EN 3315:2018
(Main)Aerospace series - Titanium alloy TI-P64001 - Solution treated and aged - Forgings - De ≤ 75 mm
Aerospace series - Titanium alloy TI-P64001 - Solution treated and aged - Forgings - De ≤ 75 mm
This document specifies the requirements relating to:
Titanium alloy TI-P64001
Solution treated and aged
Forgings
De ≤ 75 mm
for aerospace applications.
Luft- und Raumfahrt - Titanlegierung TI-P64001 - Lösungsgeglüht und ausgelagert - Schmiedestücke - De ≤ 75 mm
Série aérospatiale - Alliage de titane TI-P64001 - Mis en solution et revenu - Pièces forgées et pièces matricées - De ≤ 75 mm
Aeronavtika - Titanova zlitina TI-P64001 - Topilno žarjena in starana - Izkovki - De ≤ 75 mm
Ta dokument določa zahteve, ki se nanašajo na:
titanovo zlitino TI-P64001,
topilno žarjeno in starano
(izkovki)
De ≤ 75 mm
za uporabo v aeronavtiki.
General Information
- Status
- Published
- Publication Date
- 13-Nov-2018
- Withdrawal Date
- 30-May-2019
- Technical Committee
- ASD-STAN - Aerospace
- Drafting Committee
- ASD-STAN/D 4 - Metallic
- Current Stage
- 6060 - Definitive text made available (DAV) - Publishing
- Start Date
- 14-Nov-2018
- Completion Date
- 14-Nov-2018
Overview
EN 3315:2018 is a European aerospace material standard that defines requirements for titanium alloy TI‑P64001 supplied as solution‑treated and aged forgings with an external diameter (De) of ≤ 75 mm. Prepared under the ASD‑STAN/CEN process, the standard is part of the EN aerospace metallic materials series and is intended for use in aerospace component manufacture where controlled chemistry, heat treatment and mechanical performance are required.
Key Topics
- Material and condition: Specifies the titanium alloy designation TI‑P64001 in the solution‑treated and aged condition for forgings.
- Form and size: Applies to forgings produced from forging stock, with maximum external diameter (De) ≤ 75 mm.
- Chemical composition: Limits for alloying elements are defined (for example, aluminium and vanadium ranges are given) along with controls for interstitials and impurities.
- Heat treatment: Prescribes the delivery condition as solution treated and aged; an alternative solution temperature option (beta‑transus minus 30 °C) is noted.
- Mechanical requirements and tests: Includes requirements for tensile properties (proof stress Rp0.2, ultimate tensile strength Rm, elongation A, reduction of area Z), hardness and routine inspections. Test piece direction, dimensional and marking inspections refer to EN 2858‑3.
- Quality and acceptance: External defect inspection, marking and dimensional checks follow EN 2858‑3. Product qualification programs and additional specifications are to be agreed between manufacturer and purchaser.
- Normative references: Key linked standards include EN 2858‑3 (forging technical specification), EN 3313 (forging stock), EN 4258 and EN 4500‑004.
Applications
- Aerospace structural and engine components where high strength‑to‑weight and specific heat‑treated titanium properties are required.
- Suitable for machined forged parts, fittings, fastener blanks, small-diameter shafts and other critical aerospace forgings within the size limit.
- Used by: material suppliers, forging manufacturers, aerospace OEMs, design and materials engineers, procurement and quality assurance teams, and certification bodies involved in aerospace part approval.
Practical value
- Ensures consistent chemical and mechanical performance of TI‑P64001 forgings in the solution‑treated and aged condition.
- Simplifies procurement and acceptance by referencing established test methods and inspection criteria.
- Helps designers and manufacturers select appropriate material and heat‑treatment controls for critical aerospace forgings.
Related Standards
- EN 2858‑3 - Aerospace series: Titanium and titanium alloys - Forging stock and forgings - Part 3: Pre‑production and production forgings (technical specification)
- EN 3313 - TI‑P64001 forging stock for solution treated and aged forgings
- EN 4258, EN 4500‑004 - Organization and drafting rules for aerospace metallic material standards
Keywords: EN 3315:2018, TI‑P64001, titanium alloy, solution treated and aged, aerospace forgings, EN standards, mechanical properties, heat treatment.
Frequently Asked Questions
EN 3315:2018 is a standard published by the European Committee for Standardization (CEN). Its full title is "Aerospace series - Titanium alloy TI-P64001 - Solution treated and aged - Forgings - De ≤ 75 mm". This standard covers: This document specifies the requirements relating to: Titanium alloy TI-P64001 Solution treated and aged Forgings De ≤ 75 mm for aerospace applications.
This document specifies the requirements relating to: Titanium alloy TI-P64001 Solution treated and aged Forgings De ≤ 75 mm for aerospace applications.
EN 3315:2018 is classified under the following ICS (International Classification for Standards) categories: 49.025.30 - Titanium. The ICS classification helps identify the subject area and facilitates finding related standards.
EN 3315:2018 is available in PDF format for immediate download after purchase. The document can be added to your cart and obtained through the secure checkout process. Digital delivery ensures instant access to the complete standard document.
Standards Content (Sample)
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.49.025.30TitanTitaniumICS:Ta slovenski standard je istoveten z:EN 3315:2018SIST EN 3315:2019en,fr,de01-januar-2019SIST EN 3315:2019SLOVENSKI
STANDARD
EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 3315
November
t r s z ICS
v {ä r t wä u r English Version
Aerospace series æ Titanium alloy TIæP x v r r s æ Solution treated and aged æ Forgings æ De ≤
y w mm Série aérospatiale æ Alliage de titane TIæP x v r r s æ Mis en solution et revenu æ Pièces forgées et pièces matricées æ De ≤
y w mm
Luftæ und Raumfahrt æ Titanlegierung TIæP x v r r s æ Lösungsgeglüht und ausgelagert æ Schmiedestücke æ De ≤
y w mm This European Standard was approved by CEN on
z July
t r s zä
egulations which stipulate the conditions for giving this European Standard the status of a national standard without any alterationä Upætoædate lists and bibliographical references concerning such national standards may be obtained on application to the CENæCENELEC Management Centre or to any CEN memberä
translation under the responsibility of a CEN member into its own language and notified to the CENæCENELEC Management Centre has the same status as the official versionsä
CEN members are the national standards bodies of Austriaá Belgiumá Bulgariaá Croatiaá Cyprusá Czech Republicá Denmarká Estoniaá Finlandá Former Yugoslav Republic of Macedoniaá Franceá Germanyá Greeceá Hungaryá Icelandá Irelandá Italyá Latviaá Lithuaniaá Luxembourgá Maltaá Netherlandsá Norwayá Polandá Portugalá Romaniaá Serbiaá Slovakiaá Sloveniaá Spainá Swedená Switzerlandá Turkey and United Kingdomä
EUROPEAN COMMITTEE FOR STANDARDIZATION COMITÉ EUROPÉEN DE NORMALISATION EUROPÄISCHES KOMITEE FÜR NORMUNG
CEN-CENELEC Management Centre:
Rue de la Science 23,
B-1040 Brussels
t r s z CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Membersä Refä Noä EN
u u s wã t r s z ESIST EN 3315:2019
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