BS EN 2856-2006 Aerospace series - Nuts anchor self-locking fixed closed corner reduced series with counterbore - Classification 1100 MPa 235 C《航空和航天系列 自锁固定式锐角缩径有沉孔的地脚螺母 分类 1100 MP.pdf

《BS EN 2856-2006 Aerospace series - Nuts anchor self-locking fixed closed corner reduced series with counterbore - Classification 1100 MPa 235 C《航空和航天系列 自锁固定式锐角缩径有沉孔的地脚螺母 分类 1100 MP.pdf》由会员分享，可在线阅读，更多相关《BS EN 2856-2006 Aerospace series - Nuts anchor self-locking fixed closed corner reduced series with counterbore - Classification 1100 MPa 235 C《航空和航天系列 自锁固定式锐角缩径有沉孔的地脚螺母 分类 1100 MP.pdf（10页珍藏版）》请在麦多课文档分享上搜索。

1、BRITISH STANDARD AEROSPACE SERIESBS EN2856:2006Nuts, anchor, self-locking, fixed, closed corner, reduced series, with counterbore Classification: 1 100 MPa/235 CThe European Standard EN 2856:2006 has the status of a British StandardICS 49.030.30g49g50g3g38g50g51g60g44g49g42g3g58g44g55g43g50g56g55g3g

2、37g54g44g3g51g40g53g48g44g54g54g44g50g49g3g40g59g38g40g51g55g3g36g54g3g51g40g53g48g44g55g55g40g39g3g37g60g3g38g50g51g60g53g44g42g43g55g3g47g36g58Licensed Copy: Wang Bin, na, Wed Aug 23 03:12:17 BST 2006, Uncontrolled Copy, (c) BSIBS EN 2856:2006This British Standard was published under the authority

3、 of the Standards Policy and Strategy Committee on 30 June 2006 BSI 2006ISBN 0 580 48554 4National forewordThis British Standard is the official English language version of EN 2856:2006. The UK participation in its preparation was entrusted to Technical Committee ACE/12, Aerospace fasteners and fast

4、ening systems, which has the responsibility to: A list of organizations represented on this committee can be obtained on request to its secretary.Cross-referencesThe British Standards which implement international or European publications referred to in this document may be found in the BSI Catalogu

5、e under the section entitled “International Standards Correspondence Index”, or by using the “Search” facility of the BSI Electronic Catalogue 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

6、 application. Compliance with a British Standard does not of itself confer immunity from legal obligations. aid enquirers to understand the text; present to the responsible international/European committee any enquiries on the interpretation, or proposals for change, and keep UK interests informed;

7、monitor related international and European developments and promulgate them in the UK.Summary of pagesThis document comprises a front cover, an inside front cover, the EN title page, pages 2 to 7 and a back cover.The BSI copyright notice displayed in this document indicates when the document was las

8、t issued.Amendments issued since publicationAmd. No. Date CommentsLicensed Copy: Wang Bin, na, Wed Aug 23 03:12:17 BST 2006, Uncontrolled Copy, (c) BSIEUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 2856 June 2006 ICS 49.030.30 English Version Aerospace series - Nuts, anchor, self-locking, fixe

9、d, closed corner, reduced series, with counterbore - Classification: 1 100 MPa/235 C Srie arospatiale - crous river freinage interne fixes, angle ferm, srie rduite avec chambrage - Classification : 1 100 MPa/235 C Luft- und Raumfahrt - Annietmuttern, selbstsichernd, einseitiger verkzter Eck-Flansch

10、mit zylindrischer Aussenkung - Klasse: 1 100 MPa/235 C This European Standard was approved by CEN on 9 March 2006. 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

11、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 other language made by t

12、ranslation 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, France, Germany, Greec

13、e, 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 EUROPISCHES KOMITEE FR NORMUNG Managemen

14、t Centre: rue de Stassart, 36 B-1050 Brussels 2006 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 2856:2006: ELicensed Copy: Wang Bin, na, Wed Aug 23 03:12:17 BST 2006, Uncontrolled Copy, (c) BSI2 Contents Page Foreword3 1 Scope 4

15、 2 Normative references 4 3 Required characteristics.5 4 Designation 7 5 Marking .7 6 Technical specification .7 EN 2856:2006Licensed Copy: Wang Bin, na, Wed Aug 23 03:12:17 BST 2006, Uncontrolled Copy, (c) BSI3 Foreword This European Standard (EN 2856:2006) has been prepared by the European Associa

16、tion of Aerospace Manufacturers - Standardization (AECMA-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 AECMA, prior to its presen

17、tation 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 December 2006, and conflicting national standards shall be withdrawn at the latest by December 2006. Attention is drawn to the possib

18、ility 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 following countries are

19、 bound to implement this European Standard: Austria, Belgium, 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, Switzer

20、land and the United Kingdom. EN 2856:2006Licensed Copy: Wang Bin, na, Wed Aug 23 03:12:17 BST 2006, Uncontrolled Copy, (c) BSI4 1 Scope This standard specifies requirements for closed corner, counterbored, fixed, reduced series anchor nuts, with a self-locking feature achieved by forming the upper p

21、ortion out-of-round. These nuts are intended for use in aircraft assemblies, in which the fasteners are mainly objected to shear loads. The counterbore is deep enough to accommodate a bolt shank in excess of assembly thickness, as well as the incomplete threads. They are intended to be used with thr

