SIST EN 4632-004:2014

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 004: Schweißen und Löten gleichartiger Verbindungen aus hochlegierten StählenSérie aérospatiale - Soudabilité et brasabilité des matériaux pour constructions aérospatiales - Partie 004: Assemblages soudés et brasés homogènes d’aciers fortement alliésAerospace series - Weldability and brazeability of materials in aerospace constructions - Part 004: Welding and brazing of homogeneous assemblies of high alloyed steels49.025.10JeklaSteels25.160.01Varjenje, trdo in mehko spajkanje na splošnoWelding, brazing and soldering in generalICS:Ta slovenski standard je istoveten z:EN 4632-004:2012SIST EN 4632-004:2014en01-marec-2014SIST EN 4632-004:2014SLOVENSKI
STANDARD
EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 4632-004
September 2012 ICS 49.025.01 English Version
Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 004: Welding and brazing of homogeneous assemblies of high alloyed steels
Série aérospatiale - Soudabilité et brasabilité des matériaux pour constructions aérospatiales - Partie 004: Assemblagessoudés et brasés homogènes d'aciers fortement alliés
Luft- und Raumfahrt - Schweißeignung und Löteignung von Werkstoffen im Luft- und Raumfahrzeugbau - Teil 004: Schweißen und Löten gleichartiger Verbingungen aus hochlegeirten Stähler This European Standard was approved by CEN on 23 March 2012.
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-CENELEC 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-CENELEC Management Centre has the same status as the official versions.
CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and United Kingdom.
EUROPEAN COMMITTEE FOR STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION EUROPÄISCHES KOMITEE FÜR NORMUNG
Management Centre:
Avenue Marnix 17,
B-1000 Brussels © 2012 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 4632-004:2012: ESIST EN 4632-004:2014

1) Published as ASD-STAN Prestandard at the date of publication of this standard (www.asd-stan.org). 2) Published as ASD-STAN Standard at the date of publication of this standard (www.asd-stan.org). SIST EN 4632-004:2014

EN 3510, Aerospace series — Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15) — Solution treated and precipitation treated — Bar and section — De ≤ 100 mm 1) EN 3529, Aerospace series — Steel FE-PM2701 (X2NiCoMo18-8-5) — Vacuum induction melted and vacuum arc remelted — Solution treated and precipitation treated — Forgings — a or D ≤ 150 mm — 1 750 MPa ≤ Rm ≤ 2 000 MPa 1) EN 3531, Aerospace series — Steel FE-PM2701 (X2NiCoMo18-8-5) — Vacuum induction melted and vacuum arc remelted — Solution treated and precipitation treated — Sheet and strip — a ≤ 6 mm — 1 750 MPa ≤ Rm ≤ 2 000 MPa EN 3532, Aerospace series — Steel FE-PM-2701 (X2NiCoMo18-8-5) — Vacuum induction melted and vacuum arc remelted — Solution treated and precipitation treated — Plate — 6 mm < a ≤ 40 mm — 1 750 MPa ≤ Rm ≤ 2 000 MPa EN 3677, Aerospace series — Steel FE-PM3801 (X5CrNiCu17-4) — Air melted — Solution treated and precipitation treated — Forgings — a or D ≤ 200 mm — Rm ≥ 1 310 MPa SIST EN 4632-004:2014

EN 3889, Aerospace series — Steel FE-WM3801 (X5CrNiCu17-4) — Filler metal for welding EN 3890, Aerospace series — Steel FE-WM1502 (X11CrNiMoVN12-3) — Filler metal for welding EN 4264, Aerospace series — Heat resisting alloy FE-PA2501 (X4NiCrMoTi43-13) — As forged — Forging stock — a or D ≤ 200 mm 1) EN 4314, Aerospace series — Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15) — Non heat treated, forging stock a or D ≤ 250 mm EN 4335, Aerospace series — Steel FE-WA2602 (X4NiCrTiMoV26-15) — Filler metal for welding — Wire and rod
EN 4346, Aerospace series — Steel FE-PM1505 (X1CrNiMoAlTi12-9-2) — Vacuum induction melted and consumable electrode remelted — Softened — Forging stock — a or D ≤ 300 mm
EN 4467, Aerospace series — Steel FE-PM1505 (X1CrNiMoAlTi12-9-2) — Vacuum induction melted and consumable electrode remelted — Solution treated and precipitation treated — Bar — a or D ≤ 150 mm — Rm ≥ 1 200 MPa
EN 4468, Aerospace series — Steel FE-PM1505 (X1CrNiMoAlTi12-9-2) — Vacuum induction melted and consumable electrode remelted — Solution treated and precipitation treated — Bar — a or D ≤ 150 mm — Rm ≥ 1 300 MPa EN 4469, Aerospace series — Steel FE-PM1505 (X1CrNiMoAlTi12-9-2) — Vacuum induction melted and consumable electrode remelted — Solution treated and precipitation treated — Bar — a or D ≤ 150 mm — Rm ≥ 1 400 MPa
EN 4470, Aerospace series — Steel FE-PM1505 (X1CrNiMoAlTi12-9-2) — Vacuum induction melted and consumable electrode remelted — Solution treated and precipitation treated — Forgings — a or D ≤ 150 mm — Rm ≥ 1 200 MPa EN 4471, Aerospace series — Steel FE-PM1505 (X1CrNiMoAlTi12-9-2) — Vacuum induction melted and consumable electrode remelted — Solution treated and precipitation treated — Forgings — a or D ≤ 150 mm — Rm ≥ 1 300 MPa EN 4472, Aerospace series — Steel FE-PM1505 (X1CrNiMoAlTi12-9-2) — Vacuum induction melted and consumable electrode remelted — Solution treated and precipitation treated — Forgings — a or D ≤ 150 mm —Rm ≥ 1 400 MPa EN 4570, Aerospace series — Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20) — Solution treated — Forgings — De ≤ 100 mm 1) EN 4571, Aerospace series — Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20) — Solution treated — Bar and section — De ≤ 100 mm 1) EN 4572, Aerospace series — Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20) — Solution treated — Sheet and strip — a ≤ 3 mm 1) EN 4573, Aerospace series — Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20) — Solution treated and precipitation treated — Bar and section — De ≤ 100 mm 1) SIST EN 4632-004:2014

