1、BS EN 4133:2009ICS 49.030.20,NO COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGHT LAWBRITISH STANDARDAerospace series Bolts, normalhexagonal head, coarsetolerance normalshank, long thread,in titanium alloy,aluminium IVD coated Classification: 1100 MPa (at ambienttemperature) / 425 CThi
2、s British Standardwas published under theauthority of the StandardsPolicy and StrategyCommittee on 31 May 2009 BSI 2009ISBN 978 0 580 65952 2Amendments/corrigenda issued since publicationDate CommentsBS EN 4133:2009National forewordThis British Standard is the UK implementation of EN 4133:2009.The U
3、K 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 provisionsof a cont
4、ract. Users are responsible for its correct application.Compliance with a British Standard cannot confer immunityfrom legal obligations.BS EN 4133:2009EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 4133 April 2009 ICS 49.030.20 English Version Aerospace series - Bolts, normal hexagonal head, c
5、oarse tolerance normal shank, long thread, in titanium alloy, aluminium IVD coated - Classification: 1 100 MPa (at ambient temperature) / 425 C Srie arospatiale - Vis tte hexagonale normale, tige normale tolrance large, filetage long, en alliage de titane, revtues aluminium IVD - Classification: 1 1
6、00 MPa ( temprature ambiante)/425 C Luft- und Raumfahrt - Sechskantschrauben, langes Gewinde, aus Titanlegierung, Aluminium 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/CENEL
7、EC 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 standards may be obtained on application to the CEN Management Centre or to any
8、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 to the CEN Management Centre has the same status as the official versions. C
9、EN 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, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, S
10、weden, 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 exploitation in any form and by any means reserved worldwide for CEN national Member
11、s. Ref. No. EN 4133:2009: EBS EN 4133:2009EN 4133:2009 (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 4133:2009EN 4133:2009 (E) 3 Foreword This document (EN 4133:2009) has been prepared b
12、y 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 National Associations and the Official Services of the member countries of
13、 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 national standards shall be withdrawn at the latest by October 2009. Attention
14、 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/CENELEC Internal Regulations, the national standards organizations of the
15、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, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia,
16、 Slovenia, Spain, Sweden, Switzerland and the United Kingdom. BS EN 4133:2009EN 4133:2009 (E) 4 1 Scope This standard specifies the characteristics of bolts, normal hexagonal head, coarse tolerance normal shank, long thread, in titanium alloy, aluminium IVD coated. Classification: 1 100 MPa 1) / 425
17、 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 edition of the referenced document (including any amendments) applies. EN 2424, Aerospace se
18、ries Marking of aerospace products EN 9100, Aerospace series Quality management 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 mana
19、gement 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: Limit dimensions for bolts and nuts ISO 7913, Aerospace Bolts and screws, metric Tolerances of form and position
20、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-DTL-83488D, Coating, aluminium, high purity 4)1) Minimum tensile strength of the material at ambient temperature. 2) Maximum te
21、mperature that the bolt can withstand without continuous change in its original characterictics, after return to ambient temperature. The maximum temperature is determined by the surface treatment 3) Published as ASD Technical Report at the date of publication of this standard. 4) Published by: Depa
22、rtment of Defense (DOD), the Pentagon, Washington, D.C. 20301, USA. BS EN 4133:2009EN 4133:2009 (E) 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 f
23、orm 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 m After aluminium deposit: a) mechanical blasting, followed by a chromate conversion coating within 24 h max. 5); b) optional lubrification wit
24、h cethylic alcohol (code E). 5) Products used shall be in conformity with national regulation into force. BS EN 4133:2009EN 4133:2009 (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
25、 Continuous surface 2 2 hole D6 optional 3 Thread 4 Conforms to ISO 3353-1 5 Marking Figure 1 3,2 1,6 0,8 BS EN 4133:2009EN 4133:2009 (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 04
26、0 MJ40,7 - 4h6h 4 6,4 6,4 3 7,6 0,5 2,5 050 MJ50,8 - 4h6h 5 7,4 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
27、 5 2,35 120 MJ121,25 - 4h6h 12 18,3 12,25 18 9,8 21,1 6 2,85 140 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,
28、eL2c, d, eL3L4e, fN R Mass gnom. Tol. min. max. Length code nom. 0 0,3 max. min. hi030 6 h12 0,4 2 12 014 to 042 14 to 42 0,4 0,2 0,681 0,062 040 7 14 016 to 056 16 to 56 1,191 0,110 050 8 3,25 0,5 4 16 020 to 070 20 to 70 2 0,5 0,3 2,138 0,172 060 10 h13 4,1 0,7 18 022 to 084 22 to 84 2,3 0,7 0,5 3
29、,868 0,248 070 11 4,5 20 024 to 098 24 to 98 2, 7 5,317 0,342 080 13 5,35 22 026 to 112 26 to 112 3 8,124 0,448 100 17 7,1 0,8 6 25 032 to 140 32 to 140 3,4 0,8 0,6 15,607 0,698 120 19 7,9 0,9 30 036 to 168 36 to 168 4 0,9 25,216 0,994 140 22 9,2 1,1 34 040 to 196 40 to 196 4,7 1,1 0,8 37,666 1,352
30、160 24 10,05 38 044 to 224 44 to 224 5,4 55,269 1,768 180 27 11,3 1,3 42 048 to 252 48 to 252 6 1,3 1 77,483 2,236 200 30 12,6 46 052 to 280 52 to 280 6,7 105,410 2,760 aIn accordance with ISO 5855-2. bD4 max. shall be less than J. cFirst length corresponding to first L4length. dCondition L1min. and
31、 L2max. cannot be obtained simultaneously. eIncrements: - 2 for 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
32、 code. gApproximate 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. h Value for head and first L4.i Increase for each additional 2 mm of L4. BS EN 4133:2009EN 4133:2009 (E) 8 4 Designation EXAMPLE Description b
33、lock BOLT Identity block EN4133H050040E 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 originator code I9005 shall be placed between the description block and the identity block. Table 2 Holes Cod
34、e with H without (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 specification ISO 9152, except for clauses: a) Approval of manufacturers: See EN 9100; b) Qualification of bolts: See EN 9133. BS EN 4133:2009This pag
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