EN 3510:2019

Aerospace series - Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15) - Solution treated and precipitation treated - Bars and sections - De ≤ 100 mm

This document specifies the requirements relating to:
Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15)
Solution treated and precipitation treated
Bars and sections
De ≤ 100 mm

Luft- und Raumfahrt - Hochwarmfeste Legierung FE-PA2602 (X4NiCrTiMoV26-15) - Lösungsgeglüht und ausgehärtet - Stangen und Profile - De ≤ 100 mm

Série aérospatiale - Alliage résistant à chaud FE-PA2602 (X4NiCrTiMoV26-15) - Mis en solution et précipité - Barres et profilés - De ≤ 100 mm

Le présent document spécifie les exigences relatives à :
Alliage résistant à chaud FE-PA2602 (X4NiCrTiMoV26-15) Mis en solution et précipité Barres et profilés De ≤ 100 mm
pour applications aérospatiales.

Aeronavtika - Toplotno odporna zlitina FE-PA2602 (X4NiCrTiMoV26-15) - Topilno žarjena in izločevalno utrjena - Palice in profili - De ≤ 100 mm

Ta dokument določa zahteve, ki se navezujejo na:
toplotno odporno zlitino FE-PA2602 (X4NiCrTiMoV26-15),
topilno žarjeno in izločevalno utrjeno,
palice in profile
De ≤ 100 mm
za uporabo v aeronavtiki.

General Information

• Status: Published
• Publication Date: 17-Sep-2019
• Withdrawal Date: 30-Mar-2020
• ICS: 49.025.05 - Ferrous alloys in general
• Technical Committee: ASD-STAN - Aerospace
• Drafting Committee: ASD-STAN/D 4 - Metallic
• Current Stage: 6060 - Definitive text made available (DAV) - Publishing
• Start Date: 18-Sep-2019
• Completion Date: 18-Sep-2019
• Ref Project: SIST EN 3510:2019 - Aerospace series - Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15) - Solution treated and precipitation treated - Bar and section - De ≤ 100 mm

Overview

EN 3510:2019 specifies requirements for the aerospace heat‑resisting alloy FE‑PA2602 (X4NiCrTiMoV26‑15) in the form of bars and sections with an external diameter (De) ≤ 100 mm. Published by CEN and prepared by ASD‑STAN, this standard defines metallurgical, heat‑treatment and mechanical property requirements for solution treated and precipitation (age) treated product intended for aerospace applications.

Key topics and requirements

• Material designation: FE‑PA2602 (also referenced as X4NiCrTiMoV26‑15) - a nickel‑chromium based heat‑resisting alloy containing Ti, Mo and V. Chemical composition is defined in the standard (see Table 1).
• Product form and manufacture: Bars and sections, wrought production; melting method specified as consumable electrode remelted.
• Size limit: External diameter (De) ≤ 100 mm.
• Heat treatment / delivery condition:
  • Solution treatment: 980 °C ± 10 °C, t ≥ 14 h, air cool (AC).
  • Precipitation (age) treatment: 720 °C ± 10 °C, t = 16 h, air cool. Delivery condition codes W and U denote solution treated and solution + precipitation treated states.
• Mechanical properties:
  • Proof stress (p0.2) ≥ 580 MPa
  • Tensile strength (Rm) ≥ 850 MPa
  • Elongation A ≥ 20 %
  • Hardness ≥ 235 HB
  • Elevated‑temperature rupture: at 650 °C, tR ≥ 30 h → rupture stress σR = 410 MPa and elongation at rupture A ≥ 3.5 %
• Testing and inspection: Test specimen directions, dimensional, marking and visual inspections are referenced to EN 3235‑3; grain size and defect class requirements are specified.

Applications and users

EN 3510:2019 is targeted at suppliers, manufacturers, procurement and quality/engineering teams in the aerospace and defence sectors who specify or produce semi‑finished metallic bars and sections for high‑temperature aerospace components. Typical applications include structural and engine‑related parts where long‑term strength and heat resistance are required (specified product qualification and testing apply between purchaser and manufacturer).

Related standards

• EN 3235‑3 - Technical specification for heat resisting alloy bars and sections (referenced for tests and product requirements)
• EN 2043 - General requirements for semi‑finished product qualification
• EN 4258 - Organization of aerospace metallic material standards
• EN 4500‑005 - Rules for drafting material standards (steels)

Keywords: EN 3510:2019, FE‑PA2602, X4NiCrTiMoV26‑15, heat resisting alloy, solution treated, precipitation treated, aerospace bars, EN 3235‑3.

Standards Content (Sample)

SLOVENSKI STANDARD
01-december-2019
Aeronavtika - Toplotno odporna zlitina FE-PA2602 (X4NiCrTiMoV26-15) - Topilno
žarjena in izločevalno utrjena - Palice in profili - De ≤ 100 mm
Aerospace series - Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15) - Solution
treated and precipitation treated - Bar and section - De ≤ 100 mm
Luft- und Raumfahrt - Hochcarmfeste Legierung FE-PA2602 (X4NiCrTiMoV26-15) -
Lösungsgeglüht und ausgehärtet - Stangen und Profile - De ≤ 100 mm
Série aérospatiale - Alliage résistant à chaud FE-PA2602 (X4NiCrTiMoV26-15) - Mis en
solution et précipité - Barres et profilés - De ≤ 100 mm
Ta slovenski standard je istoveten z: EN 3510:2019
ICS:
49.025.05 Železove zlitine na splošno Ferrous alloys in general
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

EN 3510
EUROPEAN STANDARD
NORME EUROPÉENNE
September 2019
EUROPÄISCHE NORM
ICS 49.025.05
English Version
Aerospace series - Heat resisting alloy FE-PA2602
(X4NiCrTiMoV26-15) - Solution treated and precipitation
treated - Bars and sections - De ≤ 100 mm
Série aérospatiale - Alliage résistant à chaud FE- Luft- und Raumfahrt - Hochwarmfeste Legierung FE-
PA2602 (X4NiCrTiMoV26-15) - Mis en solution et PA2602 (X4NiCrTiMoV26-15) - Lösungsgeglüht und
précipité - Barres et profilés - De ≤ 100 mm ausgehärtet - Stangen und Profile - De ≤ 100 mm
This European Standard was approved by CEN on 22 April 2019.

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, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway,
Poland, Portugal, Republic of North Macedonia, Romania, Serbia, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and
United Kingdom.
EUROPEAN COMMITTEE FOR STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION

EUROPÄISCHES KOMITEE FÜR NORMUNG

CEN-CENELEC Management Centre: Rue de la Science 23, B-1040 Brussels
© 2019 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 3510:2019 E
worldwide for CEN national Members.

Contents Page
European foreword . 3
Introduction . 4
1 Scope . 5
2 Normative references . 5
3 Terms and definitions . 5
4 Requirements . 5
Bibliography . 9

European foreword
This document (EN 3510:2019) has been prepared by the Aerospace and Defence Industries Association
of Europe - Standardization (ASD-STAN).
After enquiries and votes carried out 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 publication of an
identical text or by endorsement, at the latest by March 2020, and conflicting national standards shall be
withdrawn at the latest by March 2020.
Attention is drawn to the possibility that some of the elements of this document may be the subject of
patent rights. CEN shall not be held responsible for identifying any or all such patent rights.
According to the CEN-CENELEC Internal Regulations, the
...