumfahrt - Sechskantschrauben, mit mittlerer Gewindelnge, aus Titanlegierung, Alum

7、inium IVD beschichtet - Klasse : 1 100 MPa (bei Raumtemperatur) / 425 C This European Standard was approved by CEN on 12 March 2009. 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 sta

8、ndard without any alteration. Up-to-date lists and bibliographical references concerning such national standards may be obtained on application to the CEN Management Centre or to any CEN member. This European Standard exists in three official versions (English, French, German). A version in any othe

9、r language made by translation under the responsibility of a CEN member into its own language and notified to the CEN Management Centre has the same status as the official versions. CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Cyprus, Czech Republic, Denmark, Estonia,

10、 Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom. EUROPEAN COMMITTEE FOR STANDARDIZATION COMIT EUROPEN DE NORMALISATION EUROPISC

11、HES KOMITEE FR NORMUNG Management Centre: Avenue Marnix 17, B-1000 Brussels 2009 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 4130:2009: EIncorporating corrigendum April 2010BS EN 4130:2009EN 4130:2009 (E) 2 Contents Page Forewo

12、rd 3 1 Scope 4 2 Normative references 4 3 Required characteristics .5 4 Designation 8 5 Marking .8 6 Technical specification .8 BS EN 4130:2009EN 4130:2009 (E) 3 Foreword This document (EN 4130:2009) has been prepared by the Aerospace and Defence Industries Association of Europe - Standardization (A

13、SD-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 its presentation to CEN. This European Standard shall be given the

14、 status of a national standard, either by publication of an identical text or by endorsement, at the latest by October 2009, and conflicting national standards shall be withdrawn at the latest by October 2009. Attention is drawn to the possibility that some of the elements of this document may be th

15、e subject of patent rights. CEN and/or CENELEC shall not be held responsible for identifying any or all such patent rights. According to the CEN/CENELEC Internal Regulations, the national standards organizations of the following countries are bound to implement this European Standard: Austria, Belgi

16、um, Bulgaria, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. BS EN 4130:2009EN 4

17、130:2009 (E) 4 1 Scope This standard specifies the characteristics of bolts, normal hexagonal head, coarse tolerance normal shank, medium length thread, in titanium alloy, aluminium IVD coated. Classification: 1 100 MPa 1) / 425 C 2)2 Normative references The following referenced documents are indis

18、pensable 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. EN 2424, Aerospace series Marking of aerospace products EN 9100, Aerospace series Quality man

19、agement systems Requirements (based on ISO 9001:2000) and Quality systems Model for quality assurance in design, development, production, installation and servicing (based on ISO 9001:1994) EN 9133, Aerospace series Quality management systems Qualification procedure for aerospace standard parts ISO

20、3193, Aerospace Bolts, normal hexagonal head, normal shank, short or medium length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1 100 MPa Dimensions ISO 3353-1, Aerospace Lead and runout threads Part 1: Rolled external threads ISO 5855-2, Aerospace MJ thr

21、eads Part 2: Limit dimensions for bolts and nuts ISO 7913, Aerospace Bolts and screws, metric Tolerances of form and position ISO 9152, Aerospace Bolts, with MJ threads, in titanium alloys, strength class 1 100 MPa Procurement specification TR 3775, Aerospace series Bolts and pins Materials 3)MIL-DT

22、L-83488D, Coating, aluminium, high purity 4)1) Minimum tensile strength of the material at ambient temperature. 2) Maximum that the bolt can withstand without continuous change in its original characteristics, after return to ambient temperature. The maximum temperature is determined by the surface

23、treatment. 3) Published as ASD Technical Report at the date of publication of this standard. 4) Published by: Department of Defense (DOD), the Pentagon, Washington, D.C. 20301, USA. BS EN 4130:2009EN 4130:2009 (E) 5 3 Required characteristics 3.1 Configuration Dimensions Masses See Figure 1 and Tabl

24、e 1. Dimensions and tolerances are expressed in millimetres, in conformity with ISO 3193, and apply after surface treatment. 3.2 Tolerances of form and position ISO 7913 3.3 Materials TR 3775 (titanium alloy, classification 1 100 MPa) 3.4 Surface treatment MIL-DTL-83488D, type II, class 3, 4 m to 12

25、 m. After aluminium deposit: a) mechanical blasting, followed by a chromate conversion coating within 24 h max. 5); b) optional lubrication with cethylic alcohol (code E). 5) Products used shall be in conformity with national regulation into force. BS EN 4130:2009EN 4130:2009 (E) 6 Values in microme

26、tres apply prior to surface treatment. Break sharp edges 0,1 to 0,4. Details of form not stated are left to the manufacturers discretion. Key 1 Continuous surface 2 2 holes D6 (optional) 3 1 hole D7 (optional) 4 Thread 5 Conforms to ISO 3353-1 6 Marking Figure 1 Configuration and dimensions 3,2 0,8

