Aerospace series - Heat resisting alloy NI-PH1302 (NiCr20Co13Mo4Ti3Al) - Solution treated and cold worked - Bar for forged fasteners - 3 mm ≤ D ≤ 30 mm

This document specifies the requirements relating to:
Heat resisting alloy NI-PH1302 (NiCr20Co13Mo4Ti3Al)
Solution treated and cold worked
Bar for forged fasteners
3 mm  ≤ D  ≤ 30 mm
for aerospace applications.

Luft- und Raumfahrt - Hochwarmfeste Legierung - NI-PH1302 (NiCr20Co13Mo4Ti3Al) - Lösungsgeglüht und kaltverfestigt - Stangen zum Warmstauchschmieden für Verbindungselemente - 3 mm ≤ D ≤ 30 mm

Dieses Dokument legt die Anforderungen an:
Hochwarmfeste Legierung NI PH1302 (NiCr20Co13Mo4Ti3Al)
Lösungsgeglüht und kaltverfestigt
Stangen zum Warmstauchschmieden für Verbindungselemente
3 mm ≤ D ≤ 30 mm
für Anwendungen in der Luft- und Raumfahrt fest.

Série aérospatiale - Alliage résistant à chaud - NI-PH1302 (NiCr20Co13Mo4Ti3Al) - Mis en solution et écroui - Barres pour éléments de fixations forgés - 3 mm ≤ D ≤ 30 mm

Aeronavtika - Toplotno odporna zlitina NI-PH1302 (NiCr20Co13Mo4Ti3Al) - Topilno žarjena in hladno preoblikovana - Palice za kovane vezne elemente - 3 mm ≤ D ≤ 30 mm

Ta dokument določa zahteve, ki se nanašajo na:
toplotno odporne zlitine NI-PH1302 (NiCr20Co13Mo4Ti3Al),
topilno žarjene in hladno preoblikovane,
palice za kovane vezne elemente,
3 mm ≤ D ≤ 30 mm,
za uporabo v aeronavtiki.

General Information

Status
Published
Publication Date
18-Jun-2019
Technical Committee
I13 - Imaginarni 13
Current Stage
6060 - National Implementation/Publication (Adopted Project)
Start Date
13-Jun-2019
Due Date
18-Aug-2019
Completion Date
19-Jun-2019

Overview

SIST EN 2959:2019 is a European standard published by CEN that specifies the technical requirements for the aerospace heat resisting alloy NI-PH1302 (NiCr20Co13Mo4Ti3Al). This standard covers solution treated and cold worked bars designed specifically for forged fasteners with diameters ranging from 3 mm to 30 mm. Tailored for aerospace industry applications, the document ensures material consistency, performance, and safety in demanding environments where heat resistance and mechanical strength are critical.

Key Topics

  • Material Specification: The alloy NI-PH1302 is defined by its chemical composition, including key elements such as Nickel (Ni), Chromium (Cr), Cobalt (Co), Molybdenum (Mo), Titanium (Ti), and Aluminum (Al). Precise concentration limits are defined to optimize heat resistance and mechanical properties.
  • Heat Treatment: The bars undergo solution treatment between 1010 °C to 1080 °C, followed by cold working (10% to 30%) at temperatures below 870 °C. These processes enhance strength and durability.
  • Physical Dimensions: The standard applies strictly to bars with diameters between 3 mm and 30 mm, ensuring suitability for forging processes related to aerospace fasteners.
  • Mechanical Properties: Minimum proof stress, tensile strength, elongation, reduction of area, and hardness values are specified to guarantee performance under operational stresses and temperatures.
  • Manufacturing Requirements: The bars must be vacuum melted and consumable electrode remelted to ensure purity and quality.
  • Quality Control: Requirements for grain size, dimensional tolerances, external defect inspection, and marking ensure compliance with aerospace safety standards.

Applications

SIST EN 2959:2019 is critical for manufacturers and engineers involved in producing aerospace forged fasteners such as bolts, nuts, and other fastening elements used in aircraft and aerospace vehicles. The material's heat resistance and mechanical reliability make it suitable for components exposed to high temperatures and mechanical stresses, including:

  • Jet engine components
  • Airframe fasteners exposed to elevated temperatures
  • Turbine fasteners requiring high strength and corrosion resistance
  • Structural aerospace assemblies needing durable, heat-resistant fixation elements

By adhering to this standard, aerospace manufacturers can ensure fasteners meet rigorous safety and performance criteria required in the aerospace sector, improving reliability and lifecycle performance.

