EN 4134-2009 en Aerospace series - Bolts normal hexagonal head coarse tolerance normal shank long thread in heat resisting nickel base alloy aluminium IVD coated - Classification 1.pdf

1、BS EN 4134:2009ICS 49.030.20,NO COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGHT LAWBRITISH STANDARDAerospace series Bolts, normalhexagonal head, coarsetolerance normalshank, long thread,in heat resistingnickel base alloy,aluminium IVD coated Classification: 1250 MPa (at ambienttemper

2、ature) / 425CThis British Standardwas published under theauthority of the StandardsPolicy and StrategyCommittee on 31 May 2009 BSI 2009ISBN 978 0 580 67788 5Amendments/corrigenda issued since publicationDate CommentsBS EN 4134:2009National forewordThis British Standard is the UK implementation of EN

3、 4134:2009.The UK participation in its preparation was entrusted to TechnicalCommittee ACE/12, Aerospace fasteners and fastening systems.A list of organizations represented on this committee can be obtained onrequest to its secretary.This publication does not purport to include all the necessary pro

4、visionsof a contract. Users are responsible for its correct application.Compliance with a British Standard cannot confer immunityfrom legal obligations.BS EN 4134:2009EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 4134 April 2009 ICS 49.030.20 English Version Aerospace series - Bolts, normal h

5、exagonal head, coarse tolerance normal shank, long thread, in heat resisting nickel base alloy, aluminium IVD coated - Classification: 1 250 MPa (at ambient temperature) / 425 C Srie arospatiale - Vis tte hexagonale normale, tige normale tolrance large, filetage long, en alliage rsistant chaud base

6、de nickel, revtues aluminium IVD - Classification: 1 250 MPa ( temprature ambiante)/425 CLuft- und Raumfahrt - Sechskantschrauben, langes Gewinde, aus hochwarmfester Nickelbasislegierung, Aluminium IVD beschichtet - Klasse : 1 250 MPa (bei Raumtemperatur) / 425 C This European Standard was approved

7、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 standard without any alteration. Up-to-date lists and bibliographical references concerning such national stand

8、ards 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 other language made by translation under the responsibility of a CEN member into its own language and notified t

9、o 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, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, N

10、etherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom. EUROPEAN COMMITTEE FOR STANDARDIZATION COMIT EUROPEN DE NORMALISATION EUROPISCHES KOMITEE FR NORMUNG Management Centre: Avenue Marnix 17, B-1000 Brussels 2009 CEN All rights of exploitat

11、ion in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 4134:2009: EBS EN 4134:2009EN 4134:2009 (E) 2 Contents Page Foreword 3 1 Scope 4 2 Normative references 4 3 Required characteristics .5 4 Designation 8 5 Marking .8 6 Technical specification .8 BS EN 4134:2009E

12、N 4134:2009 (E) 3 Foreword This document (EN 4134:2009) has been prepared by the Aerospace and 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

13、 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 status of a national standard, either by publication of an identical text or by endorsement, at the latest by October 2009, and conflicting nat

14、ional 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 the 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

15、/CENELEC Internal Regulations, the national standards organizations of the following countries are bound to implement this European Standard: Austria, Belgium, Bulgaria, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, L

16、uxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. BS EN 4134:2009EN 4134:2009 (E) 4 1 Scope This standard specifies the characteristics of bolts, normal hexagonal head, coarse tolerance normal shank, long thread,

17、in heat resisting nickel base alloy, aluminium IVD coated. Classification: 1 250 MPa 1) / 425 C 2)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

18、 edition of the referenced document (including any amendments) applies. EN 2424, Aerospace series Marking of aerospace products EN 2952, Aerospace series Heat resisting alloy NI-PH2601 Solution treated and cold worked Bar for forged fasteners D 50 mm 1 270 MPa Rm 1 550 MPa 3)EN 3219, Aerospace serie

19、s Heat resisting nickel base alloy (Ni-P100HT) Cold worked and softened Bar and wire for continuous forging or extrusion for fasteners 3 D 30 mm 3)EN 9100, Aerospace series Quality management systems Requirements (based on ISO 9001:2000) and Quality systems Model for quality assurance in design, dev

20、elopment, production, installation and servicing (based on ISO 9001:1994) EN 9133, Aerospace series Quality management systems Qualification procedure for aerospace standard parts ISO 3353-1, Aerospace Lead and runout threads Part 1: Rolled external threads ISO 5855-2, Aerospace MJ threads Part 2: L

21、imit dimensions for bolts and nuts ISO 7913, Aerospace Bolts and screws, metric Tolerances of form and position ISO 9154, Aerospace Bolts, with MJ threads, made of heat-resistant nickel-based alloy, strength class 1 550 MPa Procurement specification TR 3775, Aerospace series Bolts and pins Materials

