BS EN 3948-1998 Nickel base alloy NI-B15701 (NiPd34Au30) - Filler metal for brazing - Wire《镍基合金NI-B15701(NiPd34Au30) 铜焊用填充金属 线材》.pdf

《BS EN 3948-1998 Nickel base alloy NI-B15701 (NiPd34Au30) - Filler metal for brazing - Wire《镍基合金NI-B15701(NiPd34Au30) 铜焊用填充金属 线材》.pdf》由会员分享，可在线阅读，更多相关《BS EN 3948-1998 Nickel base alloy NI-B15701 (NiPd34Au30) - Filler metal for brazing - Wire《镍基合金NI-B15701(NiPd34Au30) 铜焊用填充金属 线材》.pdf（12页珍藏版）》请在麦多课文档分享上搜索。

1、BRITISH STANDARD AEROSPACE SERIES BS EN 3948:1998 Nickel base alloy NI-B15701 (NiPd34Au30) Fillermetal for brazing Wire The European Standard EN 3948:1998 has the status of a British Standard ICS 49.025.99BSEN3948:1998 This British Standard, having been prepared under the directionof the Engineering

2、 SectorBoard, was published underthe authorityof the Standards Boardand comes intoeffect on 15July 1998 BSI 04-1999 ISBN 0 580 30127 3 National foreword This British Standard is the English language version of EN3948:1998. The UK participation in its preparation was entrusted to Technical Committee

3、ACE/61, Inspection and testing requirements for aerospace metallic materials, which has the responsibility to: aid enquirers to understand the text; present to the responsible international/European committee any enquiries on the interpretation, or proposals for change, and keep the UK interests inf

4、ormed; monitor related international and European developments and promulgate them in the UK. A list of organizations represented on this committee can be obtained on request to its secretary. Cross-references The British Standards which implement international or European publications referred to i

5、n this document may be found in the BSI Standards Catalogue under the section entitled “International Standards Correspondence Index”, or by using the “Find” facility of the BSI Standards Electronic Catalogue. A British Standard does not purport to include all the necessary provisions of a contract.

6、 Users of British Standards are responsible for their correct application. Compliance with a British Standard does not of itself confer immunity from legal obligations. Summary of pages This document comprises a front cover, an inside front cover, pages i and ii, theENtitlepage, pages2 to6 and a bac

7、k cover. This standard has been updated (see copyright date) and may have had amendments incorporated. This will be indicated in the amendment table on the inside front cover. Amendments issued since publication Amd. No. Date CommentsBSEN3948:1998 BSI 04-1999 i Contents Page National foreword Inside

8、 front cover Foreword 2 Text of EN 3948 3ii blankEUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN3948 April1998 ICS Descriptors: Aircraft industry, filler metals, brazing, nickel alloys, wire, designation, chemical composition, delivery condition, characteristics, specifications English version

9、Aerospace series Nickel base alloy NI-B15701 (NiPd34Au30) Filler metal for brazing Wire Srie arospatiale Alliage base nickel NI-B15701 (NiPd34Au30) Mtal dapport de brasage Fil Luft- und Raumfahrt Nickelbasislegierung NI-B15701 (NiPd34Au30) Hartlot in Form von Draht This European Standard was approve

10、d by CEN on24 November1997. 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 st

11、andards 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 translation under the responsibility of a CEN member into its own language and notified

12、to the Central Secretariat has the same status as the official versions. CEN members are the national standards bodies of Austria, Belgium, Czech Republic, Denmark, Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and Un

13、ited Kingdom. CEN European Committee for Standardization Comit Europen de Normalisation Europisches Komitee fr Normung Central Secretariat: rue de Stassart 36, B-1050 Brussels 1998 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 39

14、48:1998 EEN3948:1998 BSI 04-1999 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 the approval of the Nat

15、ional 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 October1998, and conflicting nation

16、al standards shall be withdrawn at the latest by October1998. According to the CEN/CENELEC Internal Regulations, the national standards organizations of the following countries are bound to implement this European Standard: Austria, Belgium, Czech Republic, Denmark, Finland, France, Germany, Greece,

17、 Iceland, Ireland, Italy, Luxembourg, the Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and the United Kingdom. Contents Page Foreword 2 0 Introduction 3 1 Scope 3 2 Normative references 3EN3948:1998 BSI 04-1999 3 0 Introduction This standard is part of the series of EN metallic material

18、 standards for aerospace applications. The general organization of this series is described in EN4258. This standard has been prepared in accordance with EN4500-6. 1 Scope This standard specifies the requirements relating to: Nickel base alloy NI-B15701 (NiPd34Au30) Filler metal for brazing Wire for

19、 aerospace applications. 2 Normative references This European Standard 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

20、 amendments to or revisions of any of these publications apply to this European Standard only when incorporated in it by amendment or revision. For undated references the latest edition of the publication referred to applies. EN 2043, Aerospace series Metallic materials General requirements for semi

21、-finished product qualification (excluding forgings and castings) 1) . EN 3875, Aerospace series Metallic materials Filler metal for brazing Technical specification 1) . EN 4258, Aerospace series Metallic materials General organization of standardization Links between types of EN standards and their

22、 use 1) . EN 4500-6, Aerospace series Metallic materials Rules for drafting and presentation of material standards Part 6: Specific rules for filler metals for brazing 1) . 1) Published as AECMA Prestandard at the date of publication of this standardEN3948:1998 4 BSI 04-1999 1 Material designation N

23、ickel base braze alloy NI-B15701 (NiPd34Au30) 2 Chemical composition % Element Au Pd Others Ni Total min. 29,5 33,5 35,5 max. 30,5 34,5 0,15 36,5 3 Method of melting Inert gas or vacuum melted 4.1 Form Wire 4.2 Method of production Cold drawn or cold rolled or cold extruded 4.3 Limit dimension(s) mm

24、 5 Technical specification EN 3875 6.1 Delivery condition As manufactured Heat treatment 6.2 Delivery condition code U 7 Use condition Delivery condition Heat treatment Characteristics 8.1 Test sample(s) 8.2 Test piece(s) 8.3 Heat treatment 9 Dimensions concerned mm 10 Thickness of cladding on each

25、face % 11 Direction of test piece 12 Temperature C 13 Proof stress R p0,2 MPa 14 T Strength R m MPa 15 Elongation A % 16 Reduction of area Z % 17 Hardness 18 Shear strength R c MPa 19 Bending k 20 Impact strength 21 Temperature C 22 Time h 23 Stress B a MPa 24 C Elongation a % 25 Rupture stress B R

26、MPa 26 Elongation at rupture A % 27 Notes (see line 98) EN3948:1998 BSI 04-1999 5 44 External defects See EN 3875 53 Thermal analysis (Differential thermal analysis) See EN 3875 7 Liquidus: 1 165 C Solidus: 1 135 C 76 Wettability (Fusion test) See EN 3875 82 Batch uniformity (Material verification)

27、See EN 3875 95 Marking inspection See EN 3875 96 Dimensional inspection See EN 3875 98 Notes 99 Typical use Joining nickel and cobalt base alloys.EN3948:1998 6 BSI 04-1999 100 Product qualification See EN 2043 Qualification programme to be agreed between manufacturer and purchaser.blankBS EN 3948:19

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