SIST EN 4632-005:2010
(Main)Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 005: Homogeneous assemblies of heat resisting Ni or Co base alloys
Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 005: Homogeneous assemblies of heat resisting Ni or Co base alloys
This European Standard 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 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 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.
Luft- und Raumfahrt - Schweißbarkeit und Lötbarkeit von Werkstoffen im Luft und Raumfahrzeugbau - Teil 005: Schweißen und Löten gleichartiger Verbindungen aus hitzebeständigen Nickel- oder Kobaltbasislegierungen
Diese Europäische Norm legt den Schweißbarkeits- und Lötbarkeitsgrad für in der Luft- und Raumfahrtindustrie
verwendete Werkstoffe oder Werkstofffamilien fest.
Sie enthält eine Serie von Datenblättern, eingeteilt nach Werkstoffen und Werkstofffamilien, die:
⎯ die Haupttitel, die typische chemische Zusammensetzung und die Haupteigenschaften angeben;
⎯ Empfehlungen zum Schweißen und Hartlöten enthalten;
⎯ den Schweißbarkeits- oder Lötbarkeitsgrad für einen bestimmten Prozess unter festgelegten
Bedingungen angeben;
⎯ einen Wert für den Faktor der mechanischen Festigkeit der Schweißnaht für jeden Schweißprozess
angeben, wenn er Literaturhinweisen entnommen werden kann, die Bezug auf diesen nehmen. Der
Verbindungskoeffizient wird als Verhältnis der Zugfestigkeit der Schweißnaht zur Zugfestigkeit der Basislegierung
angegeben (in Übereinstimmung mit EN 4632-002).
Sie gilt ohne Einschränkung für die Fertigung von neuen Teilen oder für die Instandsetzung.
2
Série aérospatiale - Soudabilité et brasabilité des matériaux pour constructions aérospatiales - Partie 005: Assemblages homogènes des alliages base Ni ou Co résistant à haute température
Aeronavtika - Varivost in spajkljivost materialov v aeronavtičnih konstrukcijah - 005. del: Varjenje in spajkanje homogenih sestavov iz nikljeve ali kobaltove osnovne zlitine, odporne proti vročini
Ta evropski standard opredeljuje stopnje varivosti in spajkljivosti materialov ali skupin materialov, ki se uporabljajo v aeronavtični industriji. Sestavlja ga niz listov, po materialih ali skupini materiala, ki: - navajojo glavne naslove, kemično sestavo in glavne značilnosti; - vsebujejo priporočila za varjenje in spajkanje; - navajajo stopnjo varivosti ali spajkljivosti za določen postopek pod opredeljenimi pogoji; - navajajo vrednost koeficienta mehanske trdnosti varjenega spoja za vsak postopek varjenja, kadar ga je mogoče povzeti iz bibliografskih sklicev, ki se nanašajo nanj. Koeficient spoja je izražen kot razmerje med natezno trdnostjo varjenega spoja in natezno trdnostjo osnovne zlitine (mora biti v skladu z EN 4632-002). Velja brez omejitev za proizvodnjo novih delov ali za popravila.
General Information
Standards Content (Sample)
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Luft- und Raumfahrt - Schweißbarkeit und Lötbarkeit von Werkstoffen im Luft und Raumfahrzeugbau - Teil 005: Schweißen und Löten gleichartiger Verbindungen aus hitzebeständigen Nickel- oder KobaltbasislegierungenSérie aérospatiale - Soudabilité et brasabilité des matériaux pour constructions aérospatiales - Partie 005: Assemblages homogènes des alliages base Ni ou Co résistant à haute températureAerospace series - Weldability and brazeability of materials in aerospace constructions - Part 005: Homogeneous assemblies of heat resisting Ni or Co base alloys49.025.15Neželezove zlitine na splošnoNon-ferrous alloys in general25.160.01Varjenje, trdo in mehko spajkanje na splošnoWelding, brazing and soldering in generalICS:Ta slovenski standard je istoveten z:EN 4632-005:2009SIST EN 4632-005:2010en01-februar-2010SIST EN 4632-005:2010SLOVENSKI
STANDARD
EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 4632-005
December 2009 ICS 49.025.01 English Version
Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 005: Homogeneous assemblies of heat resisting Ni or Co base alloys
Série aérospatiale - Assemblages soudés et brasés pour constructions aérospatiales - Soudabilité et brasabilité des matériaux - Partie 005: assemblage homogènes des alliages base Ni ou Co résistant à haute température
Luft- und Raumfahrt - Schweißbarkeit und Lötbarkeit von Werkstoffen im Luft und Raumfahrzeugbau- - Teil 005: Schweißen und Löten gleichartiger Verbindungen aus hitzebeständigen Nickel- oder Kobaltbasislegierungen This European Standard was approved by CEN on 12 September 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 obtained 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 Management 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, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom.
