EN 4632-005-2009 en Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 005 Homogeneous assemblies of heat resisting Ni or Co base alloys.pdf

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1、BS EN4632-005:2009ICS 49.025.01NO COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGHT LAWBRITISH STANDARDAerospace series Weldability andbrazeability ofmaterials in aerospaceconstructionsPart 005: Homogeneous assemblies ofheat resisting Ni or Co base alloysThis British Standardwas publis

2、hed under theauthority of the StandardsPolicy and StrategyCommittee on 31 March2010 BSI 2010ISBN 978 0 580 58876 1Amendments/corrigenda issued since publicationDate CommentsBS EN 4632-005:2009National forewordThis British Standard is the UK implementation of EN 4632-005:2009.The UK participation in

3、its preparation was entrusted to TechnicalCommittee ACE/61/-/2, Heat Treatment of Metallic Materials forAerospace Purposes.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 co

4、ntract. Users are responsible for its correct application.Compliance with a British Standard cannot confer immunityfrom legal obligations.BS EN 4632-005:2009EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 4632-005 December 2009 ICS 49.025.01 English Version Aerospace series - Weldability and br

5、azeability of materials in aerospace constructions - Part 005: Homogeneous assemblies of heat resisting Ni or Co base alloys Srie arospatiale - Assemblages souds et brass pour constructions arospatiales - Soudabilit et brasabilit des matriaux - Partie 005: assemblage homognes des alliages base Ni ou

6、 Co rsistant haute temprature Luft- und Raumfahrt - Schweibarkeit und Ltbarkeit von Werkstoffen im Luft und Raumfahrzeugbau- - Teil 005: Schweien und Lten gleichartiger Verbindungen aus hitzebestndigen Nickel- oder Kobaltbasislegierungen This European Standard was approved by CEN on 12 September 200

7、9. 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 obtained o

8、n 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 Management C

9、entre 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, Norway, Po

10、land, 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 and by

11、 any means reserved worldwide for CEN national Members. Ref. No. EN 4632-005:2009: EBS EN 4632-005:2009EN 4632-005:2009 (E) 2 Contents Page Foreword 31 Scope 42 Normative references 43 Terms, definitions, symbols and abbreviations .74 Use of this standard 85 Updating this standard 86 List of heat re

12、sisting Ni or Co base alloys 87 Heat resisting Ni or Co base alloys9BS EN 4632-005:2009EN 4632-005:2009 (E) 3 Foreword This document (EN 4632-005:2009) has been prepared by the Aerospace and Defence Industries Association of Europe - Standardization (ASD-STAN). After enquiries and votes carried out

13、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 ASD, prior to its presentation to CEN. This European Standard shall be given the status of a national standard, either by public

14、ation of an identical text or by endorsement, at the latest by June 2010, and conflicting national standards shall be withdrawn at the latest by June 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 n

15、ot 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 bound to implement this European Standard: Austria, Belgium, Bulgaria, Cyprus, Czech Republic, Denmark, Estonia

16、, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. BS EN 4632-005:2009EN 4632-005:2009 (E) 4 1 Scope This European Standard

17、defines degrees of weldability and brazeability for materials or families of materials used in the aerospace industry. It comprises a series of sheets, by materials or by material family, which: indicate the main titles, the chemical composition and the main characteristics; contain recommendations

18、for welding and brazing; indicate a degree of weldability or brazeability for a given process under defined conditions; indicate a value of the mechanical strength coefficient of the welded joint for each welding process, when it could be extracted from bibliographic references referring to it. The

19、joint coefficient is expressed as a ratio of the tensile strength of the welded joint to the tensile strength of the base alloy (to be in accordance with EN 4632-002). It is applicable without restriction for the manufacturing of new parts or for repair. 2 Normative references The following referenc

20、ed 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 2161, Aerospace series Heat resisting alloy CO-CH1401 (CoCr26Ni11W)

21、Not heat treated Precision castings 1)EN 2183, Aerospace series Heat resisting alloy NI-PH2301 (NiCr21Fe18Mo9) Solution treated Forging De 200 mm 1)EN 2184, Aerospace series Heat resisting alloy NI-PH2301 (NiCr21Fe18Mo9) Solution treated Bar and section De 200 mm 1)EN 2185, Aerospace series Heat res

22、isting alloy NI-PH2301 (NiCr21Fe18Mo9) Solution treated Sheet, strip and plate 0,2 mm a 10 mm 1)EN 2199, Aerospace series Heat resisting alloy NI-PH1303 (NiCo20Cr20Mo5Ti2Al) Solution treated and precipitation treated Bar and section De 200 mm 1)EN 2203, Aerospace series Heat resisting alloy NI-PH130

