EN 4135-2009 en Aerospace series - Bolts normal bi-hexagonal head coarse tolerance normal shank medium length thread in titanium alloy anodized MoS2 lubricated - Classification 1 1.pdf

1、BS EN 4135:2009ICS 49.030.20NO COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGHT LAWBRITISH STANDARDAerospace series Bolts, normal bi-hexagonal head, coarse tolerance normal shank, medium length thread, in titanium alloy, anodized, MoS2 lubricated Classification: 1 100 MPa (at ambient

2、temperature) / 315 nullCThis British Standardwas published under theauthority of the StandardsPolicy and StrategyCommittee on 31 July 2009 BSI 2009ISBN 978 0 580 68583 5Amendments/corrigenda issued since publicationDate CommentsBS EN 4135:2009National forewordThis British Standard is the UK implemen

3、tation of EN 4135:2009.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 n

4、ecessary provisionsof a contract. Users are responsible for its correct application.Compliance with a British Standard cannot confer immunityfrom legal obligations.BS EN 4135:2009EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 4135 July 2009 ICS 49.030.20 English Version Aerospace series - Bolt

5、s, normal bi-hexagonal head, coarse tolerance normal shank, medium length thread, in titanium alloy, anodized, MoS2 lubricated - Classification: 1 100 MPa (at ambient temperature) / 315 C Srie arospatiale - Vis tte bihexagonale normale, tige normale tolrance large, filetage moyen, en alliage de tita

6、ne, anodises, lubrifies MoS2 - Classification : 1 100 MPa ( temprature ambiante) / 315 C Luft- und Raumfahrt - Zwlfkantschrauben, mittlere Gewindelnge, aus Titanlegierung, anodisiert, MoS2-geschmiert - Klasse: 1 100 MPa (bei Raumtemperatur) / 315 C This European Standard was approved by CEN on 6 Jun

7、e 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 standards may be obtai

8、ned 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 to the CEN Managem

9、ent 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, Netherlands, Norwa

10、y, 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 exploitation in any form a

11、nd by any means reserved worldwide for CEN national Members. Ref. No. EN 4135:2009: EBS EN 4135:2009EN 4135:2009 (E) 2 Contents Page Foreword 3 1 Scope 4 2 Normative references 4 3 Required characteristics .4 4 Designation 7 5 Marking .7 6 Technical specification .7 BS EN 4135:2009EN 4135:2009 (E) 3

12、 Foreword This document (EN 4135:2009) 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 National Associa

13、tions 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 January 2010, and conflicting national standards s

14、hall be withdrawn at the latest by January 2010. 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/CENELEC Internal

15、 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, Luxembourg, Malta,

16、 Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. BS EN 4135:2009EN 4135:2009 (E) 4 1 Scope This standard specifies the characteristics of bolts, normal bi-hexagonal head, coarse tolerance normal shank, medium length thread, in ti

17、tanium alloy, anodized, MoS2lubrificated. Classification: 1 100 MPa 1) / 315 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 r

18、eferenced document (including any amendments) applies. EN 2424, Aerospace series Marking of aerospace products. EN 2491, Aerospace series Molybdenum disulphide dry lubricants Coating methods. EN 9100, Aerospace series Quality management systems Requirements (based on ISO 9001:2000) and Quality syste

19、ms 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 3185, Aerospace Bolts, normal bihexagonal head, normal shank, short o

20、r 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 4095, Aerospace Bihexagonal drives Wrenching configuration Metric series. ISO 5855-2, Aer

21、ospace MJ threads 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 M

22、aterials.3) TR 4070, Aerospace series Molybdenum disulphide coatings List of commercial products. 3)3 Required characteristics 3.1 Configuration Dimensions Masses See Figure 1 and Table 1. 1) Minimum tensile strength of the material at ambient temperature. 2) Maximum temperature that the bolt can wi

