SIST EN 2400:2020

Aerospace series - Heat resisting nickel base alloy Ni-P96-HT - Cold drawn and precipitation treated - Wires D ≤ 10 mm

This document specifies the requirements relating to:
Heat resisting nickel base alloy Ni-P96-HT
Cold drawn and precipitation treated
Wire
D ≤ 10 mm
for aerospace applications.

Luft- und Raumfahrt - Hochwarmfeste Nickelbasislegierung Ni-P96-HT - Kaltgezogen und Ausgelagert - Draht D ≤ 10 mm

Dieses Dokument legt die Anforderungen an:
Hochwarmfeste Nickelbasislegierung Ni-P96-HT
Kaltgezogen und ausgehärtet
Draht
D ≤ 10 mm
für Anwendungen in der Luft- und Raumfahrt fest.

Série aérospatiale - Alliage résistant à chaud à base de nickel Ni-P96-HT - Écroui et précipité - Fils D ≤ 10 mm

Le présent document spécifie les exigences relatives à :
Alliage résistant à chaud à base de nickel Ni-P96-HT
Étiré à froid et précipité
Fil
D ≤ 10 mm
pour applications aérospatiales.

Aeronavtika - Toplotnoodporne zlitine na nikljevi osnovi Ni-P96-HT - Hladno vlečene in izločevalno utrjene - Žice D ≤ 10 mm

Ta dokument določa zahteve, ki se navezujejo na: toplotno odporne zlitine na nikljevi osnovi Ni-P96-HT, hladno vlečene in izločevalno utrjene, žice, D ≤ 10 mm, za uporabo v aeronavtiki.

General Information

• Status: Published
• Publication Date: 11-Dec-2019
• ICS: 49.025.15 - Non-ferrous alloys in general
• ICS: 77.120.40 - Nickel, chromium and their alloys
• Technical Committee: I13 - Imaginarni 13
• Current Stage: 6060 - National Implementation/Publication (Adopted Project)
• Start Date: 06-Dec-2019
• Due Date: 10-Feb-2020
• Completion Date: 12-Dec-2019
• Ref Project: EN 2400:2019 - Aerospace series - Heat resisting nickel base alloy NI-P96-HT - Cold drawn and precipitation treated - Wire - D ≤ 10 mm

Overview

EN 2400:2019 (CEN) specifies requirements for heat‑resisting nickel‑base alloy Ni‑P96‑HT in the form of cold‑drawn, precipitation‑treated wire with diameter D ≤ 10 mm for aerospace applications. The European standard defines chemical composition limits, acceptable melting and production methods, delivery/heat‑treatment conditions and mandatory mechanical and dimensional requirements for use in high‑temperature aerospace environments.

Key topics and requirements

• Material and form: Ni‑P96‑HT alloy in wire form, cold drawn and precipitation treated, maximum diameter 10 mm.
• Chemical composition: Limits and controls for principal alloying elements (notably Ni, Co, Cr, Al, Ti, Zr and others) are specified to ensure heat‑resisting performance; exact composition tolerances are defined in the standard.
• Melting methods: Acceptable melting/refining routes include air melt with vacuum refining, vacuum melt or consumable electrode remelt - method to be agreed between manufacturer and purchaser.
• Heat treatment / delivery condition: Primary condition of use is cold drawn and precipitation treated; specified heat treatment example: 600 °C ±10 °C for 16 h followed by air cooling (alternative test heat treatment is defined if requested).
• Mechanical properties: High proof stress and tensile strength values are specified (examples in the standard show Rp0.2 up to ≥1 160 MPa and Rm values up to ≥1 540 MPa for particular diameter ranges). Minimum elongation (A50 mm ≥ 10 %) and other performance checks are provided.
• Testing & inspection: Dimensional inspection, marking, and mechanical testing (tension, bending, torsion/wrapping where applicable) are included; product qualification programs are to be agreed between supplier and purchaser.

Applications and who uses it

• Primary users: Aerospace materials engineers, component designers, wire manufacturers, quality assurance and procurement teams, and certification authorities.
• Typical uses: Procurement and specification of high‑temperature nickel‑base wires for aerospace components where high strength and heat resistance are required (wires up to 10 mm diameter used in manufacturing, forming, and assembly processes subject to elevated temperatures).
• Practical value: Ensures consistent chemical and mechanical performance, compatibility between suppliers and OEMs, and traceability for safety‑critical aerospace parts.

Related standards

• EN 2369 - Wires, heat resisting alloys - dimensions (0.2 mm ≤ D ≤ 8 mm)
• EN 4700‑004 - Aerospace series - Technical specification for wire wrought products
• EN 4258 and EN 4500‑003 - General organization and drafting rules for aerospace metallic material standards

Keywords: EN 2400:2019, Ni‑P96‑HT, heat resisting nickel base alloy, aerospace wire, cold drawn, precipitation treated, wire D ≤ 10 mm, CEN, aerospace standards.

Standards Content (Sample)

SLOVENSKI STANDARD
01-februar-2020
Aeronavtika - Toplotnoodporne zlitine na nikljevi osnovi Ni-P96-HT - Hladno
vlečene in izločevalno utrjene - Žice D ≤ 10 mm
Aerospace series - Heat resisting nickel base alloy Ni-P96-HT - Cold drawn and
precipitation treated - Wires D ≤ 10 mm
Luft- und Raumfahrt - Hochwarmfeste Nickelbasislegierung Ni-P96-HT - Kaltgezogen
und Ausgelagert - Draht D ≤ 10 mm
Série aérospatiale - Alliage résistant à chaud à base de nickel Ni-P96-HT - Écroui et
précipité - Fils D ≤ 10 mm
Ta slovenski standard je istoveten z: EN 2400:2019
ICS:
49.025.15 Neželezove zlitine na Non-ferrous alloys in general
splošno
77.120.40 Nikelj, krom in njune zlitine Nickel, chromium and their
alloys
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

EN 2400
EUROPEAN STANDARD
NORME EUROPÉENNE
November 2019
EUROPÄISCHE NORM
ICS 49.025.15
English Version
Aerospace series - Heat resisting nickel base alloy NI-P96-
HT - Cold drawn and precipitation treated - Wire - D ≤ 10
mm
Série aérospatiale - Alliage résistant à chaud à base de Luft- und Raumfahrt - Hochwarmfeste
nickel NI-P96-HT - Étiré à froid et précipité - Fil - D ≤ Nickelbasislegierung NI-P96-HT - Kaltgezogen und
10 mm ausgehärtet - Draht - D ≤ 10 mm
This European Standard was approved by CEN on 8 July 2018.

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 2400:2019 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 2400:2019) 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 May 2020, and conflicting national standards shall be
withdrawn at the latest by May 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 nation
...