BS EN 3150-1995 Pins shoulder headless in heat resisting nickel base alloy NI-P100HT (Inconel 718)《耐热镍基NI-P100HT(因康718)型合金肩部无头轴销》.pdf

1、BRITISH STANDARD AEROSPACE SERIES BS EN 3150:1995 Pins, shoulder, headless, in heat resisting nickel base alloy NI-P100HT (Inconel718) The European Standard EN3150:1995 has the status of a BritishStandardBSEN3150:1995 This BritishStandard, having been prepared under the directionof the Engineering S

2、ectorBoard, was published underthe authority of the Standards Board and comes intoeffect on 15 November 1995 BSI 12-1999 The following BSI references relate to the work on this standard: Committee reference ACE/12 Draft for comment88/78140DC ISBN 0 580 24486 5 Committees responsible for this British

3、Standard The preparation of this BritishStandard was entrusted to Technical Committee ACE/12, Aerospace fasteners and fastening systems, upon which the following bodies were represented: Association of Electronics, Telecommunications and Business Equipment Industries British Industrial Federation Mi

4、nistry of Defence Society of British Aerospace Companies Ltd. Amendments issued since publication Amd. No. Date CommentsBSEN3150:1995 BSI 12-1999 i Contents Page Committees responsible Inside front cover National foreword ii Foreword 2 1 Scope 3 2 Normative references 3 3 Required characteristics 3

5、4 Designation 5 5 Marking 5 6 Quality assurance 5 Figure 1 4 Table 1 5 List of references Inside back coverBSEN3150:1995 ii BSI 12-1999 National foreword This BritishStandard has been prepared by Technical Committee ACE/12 and is the English language version of EN3150:1995 Aerospace series Pins, sho

6、ulder, headless, in heat resistance nickel base alloy NI-P100HT (Inconel718), published by the European Committee for Standardization (CEN). EN3150:1995 was produced as a result of international discussions in which the United Kingdom took an active part. A British Standard does not purport to inclu

7、de all the necessary provisions of a contract. Users of British Standards are responsible for their correct application. Compliance with a British Standard does not of itself confer immunity from legal obligations. Cross-reference Publication referred to Corresponding BritishStandard EN2000:1991 BS

8、EN2000:1992 Quality assurance EN aerospace products Approval of the quality system of the manufacturers Summary of pages This document comprises a front cover, an inside front cover, pagesi andii, the EN title page, pages2 to6, an inside back cover and a back cover. This standard has been updated (s

9、ee copyright date) and may have had amendments incorporated. This will be indicated in the amendment table on the inside front cover.EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN3150 July 1995 ICS 49.040.20 Descriptors: Aircraft industry, locating pin, positioning, nickel alloy, heat resistan

10、t material, characteristic, dimension, designation English version Aerospace series Pins, shoulder, headless, in heat resiting nickel base alloy NI-P100HT (Inconel718) Srie arospatiale Pieds de centrage pauls, en alliage rsistant chaud base nickel NI-P100HT (Inconel718) Luft- und Raumfahrt Zylinders

11、tifte mit Bund, aus hochwarmfester Nickelbasislegierung NI-P100HT (Inconel718) This European Standard was approved by CEN on 1995-03-06. 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

12、 standard without any 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 ot

13、her language made by translation 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, Denmark, Finland, France, Germany, Greece, Iceland,

14、 Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and United Kingdom. CEN European Committee for Standardization Comit Europen de Normalisation Europisches Komitee fr Normung Central Secretariat: rue de Stassart 36, B-1050 Brussels 1995 Copyright reserved to CEN

15、members Ref. No. EN3150:1995 EEN3150:1995 BSI 12-1999 2 Foreword This European Standard has been prepared by the European Association of Aerospace Manufacturers (AECMA). After inquiries and votes carried out in accordance with the rules of this Association, this standard has successively received th

16、e approval of the National Associations and the Official Services of the member countries of AECMA, 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 1996,

17、and conflicting national standards shall be withdrawn at the latest by January 1996. According to the CEN/CENELEC Internal Regulations, the following countries are bound to implement this European Standard: Austria, Belgium, Denmark, Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxembo

18、urg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and United Kingdom.EN3150:1995 BSI 12-1999 3 1 Scope This standard specifies the characteristics of headless shoulder pins in NI-P100HT for aerospace applications. NOTEInstallation holes EN3368 2 Normative references This European Standa

19、rd incorporates by dated or undated reference provisions from other publications. These normative references are cited at the appropriate places in the text and the publications are listed hereafter. For dated references, subsequent amendments to or revisions of any of these publications apply to th

20、is European Standard only when incorporated in it by amendment or revision. For undated references the latest edition of the publication referred to applies. EN2000, Aerospace series Quality assurance EN aerospace products Approval of the quality system of manufacturers. EN2404, Heat resisting nicke

21、l base alloy NI-P100HT Solution treated and precipitation treated Bars Aerospace series 1) . EN2424, Aerospace series Marking of aerospace products. EN3368, Aerospace series Aerospace design standard Holes for locating pins 2) . 3 Required characteristics 3.1 Configuration Dimensions Tolerances Mass

22、es See Figure 1 and Table 1. Dimensions and tolerances are in millimetres. 3.2 Material EN2404 1) Published as AECMA Standard at the date of publication of this standard 2) Published as AECMA Prestandard at the date of publication of this standardEN3150:1995 4 BSI 12-1999 Figure 1 EN3150:1995 BSI 12

23、-1999 5 Table 1 4 Designation EXAMPLE: NOTEIf necessary, the codeI9005 shall be placed between the description block and the identity block. 5 Marking EN2424, style G 6 Quality assurance EN2000 Diameter code A B C D Length code L Mass kg/1000 pieces . 0 0,3 0 0,2 0 0,25 nom. Tol. nom. Tol. 030 3 r6

24、4,1 2,6 0,5 0,1 055 5,5 0,717 075 7,5 0,95 040 4 p6 5,1 3,6 055 5,5 1,257 075 7,5 1,699 050 5 6,1 4,6 1 0,2 055 5,5 1,944 075 7,5 2,59 060 6 7,1 5,6 055 5,5 2,783 075 7,5 3,729 070 7 8,1 6,6 055 5,5 3,772 075 7,5 5,112 080 8 9,1 7,6 055 5,5 4,912 075 7,5 6,565 100 10 11,1 9,6 055 5,5 7,643 075 7,5 1

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