23、thstand without continuous change in its original characteristics, 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. BS EN 4135:2009EN 4135:2009 (E) 5 Dimensions and t

24、olerances are: in conformity with ISO 3185, expressed in millimetres and apply after anodizing but before lubricating. 3.2 Tolerances of form and position ISO 7913 3.3 Materials TR 3775 (titanium alloy, classification 1 100 MPa) 3.4 Surface treatment Lubrification: a) Lubricant: see Clause 4; b) App

25、lication: EN 2491, 5 m to 10 m. Values in micrometres apply prior to surface treatment. Break sharp edges 0,1 to 0,4. Key 1 Radius 0,3 min. 2 1 hole D8 optional 3 Thread 4 Conforms to ISO 3353-1 5 Shape optional 6 Marking 7 4 holes D7 equidistant optional aRounded or chamfered in this area. Figure 1

26、 3,2 1,6 0,8 BS EN 4135:2009EN 4135:2009 (E) 6 Table 1 Diameter code Thread aD1D2D3D4D5D6D7D8H K h12 + 0,5 0 0,5 min. min. max. H13 H13 min. h15 050 MJ50,8 - 4h6h 5 3,2 3,4 6,8 8,3 9,1 1 1,5 1 6,5 060 MJ61 - 4h6h 6 4,1 4,2 7,8 9,8 10,6 1,4 1,2 7,5 070 MJ71 - 4h6h 7 4,9 5,2 8,8 11,3 12,1 1,9 1,4 8,2

27、080 MJ81 - 4h6h 8 5,2 6,2 9,8 12,8 13,6 1,6 8,6 100 MJ101,25 - 4h6h 10 6,7 7,9 11,8 15,7 16,7 1,6 2,4 2 10,1 120 MJ121,25 - 4h6h 12 8 9,8 13,7 18,8 19,9 2,4 11,4 Diameter code L1 0,2 b, cL2L3P R S T Wrenching dash number dMass eLength code Nom. Nom. Tol. + 0,40 min.fg050 003 to 050 3 to 50 12 7,5 4,

28、5 0,5 0 0,2 2,5 2,8 07 2,201 0,087 060 003 to 060 3 to 60 14 8,5 5,2 0,7 2,8 3,5 08 3,350 0,126 070 004 to 070 4 to 70 15 9,5 5,9 3,3 3,8 09 4,925 0,171 080 004 to 080 4 to 80 16,5 10,5 6,3 3,7 3,9 10 7,012 0,224 100 005 to 100 5 to 100 20,5 13 7,7 0,8 4,7 4,2 12 12,897 0,349 120 006 to 120 6 to 120

29、 22,5 14,5 8,8 0,9 0 0,3 5,6 4,5 14 21,155 0,503 aIn accordance with ISO 5855-2. bIncrements: 1 for L1 30; 2 for 30 100. cIf greater lengths are required, they shall be chosen using the above increments. The length code corresponds to the length L1, completed by one or two zeros to the left, where n

30、ecessary, to obtain a three digit code. dIn accordance with ISO 4095 over T min. e Approximate 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 each additional millim

31、etre of L4. BS EN 4135:2009EN 4135:2009 (E) 7 4 Designation EXAMPLE Description block BOLT Identity block EN4135H050040F Number of this standard Hole code (see Table 2) Diameter code (see Table 1) Length code (see Table 1) Lubricant code (see TR 4070) NOTE If necessary the originator code I9005 shou

32、ld 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 EN 2424, style B (see Figure 1). 6 Technical specification ISO 9152, except for clauses: a) Approval of manufacturers: see EN 9100; b) Qual

33、ification of bolts: see EN 9133. BS EN4135:2009BSI GroupHeadquarters 389Chiswick High Road,London, W4 4AL, UKTel +44 (0)20 8996 9001Fax +44 (0)20 8996 - British Standards InstitutionBSI is the independent national body responsible for preparing BritishStandards. It presents the UK view on standards

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