22、 4) MIL-DTL-83488D, Coating, aluminium, high purity 5)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 th

23、e surface treatment. 3) Published as ASD Prestandard at the date of publication of this standard. 4) Published as ASD Technical Report at the date of publication of this standard. 5) Published by: Department of Defense (DOD), the Pentagon, Washington, D.C. 20301, USA. BS EN 4134:2009EN 4134:2009 (E)

24、 5 3 Required characteristics 3.1 Configuration Dimensions Masses See Figure 1 and Table 1. Dimensions and tolerances are expressed in millimetres and apply after surface treatment. 3.2 Tolerances of form and position ISO 7913 3.3 Materials EN 2952, EN 3219 or TR 3775 (heat resisting nickel base all

25、oy, classification 1 250 MPa) 3.4 Surface treatment MIL-DTL-83488D, type II, class 3, 7 m to 20 m After aluminium deposit: a) mechanical blasting, followed by a chromate conversion coating within 24 h max 6); b) optional lubrication with cethylic alcohol (code E). 6) Products used shall be in confor

26、mity with national regulation into force. BS EN 4134:2009EN 4134:2009 (E) 6 Values in micrometres 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 hole D6 optional 3 Thread 4 Conforms to

27、ISO 3353-1 5 Marking Figure 1 3,2 1,6 0,8 BS EN 4134:2009EN 4134:2009 (E) 7 Table 1 Diameter code Thread aD1D2D3D4bD5D6E F G H h12 min. 0 0,5 min. nom. Tol. H13 min. max. min. 0 0,3 030 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 7,6 0,5 2,5 050 MJ50,8 - 4h6h 5 7,4

28、5,25 7,4 3,4 0,5 1 8,7 3 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 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 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

29、 MJ141,5 - 4h6h 14 21,3 14,25 21 11,5 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 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 L1c, d, eL2c, d, eL3L4e, fN R Mass gnom. Tol. min. max. Length code nom.

30、 0 0,3 max. min. hi030 6 h12 0,4 2 12 014 to 042 14 to 42 0,4 0,2 1,254 0,114 040 7 14 016 to 056 16 to 56 2,193 0,202 050 8 3,25 0,5 4 16 020 to 070 20 to 70 2 0,5 0,3 3,938 0,316 060 10 h13 4,1 0,7 18 022 to 084 22 to 84 2,3 0,7 0,5 7,123 0,456 070 11 4,5 20 024 to 098 24 to 98 2, 7 9,792 0,622 08

31、0 13 5,35 22 026 to 112 26 to 112 3 14,961 0,814 100 17 7,1 0,8 6 25 032 to 140 32 to 140 3,4 0,8 0,6 28,741 1,270 120 19 7,9 0,9 30 036 to 168 36 to 168 4 0,9 46,437 1,830 140 22 9,2 1,1 34 040 to 196 40 to 196 4,7 1,1 0,8 69,365 2,490 160 24 10,05 38 044 to 224 44 to 224 5,4 101,783 3,256 180 27 1

32、1,3 1,3 42 048 to 252 48 to 252 6 1,3 1 142,691 4,118 200 30 12,6 46 052 to 280 52 to 280 6,7 194,120 5,082 aIn accordance with ISO 5855-2. bD4 max. shall be less than J. cFirst length corresponding to first L4length. dCondition L1min. and L2max. cannot be obtained simultaneously. eIncrements: - 2 f

33、or L4 100; - 4 for L4 100. fIf greater lengths are required, they shall be chosen using the above increments. The length code corresponds to the length L4, completed by one or two zeros to the left, where necessary, to obtain a three digit code. gApproximate values (kg/1 000 pieces), calculated on t

34、he basis of 8,195 kg/dm3, given for information purposes only. They apply to bolts without holes. h Value for head and first L4.i Increase for each additional 2 mm of L4. BS EN 4134:2009EN 4134:2009 (E) 8 4 Designation EXAMPLE Description block BOLT Identity block EN4134H050040E Number of this stand

35、ard Hole code (see Table 2) Diameter code (see Table 1) Length code (see Table 1) Lubrication code (see 3.4) NOTE If necessary the originator code I9005 shall be placed between the description block and the identity block. Table 2 Holes Code with H without (hyphen) 5 Marking See Table 3 and Figure 1

36、. Table 3 Diameter code EN 2424 Style 030 and 040 N 050 to 200 C + MJ 6 Technical specification 6.1 General ISO 9154, with the following modifications. BS EN 4134:2009EN 4134:2009 (E) 9 6.2 Approval of manufacturers EN 9100 6.3 Qualification of bolts EN 9133 6.4 Other modified requirement Test loads

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