EUROPEAN COMMITTEE FOR STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION EUROPÄISCHES KOMITEE FÜR NORMUNG
Management Centre:
Avenue Marnix 17,
B-1000 Brussels © 2009 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 4632-005:2009: ESIST EN 4632-005:2010
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 resisting 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-PH1303 (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 (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 of publication of this standard. SIST EN 4632-005:2010
EN 2657, Aerospace series — Heat resisting alloy CO-PH1402 — Consumable electrode remelted — Solution treated — Bar — a or D ≤ 150 mm — Rm ≥ 860 MPa 2) EN 2658, Aerospace series — Heat resisting alloy CO-PH1402 — Consumable electrode remelted — As forged — Forging stock — De ≤ 360 mm 2) EN 2659, Aerospace series — Heat resisting alloy CO-PH1402 — Consumable electrode remelted — Solution treated — Forgings — De ≤ 100 mm — Rm ≥ 860 MPa 2) EN 2661, Aerospace series — Heat resisting alloy CO-PH1402 — Consumable electrode remelted — Solution treated — Sheet and strip — a ≤ 3 mm — Rm ≥ 860 MPa 2) EN 2662, Aerospace series — Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) — Annealed — Sheet, strip and plate — 0,2 mm ≤ a ≤ 10 mm 2) EN 2663, Aerospace series — Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) — Solution treated — Sheet, strip and plate — 0,2 mm ≤ a ≤ 10 mm 2) EN 2959, Aerospace series — Heat resisting alloy NI-PH1302 (NiCr20Co13Mo4Ti3Al) — Solution treated and cold worked — Bar for forged fasteners — 3 mm ≤ D ≤ 30 mm 2) EN 3668, Aerospace series — Heat resisting 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 mm
EN 3884, Aerospace series — Heat resisting alloy NI-WH2601 (NiCr19Nb5Mo3Ti) — Filler metal for welding EN 3887, 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 — Precision castings 2) EN 4222, Aerospace series — Heat resisting alloy NI-PH1305 (NiCr22Co13Mo9Al1) — Air melted and vacuum refined — Annealed — Sheet and strip — 0,25 mm ≤ a ≤ 3 mm 2) EN 4327, Aerospace series — Heat resisting alloy CO-WH1401 (CoCr26Ni11W8) — Filler metal for welding — Wire and rod EN 4329, Aerospace series — Heat 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 mm 2) EN 4377, Aerospace series — Heat resisting alloy NI-PH2601 (NiCr19Fe19Nb5Mo3) — Non heat treated — Forging stock — a or D ≤ 300 mm 2)
2) Published as ASD-STAN Prestandard at the date of publication of this standard. SIST EN 4632-005:2010
EN 4381, Aerospace series — Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) — Solution treated — Seamless tubes — For structural application — D ≤ 50 mm, a ≤ 3 mm 3) EN 4382, Aerospace series — Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) — 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 — Forgings — De ≤ 100 mm 3) EN 4567, Aerospace series — Heat resisting alloy CO-PH4101 (CoCr20W15Ni) — Vacuum melted — Solution treated — Bar and section — a or D ≤ 100 mm 3) EN 4568, Aerospace series — Heat resisting alloy CO-PH4101 (CoCr20W15Ni) — Vacuum melted — Solution treated — Sheet and strip — a ≤ 6 mm 3) EN 4569, Aerospace series — 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 brazed 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 4063:2009)
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, investment 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 heat-resistant, investment castings 62Ni - 21.5Cr - 9.0Mo - 3.6Cb (Nb) as cast 4)
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. SIST EN 4632-005:2010
AMS 5580, Nickel alloy, corrosion and heat resistant, seamless tubing 74Ni - 15.5Cr - 8.0Fe annealed 5) AMS 5665, Nickel alloy, corrosion and heat resistant, bars, forgings, and rings 74Ni - 15.5Cr - 8.0Fe 5) AMS 5687, Nickel alloy, corrosion and heat resistant, wire 74Ni - 15.5Cr - 8.0Fe annealed 5) 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 For 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 : Flash 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 - Warrendale, PA 15096-0001 USA. 6) Published by: AWS, 550 N.W. LeJeune Road, Miami, F
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