22、eaded parts of 1 100 MPa 1)tensile strength classification. The cadmium plating restricts the application to temperature not exceeding 235 C. 2 Normative references The following referenced documents are indispensable for the application of this document. For dated references, only the edition cited

23、 applies. For undated references, the latest edition of the referenced document (including any amendments) applies. ISO 3222, Aerospace Nuts, anchor, self-locking, fixed, closed corner, reduced series, with counterbore, with MJ threads, classifications: 1 100 MPa (at ambient temperature)/235 C, 1 10

24、0 MPa (at ambient temperature)/315 C and 1 100 MPa (at ambient temperature)/425 C Dimensions. ISO 5855-2, Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts. ISO 5858, Aerospace Nuts, self-locking, with maximum operating temperature less than or equal to 425 C Procurement specification

25、. ISO 8788, Aerospace Nuts, metric Tolerances of form and position. EN 2133, Aerospace series Cadmium plating of steels with specified tensile strength 1 450 MPa, copper, copper alloys and nickel alloys. EN 2424, Aerospace series Marking of aerospace products. EN 2491, Aerospace series Molybdenum di

26、sulphide dry lubricants Coating methods. EN 2542, Aerospace series Steel FE-PL43S Annealed Bar and wire De 40 mm for prevailing torque nuts. 2)EN 2543, Aerospace series Steel FE-PL43S Annealed Sheet and strip 0,3 a 2 mm for prevailing torque nuts. 2)EN 9100, Aerospace series Quality management syste

27、ms 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). 1) This strength class applies at room temperatures. 2) Published as AECMA Prestandard at the date of publication of this

28、standard. EN 2856:2006Licensed Copy: Wang Bin, na, Wed Aug 23 03:12:17 BST 2006, Uncontrolled Copy, (c) BSI5 3 Required characteristics 3.1 Configuration Dimensions Tolerances The configuration shall be in accordance with Figure 1; the dimensions and tolerances shall conform to the values shown in F

29、igure 1 and Table 1, after cadmium plating but before MoS2lubrication. The dimensions are in conformity with ISO 3222 and the geometrical tolerances with ISO 8788. Details of form not defined are at the option of the manufacturer. 3.2 Surface roughness See Figure 1. Values apply prior to cadmium pla

30、ting and lubrication. They do not apply to the thread, sheared edges and punched edges; the surface roughness will be as achieved by normal methods of manufacture. 3.3 Materials Steel EN 2542 or EN 2543. 3.4 Surface treatment Cadmium plating EN 2133, 5 m minimum on the threads and all areas which ca

31、n be contacted by a 20 mm diameter ball. On all other areas, a continuous deposit shall be present, but no minimum value is specified. Lubrication by MoS2EN 2491, mandatory on threads, optional on other surfaces. EN 2856:2006Licensed Copy: Wang Bin, na, Wed Aug 23 03:12:17 BST 2006, Uncontrolled Cop

32、y, (c) BSI6 Remove sharp edges 0,1 to 0,4 Y-Y Key 1 Group of 2 holes 2,5 020,+2 Form out-of-round in this area to achieve the self-locking requirement (tooling marks permissible) 3 Pitch diameter 4 Thread 5 Applicable over a diameter equal to 2 K 6 Radius or chamfer 7 Part marking in these areas Fig

33、ure 1 Configuration 6,3 3,2 EN 2856:2006Licensed Copy: Wang Bin, na, Wed Aug 23 03:12:17 BST 2006, Uncontrolled Copy, (c) BSI7 Table 1 Dimensions and mass Dimensions in millimetres Thread a Code Designation E F G min.H min. J b max.K max.L max.M max.N c max. R aux. W max. Mass kg/1 000 piecesmax. 04

34、0 MJ 4 0,7 - 4H6H 6 5,5 4,4 2,2 6,2 4 12 5,8 1 2,5 10,5 1,1 050 MJ 5 0,8 - 4H6H 7 5,5 5,5 2,4 7,3 4,5 13,6 6,9 1 2,5 10,5 1,6 060 MJ 6 1 - 4H5H 8 5,5 6,5 2,7 8,7 5 15,7 8,1 1,2 3 11,5 2,2 aIn conformity with ISO 5855-2. In the self-locking zone, the tolerances apply before deformation. bIs to sharp

35、corners (chamfered) or point of tangency (radiused). cIs applicable at the rivet hole location. 4 Designation Each nut shall only be designated as in the following example EXAMPLE Description block NUT, ANCHOR Identity block EN2856-060 Number of EN Standard Thread code (see Table 1) NOTE If necessar

36、y, the code I9005 shall be placed between the description block and the identity block. 5 Marking Each nut shall be marked in any of the positions shown in Figure 1 in accordance with EN 2424, style N. 6 Technical specification Conforming to ISO 5858 except for quality assurance requirements See EN

37、9100 EN 2856:2006Licensed Copy: Wang Bin, na, Wed Aug 23 03:12:17 BST 2006, Uncontrolled Copy, (c) BSIBS EN 2856:2006BSI389 Chiswick High RoadLondonW4 4ALBSI British Standards InstitutionBSI is the independent national body responsible for preparing British Standards. It presents the UK view on stan

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