Aerospace series - Heat-resisting alloy NI-PH1301 (NiCr19Co18Mo4Ti3Al3) - Solution treated and precipitation treated - Bars and sections - De ≤ 200 mm

This document specifies the requirements relating to:
Heat-resisting alloy NI-PH1301 (NiCr19Co18Mo4Ti3Al3)
Solution treated and precipitation treated
Bars and sections
De ≤ 200 mm
for aerospace applications.

Luft- und Raumfahrt - Hochwarmfeste Legierung NI-PH1301 (NiCr19Co18Mo4Ti3Al3) - Lösungsgeglüht und ausscheidungsgehärtet - Stangen und Profile - De ≤ 200 mm

Série aérospatiale - Alliage résistant à chaud NI-PH1301 (NiCr19Co18Mo4Ti3Al3) - Mis en solution et précipité - Barres et profilés - De ≤ 200 mm

Le présent document spécifie les exigences relatives à :
Alliage résistant à chaud NI-PH1301 (NiCr19Co18Mo4Ti3Al3)
Mis en solution et précipité
Barres et profilés
De ≤ 200 mm
pour les applications aérospatiales.

Aeronavtika - Toplotno odporna zlitina NI-PH1301 (NiCr19Co18Mo4Ti3Al3) - Topilno žarjena in izločevalno utrjena - Palice in profili - De ≤ 200 mm

Ta dokument določa zahteve, ki se navezujejo na:
toplotno odporno zlitino NI-PH1301 (NiCr19Co18Mo4Ti3Al3),
topilno žarjeno in izločevalno utrjeno,
palice in profile,
De ≤ 200 mm,
za uporabo v aeronavtiki.

General Information

Status
Published
Publication Date
22-Jan-2023
Technical Committee
I13 - Imaginarni 13
Current Stage
6060 - National Implementation/Publication (Adopted Project)
Start Date
04-Jan-2023
Due Date
11-Mar-2023
Completion Date
23-Jan-2023

Overview

SIST EN 4374:2023 is a European standard developed by CEN that specifies technical requirements for the heat-resisting alloy NI-PH1301 (NiCr19Co18Mo4Ti3Al3). This alloy is designed for aerospace applications where exceptional heat resistance and mechanical performance are critical. The standard covers solution treated and precipitation treated forms of the alloy, specifically in bars and sections with external diameters (De) up to 200 mm.

This standard ensures quality, consistency, and suitability of NI-PH1301 alloy products for high-temperature aerospace environments. It forms part of the wider aerospace metallic materials series, aligned with other CEN standards focused on aerospace steel and heat-resistant alloys.


Key Topics

  • Material Composition: Covers detailed chemical composition of NI-PH1301 alloy with specified minimum and maximum limits for elements such as Nickel (Ni), Chromium (Cr), Cobalt (Co), Molybdenum (Mo), Titanium (Ti), Aluminum (Al), Carbon (C), Silicon (Si), and others, ensuring optimal heat resistance and structural integrity.

  • Heat Treatment Processes: Defines solution treatment at 1175 °C ± 10 °C followed by air cooling, and precipitation treatment involving controlled heating cycles at 1080 °C and aging at 850 °C and 760 °C to enhance mechanical properties.

  • Product Form and Dimensions: Applicable to wrought bars and sections with external diameters not exceeding 200 mm, providing flexibility in manufacturing for a variety of aerospace components.

  • Mechanical Properties: Specifies minimum requirements for proof stress (Rp0.2 ≥ 340 MPa), rupture stress (≥ 370 MPa), and elongation at rupture (≥ 8%), to guarantee mechanical robustness under operational conditions.

  • Quality and Inspection: References EN 4700-002 for testing methods, inspection procedures for internal and external imperfections, grain size, microstructure, and dimensional accuracy to maintain strict aerospace quality standards.

  • Product Qualification: Emphasizes the need for agreed qualification programs between manufacturers and purchasers per EN 2043, ensuring products meet intended aerospace application demands.


Applications

SIST EN 4374:2023's heat-resisting alloy NI-PH1301 is primarily utilized in aerospace industries requiring components that endure extreme temperatures and mechanical stresses, such as:

  • Aerospace engine components: Turbine blades, combustion chambers, and exhaust systems where heat resistance and strength at elevated temperatures are vital.

  • Structural elements in aircraft and spacecraft: Bars and sections used in high-temperature zones, contributing to the safety and durability of airframes and propulsion systems.

  • High-temperature mechanical systems: Any aerospace assembly demanding alloys with superior creep resistance, oxidation resistance, and mechanical integrity under cyclic thermal loading.