23、3 (NiCo20Cr20Mo5Ti2Al) Solution treated Sheet, strip and plate 0,2 mm a 10 mm 1)EN 2204, Aerospace series Heat resisting alloy NI-CH1303 (NiCo20Cr20Mo5Ti2Al) Vacuum melted Solution treated and precipitation treated Precision casting De 50 mm 1)EN 2403, Aerospace series Heat resisting alloy NI-CH2601

24、 (NiCr19Fe19Nb5Mo3) Vacuum melted Solution treated and precipitation treated Precision casting a or D 50 mm 1)EN 2405, Aerospace series Heat resisting alloy NI-PH2601 (NiCr19Fe19Nb5Mo3) Solution treated and precipitation treated Forgings De 200 mm 1)1) Published as ASD-STAN Prestandard at the date o

25、f publication of this standard. BS EN 4632-005:2009EN 4632-005:2009 (E) 5 EN 2407, Aerospace series Heat resisting alloy NI-PH2601 (NiCr19Fe19Nb5Mo3) Solution treated and precipitation treated Sheet, strip and plate 0,2 mm a 10 mm 2)EN 2657, Aerospace series Heat resisting alloy CO-PH1402 Consumable

26、 electrode remelted Solution treated Bar a or D 150 mm Rm 860 MPa2)EN 2658, Aerospace series Heat resisting alloy CO-PH1402 Consumable electrode remelted As forged Forging stock De 360 mm2)EN 2659, Aerospace series Heat resisting alloy CO-PH1402 Consumable electrode remelted Solution treated Forging

27、s De 100 mm Rm 860 MPa2)EN 2661, Aerospace series Heat resisting alloy CO-PH1402 Consumable electrode remelted Solution treated Sheet and strip a 3 mm Rm 860 MPa2)EN 2662, Aerospace series Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) Annealed Sheet, strip and plate 0,2 mm a 10 mm2)EN 2663, Aerospace

28、 series Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) Solution treated Sheet, strip and plate 0,2 mm a 10 mm2)EN 2959, Aerospace series Heat resisting alloy NI-PH1302 (NiCr20Co13Mo4Ti3Al) Solution treated and cold worked Bar for forged fasteners 3 mm D 30 mm2)EN 3668, Aerospace series Heat resisting

29、alloy NI-PH2301 (NiCr21Fe18Mo9) Non heat treated Forging stock a or D 250 mm EN 3671, Aerospace series Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) Non heat treated Forging stock a or D 250 mmEN 3884, Aerospace series Heat resisting alloy NI-WH2601 (NiCr19Nb5Mo3Ti) Filler metal for welding EN 3887,

30、Aerospace series Heat resisting alloy CO-WH4101 (CoCr20W15Ni) Filler metal for welding EN 3888, Aerospace series Heat resisting alloy CO-WH1402 (CoCr22Ni22W15) Filler metal for welding EN 4095, Aerospace series Heat resisting alloy NI-CH1305 (NiCr16Co10Mo8Al4Ti4) Vacuum melted Non heat treated Preci

31、sion castings2)EN 4222, Aerospace series Heat resisting alloy NI-PH1305 (NiCr22Co13Mo9Al1) Air melted and vacuum refined Annealed Sheet and strip 0,25 mm a 3 mm2)EN 4327, Aerospace series Heat resisting alloy CO-WH1401 (CoCr26Ni11W8) Filler metal for welding Wire and rod EN 4329, Aerospace series He

32、at resisting alloy NI-WH0001 (NiCr20) Filler metal for welding Wire and rod EN 4376, Aerospace series Heat resisting alloy NI-PH2601 (NiCr19Fe19Nb5Mo3) Solution treated and precipitation treated Bar and section De 200 mm2)EN 4377, Aerospace series Heat resisting alloy NI-PH2601 (NiCr19Fe19Nb5Mo3) No

33、n heat treated Forging stock a or D 300 mm2)2) Published as ASD-STAN Prestandard at the date of publication of this standard. BS EN 4632-005:2009EN 4632-005:2009 (E) 6 EN 4379, Aerospace series Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) Solution treated Forging De 200 mm EN 4380, Aerospace series

34、Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) Solution treated Bar and section De 200 mm 3)EN 4381, Aerospace series Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) Solution treated Seamless tubes For structural application D 50 mm, a 3 mm3)EN 4382, Aerospace series Heat resisting alloy NI-PH3601 (NiCr2

35、2Mo9Nb) Solution treated Seamless tubes For hydraulic application D 50 mm, a 3 mm EN 4384, Aerospace series Heat resisting alloy NI-CH1303 (NiCo20Cr20Mo5Ti2Al) Non heat treated Remelting stock EN 4566, Aerospace series Heat resisting alloy CO-PH4101 (CoCr20W15Ni) Vacuum melted Solution treated Forgi