3) Published by: Society of Automotive Engineers (SAE), (www.sae.org). 4) Published by: AWS, 550 N.W. LeJeune Road, Miami, Florida 33126, USA. SIST EN 4632-004:2014

PJHT : Post joining heat treatment PWHT : Post-weld heat treatment SIST EN 4632-004:2014

Current : Maraging 250 ASD-STAN : FE-PM2701
8.1.2 Chemical composition See Table 3. Table 3 — Typical chemical composition (w %) (on cast) Grade Fe C Ni Co Mo Ti Al Si Mn Zr P S B X2NiCoMo18-8-5 Base– 0,03 17,0 19,0 7,08,5 4,65,2 0,300,60 0,050,15 – 0,10 – 0,10 – 0,02 – 0,010 – 0,010– 0,003 8.1.3 Structure Martensitic with structural hardening 8.1.4 Particular characteristics High resisting steel for highly stressed parts Steel with good weldability 8.1.5 Forms Sheet and strip (EN 3531) – Forgings (EN 3529) – Plates (EN 3532). See Table 4. SIST EN 4632-004:2014

and corresponding EN ISO 4063 reference number Thickness range
mm State before welding PWHT Degree aof weldabilityJoint coefficientComments and
bibliographical references [ ] 141 ≤ 5 Solution treated Aged 480 °C during 4 h 1 1 [1] [2] Solution treated Solution treated and aged 1 1 [1] [8] Solution treated and aged Aged 480 °C during 4 h 1 – [8] Filler metal of same grade:
AMS 6501 PAW 15 pulsed ≤ 5 Solution treated Aged 480 °C during 4 h 1 1 [2] Compared with pulsed 141, this process allows to decrease proportions of retained austenite and to increase mechanical characteristics
Filler metal of same grade: AMS 6501 EBW 51 ≤ 2,5 Solution treated Aged 482 °C during 9 h 1 to 2 0,99 [9] ≤ 10 Solution treated Aged 480 °C during 4 h 1 to 2 1 [6]
Solution treated and aged Aged 480 °C during 4 h 1 to 2 –
FRW 42 ≤ 15 H2H3 b H3T2 c 1 1 [9] 522 ≤ 1 Solution treated Aged 480 °C during 4 h 1 to 2 1 – Solution treated and aged Aged 480 °C during 4 h 1 to 2 1
1 < t < 3 Solution treated Aged 480 °C during 4 h 1 to 2 0,92 [9] RSEW 22,
RSW 21 ≤ 4 Solution treated Aged 480°C during 4 h 1 – – Solution treated and aged Aged 480 °C during 4 h 1 –
FW 24 All Solution treated Solution treated and aged 1 – – T = 480 °C for 4 h. a If two degrees are indicated, the responsible person shall select the degree that is most appropriate for the definition of the assembly. b H2: 950 °C for 1 h – air cooled. c H3: 790 °C during 1 h – air cooled, T2: 455 °C for 9 h – air cooled.
EN 2821, EN 3361, EN 3469, EN 3479 : X5CrNiCu15-5 EN 10027-1 : Z5CNU15.05 ASD-STAN : FE-PM1802 EN 3160, EN 3161, EN 3162, EN 3677, EN 3678 : X5CrNiCu17-4 EN 10027-1 : Z5CNU17.04 ASD-STAN : FE-
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