The standard's precise requirements enable manufacturers and engineers to select and validate NI-PH1301 alloy components for critical aerospace applications, balancing material performance and reliability.


Related Standards

  • EN 4258: Aerospace series general organization of metallic materials standardization, outlining the framework for the series EN 4374 belongs to.

  • EN 4700-002: Technical specification for steel and heat resisting alloys in wrought products, detailing testing and inspection methods applied within EN 4374.

  • EN 2043: General requirements for aerospace semi-finished product qualification, including qualification protocols critical for NI-PH1301 bars and sections.

  • EN 4500-003: Rules for drafting and presentation of aerospace metallic material standards, ensuring consistent and clear documentation for heat-resisting alloys.


By adhering to SIST EN 4374:2023, aerospace manufacturers ensure NI-PH1301 alloy components meet the stringent quality, mechanical, and thermal performance required in modern aerospace engineering. Compliance with this standard supports enhanced safety, durability, and efficiency of aerospace systems exposed to high-temperature operational environments.

Frequently Asked Questions

SIST EN 4374:2023 is a standard published by the Slovenian Institute for Standardization (SIST). Its full title is "Aerospace series - Heat-resisting alloy NI-PH1301 (NiCr19Co18Mo4Ti3Al3) - Solution treated and precipitation treated - Bars and sections - De ≤ 200 mm". This standard covers: This document specifies the requirements relating to: Heat-resisting alloy NI-PH1301 (NiCr19Co18Mo4Ti3Al3) Solution treated and precipitation treated Bars and sections De ≤ 200 mm for aerospace applications.

This document specifies the requirements relating to: Heat-resisting alloy NI-PH1301 (NiCr19Co18Mo4Ti3Al3) Solution treated and precipitation treated Bars and sections De ≤ 200 mm for aerospace applications.

SIST EN 4374:2023 is classified under the following ICS (International Classification for Standards) categories: 49.025.99 - Other materials; 77.140.60 - Steel bars and rods. The ICS classification helps identify the subject area and facilitates finding related standards.

You can purchase SIST EN 4374:2023 directly from iTeh Standards. The document is available in PDF format and is delivered instantly after payment. Add the standard to your cart and complete the secure checkout process. iTeh Standards is an authorized distributor of SIST standards.

Standards Content (Sample)


SLOVENSKI STANDARD
01-marec-2023
Aeronavtika - Toplotno odporna zlitina NI-PH1301 (NiCr19Co18Mo4Ti3Al3) -
Topilno žarjena in izločevalno utrjena - Palice in profili - De ≤ 200 mm
Aerospace series - Heat-resisting alloy NI-PH1301 (NiCr19Co18Mo4Ti3Al3) - Solution
treated and precipitation treated - Bars and sections - De ≤ 200 mm
Luft- und Raumfahrt - Hochwarmfeste Legierung NI-PH1301 (NiCr19Co18Mo4Ti3Al3) -
Lösungsgeglüht und ausscheidungsgehärtet - Stangen und Profile - De ≤ 200 mm
Série aérospatiale - Alliage résistant à chaud NI-PH1301 (NiCr19Co18Mo4Ti3Al3) - Mis
en solution et précipité - Barres et profilés - De ≤ 200 mm
Ta slovenski standard je istoveten z: EN 4374:2022
ICS:
49.025.99 Drugi materiali Other materials
77.140.60 Jeklene palice in drogovi Steel bars and rods
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

EN 4374
EUROPEAN STANDARD
NORME EUROPÉENNE
December 2022
EUROPÄISCHE NORM
ICS 49.025.99
English Version
Aerospace series - Heat-resisting alloy NI-PH1301
(NiCr19Co18Mo4Ti3Al3) - Solution treated and
precipitation treated - Bars and sections - De  200 mm
Série aérospatiale - Alliage résistant à chaud NI- Luft- und Raumfahrt - Hochwarmfeste Legierung NI-
PH1301 (NiCr19Co18Mo4Ti3Al3) - Mis en solution et PH1301 (NiCr19Co18Mo4Ti3Al3) - Lösungsgeglüht
précipité - Barres et profilés - De  200 mm und ausscheidungsgehärtet - Stangen und Profile - De 
200 mm
This European Standard was approved by CEN on 24 July 2022.

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, Türkiye 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
© 2022 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 4374:2022 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 4734:2022) 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
document has received the approval of the National Associations and the Official Services of the
member countries of ASD-STAN, 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 June 2023, and conflicting national standards shall
be withdrawn at the latest by June 2023.
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.
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