36、ngs De 100 mm3)EN 4567, Aerospace series Heat resisting alloy CO-PH4101 (CoCr20W15Ni) Vacuum melted Solution treated Bar and section a or D 100 mm3)EN 4568, Aerospace series Heat resisting alloy CO-PH4101 (CoCr20W15Ni) Vacuum melted Solution treated Sheet and strip a 6 mm3)EN 4569, Aerospace series

37、Heat resisting alloy CO-PH4101 (CoCr20W15Ni) Vacuum melted Solution treated Wire D 4 mm 3)EN 4632-001:2008, Aerospace series Welded and brazed assemblies for aerospace constructions Weldability and brazeability of materials Part 001: General requirements EN 4632-002, Aerospace series Welded and braz

38、ed assemblies for aerospace constructions Weldability and brazeability of materials Part 002: Homogeneous asssemblies aluminium and aluminium alloys EN 10095, Heat resisting steels and nickel alloys EN ISO 4063:2009, Welding and allied processes Nomenclature of processes and reference numbers (ISO 4

39、063:2009) EN ISO 18274, Welding consumables Wire and strips electrodes, wires and rods for fusion welding of nickel and nickel alloys Classification (ISO 18274:2004) ISO 9722, Nickel and nickel alloys Composition and forms of wrought products AMS 5390, Nickel alloy, corrosion and heat resistant, inv

40、estment castings 47.5Ni - 22Cr - 1.5Co - 9Mo - 0.60W - 18.5Fe (N-12mv) as cast 4)AMS 5399, Nickel alloy, corrosion and heat resistant, investment castings 52Ni - 19Cr - 11Co - 9.8Mo - 3.2Ti - 1.6Al - 0.006B vacuum-melted, vacuum-cast, solution heat treated 4)AMS 5402, Nickel alloy, corrosion and hea

41、t-resistant, investment castings 62Ni - 21.5Cr - 9.0Mo - 3.6Cb (Nb) as cast4)3) Published as ASD-STAN Prestandard at the date of publication of this standard. 4) Published by: SAE, 400 Commonwealth Drive - Warrendale, PA 15096-0001 USA. BS EN 4632-005:2009EN 4632-005:2009 (E) 7 AMS 5540, Nickel allo

42、y, corrosion and heat resistant, sheet, strip, and plate 74Ni - 15.5Cr - 8.0Fe annealed 5)AMS 5580, Nickel alloy, corrosion and heat resistant, seamless tubing 74Ni - 15.5Cr - 8.0Fe annealed5)AMS 5665, Nickel alloy, corrosion and heat resistant, bars, forgings, and rings 74Ni - 15.5Cr - 8.0Fe5)AMS 5

43、687, Nickel alloy, corrosion and heat resistant, wire 74Ni - 15.5Cr - 8.0Fe annealed5)AWS A5.14, Specification for Nickel and Nickel Alloy Bare Welding Electrodes and Rods 6)AWS A5.8-92, Specification for filler metals for brazing and braze welding 6)3 Terms, definitions, symbols and abbreviations F

44、or the purposes of this document, the terms and definitions given in EN 4632-001:2008 and EN ISO 4063:2009 apply. F : Foil p : Powder PJHT : Post joining heat treatment PWHT : Post-weld heat treatment w : Wire 15 : Plasma arc welding 21 : Resistance spot welding 22 : Resistance seam welding 24 : Fla

45、sh welding 42 : Friction welding 51 : Electron beam welding 52 : Laser welding 91 : Brazing with local heating 111 : Shielded metal arc welding 141 : Gas tungsten arc welding 522 : Gas laser welding 521 : Solid state laser welding 922 : Vacuum brazing 5) Published by: SAE, 400 Commonwealth Drive - W

46、arrendale, PA 15096-0001 USA. 6) Published by: AWS, 550 N.W. LeJeune Road, Miami, Florida 33126. BS EN 4632-005:2009EN 4632-005:2009 (E) 8 4 Use of this standard The index of material sheets contained in this standard, classified by family based on the main element used in the chemical composition a

47、nd on the alloy structure, is given in Clause 6. The degree of weldability or brazeability (see EN 4632-001) to be used is the value indicated by the material sheet considered for the process chosen. In the operating cycle, preferably select thermal states that give the lowest degree. If two degrees

48、 are indicated, the responsible person shall select the degree that is most appropriate for the definition of the assembly. 5 Updating this standard See EN 4632-001. 6 List of heat resisting Ni or Co base alloys Table 1 Sheet Material 7.1 7.2 7.3 7.4 7.5 7.6 7.7 7.8 7.9 7.10 7.11 7.12 7.13 7.14 7.15 7.16 7.17 7.18 NiCr15Fe NiCr16Co10Mo8Al4Ti4 NiCr19Fe19Nb5Mo3 NiCr19Fe19Nb5Mo3 NiCr19Co11Mo10Ti3 NiCr20Co13Mo4Ti3Al NiCr20Nb NiCr20Ti Ni