Related Standards

This standard is part of the comprehensive series of EN metallic material specifications tailored for aerospace applications and references related standards to ensure holistic quality management:

  • EN 2043 – Aerospace series: General requirements for semi-finished product qualification (excluding forgings and castings).
  • EN 4258 – General organization of aerospace material standardization and classification framework.
  • EN 4500-003 – Specific rules for drafting and presentation of material standards for heat resisting alloys.
  • EN 4700-002 – Technical specifications for wrought steel and heat resisting alloy bars and sections, detailing testing and inspection procedures.

Compliance with SIST EN 2959:2019 along with these associated standards ensures robust quality systems and harmonization across aerospace material supply chains.


Keywords: SIST EN 2959:2019, aerospace heat resisting alloy, NI-PH1302, forged fasteners, solution treated, cold worked bars, aerospace materials standard, heat resistant alloy bar, NiCr20Co13Mo4Ti3Al, aerospace fastener alloy specification, CEN aerospace standards.

Frequently Asked Questions

SIST EN 2959:2019 is a standard published by the Slovenian Institute for Standardization (SIST). Its full title is "Aerospace series - Heat resisting alloy NI-PH1302 (NiCr20Co13Mo4Ti3Al) - Solution treated and cold worked - Bar for forged fasteners - 3 mm ≤ D ≤ 30 mm". This standard covers: This document specifies the requirements relating to: Heat resisting alloy NI-PH1302 (NiCr20Co13Mo4Ti3Al) Solution treated and cold worked Bar for forged fasteners 3 mm ≤ D ≤ 30 mm for aerospace applications.

This document specifies the requirements relating to: Heat resisting alloy NI-PH1302 (NiCr20Co13Mo4Ti3Al) Solution treated and cold worked Bar for forged fasteners 3 mm ≤ D ≤ 30 mm for aerospace applications.

SIST EN 2959:2019 is classified under the following ICS (International Classification for Standards) categories: 49.025.15 - Non-ferrous alloys in general. The ICS classification helps identify the subject area and facilitates finding related standards.

You can purchase SIST EN 2959:2019 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-september-2019
Aeronavtika - Toplotno odporna zlitina NI-PH1302 (NiCr20Co13Mo4Ti3Al) - Topilno
žarjena in hladno preoblikovana - Palice za kovane vezne elemente - 3 mm ≤ D ≤ 30
mm
Aerospace series - Heat resisting alloy NI-PH1302 (NiCr20Co13Mo4Ti3Al) - Solution
treated and cold worked - Bar for forged fasteners - 3 mm ≤ D ≤ 30 mm
Luft- und Raumfahrt - Hochwarmfeste Legierung - NI-PH1302 (NiCr20Co13Mo4Ti3Al) -
Lösungsgeglüht und kaltverfestigt - Stangen zum Warmstauchschmieden für
Verbindungselemente - 3 mm ≤ D ≤ 30 mm
Série aérospatiale - Alliage résistant à chaud - NI-PH1302 (NiCr20Co13Mo4Ti3Al) - Mis
en solution et écroui - Barres pour éléments de fixations forgés - 3 mm ≤ D ≤ 30 mm
Ta slovenski standard je istoveten z: EN 2959:2019
ICS:
49.025.15 Neželezove zlitine na Non-ferrous alloys in general
splošno
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

EN 2959
EUROPEAN STANDARD
NORME EUROPÉENNE
June 2019
EUROPÄISCHE NORM
ICS 49.025.15; 49.025.99
English Version
Aerospace series - Heat resisting alloy NI-PH1302
(NiCr20Co13Mo4Ti3Al) - Solution treated and cold
worked - Bar for forged fasteners - 3 mm ≤ D ≤ 30 mm
Série aérospatiale - Alliage résistant à chaud - NI- Luft- und Raumfahrt - Hochwarmfeste Legierung - NI-
PH1302 (NiCr20Co13Mo4Ti3Al) - Mis en solution et PH1302 (NiCr20Co13Mo4Ti3Al) - Lösungsgeglüht und
écroui - Barres pour éléments de fixations forgés - 3 kaltverfestigt - Stangen zum Warmstauchschmieden
mm ≤ D ≤ 30 mm für Verbindungselemente - 3 mm ≤ D ≤ 30 mm
This European Standard was approved by CEN on 6 January 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, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania,
Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, 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 2959:2019 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

European foreword
This document (EN 2959:2019) 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 December 2019, and conflicting national standards shall be withdrawn
at the latest by December 2019.
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.
Acc
...

Questions, Comments and Discussion

Ask us and Technical Secretary will try to provide an answer. You can facilitate discussion about the standard in here.

Loading comments...