27、1,6 BS EN 4130:2009EN 4130:2009 (E) 7 Table 1 Diameter code Thread aD1D2D3D4bD5D6D7E F G H h12 min. 0 0,5 min. nom. Tol. H13 H13 min. max. min. 0 0,3030 MJ30,5 - 4h6h 3 5,5 5,4 2,3 0 0,5 6,5 0,4 0,2 2 040 MJ40,7 - 4h6h 4 6,4 6,4 3 1,1 7,6 0,5 2,5 050 MJ50,8 - 4h6h 5 7,4 5,25 7,4 3,4 0,5 1 1,5 8,7 3

28、1,35 060 MJ61 - 4h6h 6 9,4 6,25 9,3 4,2 1,4 10,9 3,5 1,6 070 MJ71 - 4h6h 7 10,3 7,25 10,2 5,2 1,9 12 4 1,85 080 MJ81 - 4h6h 8 12,3 8,25 12,2 6,2 14,3 4,5 2,1 100 MJ101,25 - 4h6h 10 16,3 10,25 16 7,9 1,6 2,4 18,9 0,6 0,3 5 2,35 120 MJ121,25 - 4h6h 12 18,3 12,25 18 9,8 21,1 6 2,85 140 MJ141,5 - 4h6h 1

29、4 21,3 14,25 21 11,5 3 24,5 7 3,35 160 MJ161,5 - 4h6h 16 23,3 16,25 23 13,5 26,8 8 3,85 180 MJ181,5 - 4h6h 18 26,3 18,25 26 15,5 3,8 30,2 9 4,35 200 MJ201,5 - 4h6h 20 29,3 20,25 29 17,5 33,6 10 4,85 Diameter code J K L1 0,2c, dL2L3N R Mass enom. Tol. Length code nom. 0 0,3 max. min. fg030 6 h12 002

30、to 030 2 to 30 7,5 0,4 0,2 0,526 0,031 040 7 002 to 040 2 to 40 10 6 1,039 0,056 050 8 3,25 003 to 050 3 to 50 12 7,5 2 0,5 0,3 1,839 0,087 060 10 h13 4,1 003 to 060 3 to 60 14 8,5 2,3 0,7 0,5 3,445 0,126 070 11 4,5 004 to 070 4 to 70 15 9,5 2, 7 4,734 0,171 080 13 5,35 004 to 080 4 to 80 16,5 10,5

31、3 7,225 0,224 100 17 7,1 005 to 100 5 to 100 20,5 13 3,4 0,8 0,6 13,961 0,349 120 19 7,9 006 to 120 6 to 120 22,5 14,5 4 0,9 22,330 0,503 140 22 9,2 007 to 140 7 to 140 26 17 4,7 1,1 0,8 34,159 0,685 160 24 10,05 008 to 160 8 to 160 28,5 18,5 5,4 50,196 0,895 180 27 11,3 009 to 180 9 to 180 31 21 6

32、1,3 1 70,451 1,132 200 30 12,6 010 to 200 10 to 200 33,5 22,5 6,7 95,985 1,398 aIn accordance with ISO 5855-2. bD4 max. shall be less than J. cIncrements: - 1 for L1 30; - 2 for 30 100. dIf greater lengths are required, they shall be chosen using the above increments. The length code corresponds to

33、the length L1, completed by one or two zeros to the left, where necessary, to obtain a three digit code. eApproximate values (kg/1 000 pieces), calculated on the basis of 4,45 kg/dm3, given for information purposes only. They apply to bolts without holes. f Value for head and first L4.g Increase for

34、 each additional millimetre of L4. BS EN 4130:2009EN 4130:2009 (E) 8 4 Designation EXAMPLE Description block BOLT Identity block EN4130H050040E Number of this standard Hole code (see Table 2) Diameter code (see Table 1) Length code (see Table 1) Lubrication code (see 3.4) NOTE If necessary the origi

35、nator code I9005 should be placed between the description block and the identity block. Table 2 Holes Code Lockwire H Split pin D Lockwire and split pin C No hole (hyphen) 5 Marking See Table 3 and Figure 1. Table 3 Diameter code EN 2424 Style 030 and 040 N 050 to 120 B 140 to 200 A 6 Technical spec

36、ification ISO 9152, except for clauses: a) Approval of manufacturers: see EN 9100; b) Qualification of bolts: see EN 9133. BS EN 4130:2009This page has been intentionally left blankBSI GroupHeadquarters 389 Chiswick High Road, London, W4 4AL, UK Tel +44 (0)20 8996 9001 Fax +44 (0)20 8996 7001 stand

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