Aerospace series - Heat resisting nickel base alloy (Ni-P101HT) - Cold worked and softened - Bar and wire for continuous forging or extrusion for fasteners - 3 mm ≤ D ≤ 30 mm

This document specifies the requirements relating to:
Heat resisting nickel base alloy (Ni-P101HT)
Cold worked and softened
Bar and wire for continuous forging or extrusion for fasteners
3 mm ≤ D ≤ 30 mm
for aerospace applications.

Luft- und Raumfahrt - Hochwarmfeste Nickellegierung (Ni-P101HT) - Kaltverfestigt und abgeschreckt - Stangen und Drähte zum kontinuierlichen Verformen oder Strangpressen für Verbindungselemente - 3 mm ≤ D ≤ 30 mm

Aerospace series - Heat resisting nickel base alloy (Ni-P101HT) - Cold worked and softened - Bar and wire for continuous forging or extrusion for fasteners - 3 mm ≤ D ≤ 30 mm

Aeronavtika - Toplotno odporne zlitine na nikljevi osnovi (Ni-P101HT) - Hladno preoblikovana in mehko žarjena - Palice in žice za kontinuirno kovanje ali iztiskanje vezalnih elementov - 3 mm ≤ D ≤ 30 mm

Ta dokument določa zahteve, ki se nanašajo na:
toplotno odporne zlitine na nikljevi osnovi (Ni-P101HT),
hladno preoblikovane in mehko žarjene,
palice in žice za kontinuirno kovanje ali iztiskanje vezalnih elementov,
3 mm ≤ D ≤ 30 mm,
za uporabo v aeronavtiki.

General Information

Status
Published
Publication Date
14-Apr-2019
Technical Committee
Current Stage
6060 - National Implementation/Publication (Adopted Project)
Start Date
11-Apr-2019
Due Date
16-Jun-2019
Completion Date
15-Apr-2019

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2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.PPPP49.030.01Vezni elementi na splošnoFasteners in general49.025.05Železove zlitine na splošnoFerrous alloys in generalICS:Ta slovenski standard je istoveten z:EN 3220:2019SIST EN 3220:2019en,fr,de01-junij-2019SIST EN 3220:2019SLOVENSKI

STANDARD
SIST EN 3220:2019
EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 3220
April
t r s { ICS
v {ä r t wä { { English Version
tened æ Bar and wire for continuous forging or extrusion for fasteners æ

u mm ≤ D ≤ u r mm Série aérospatiale æ Alliage résistant à chaud base le forgeage ou l 5extrusion en continu pour fixations æ

u mm ≤ D ≤
u r mm

Luftæ und Raumfahrt æ Hochwarmfeste Nickellegierung Stangen und Drähte zum kontinuierlichen Verformen oder Strangpressen für Verbindungselemente æ

u mm ≤D ≤
u r mm This European Standard was approved by CEN on
t December
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 { CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Membersä Refä Noä EN

u t t rã t r s { ESIST EN 3220:2019

EN 3220:2019 (E) 2 Contents Page European foreword .................................................................................................................................................... 3 Introduction .................................................................................................................................................................. 4 1 Scope .................................................................................................................................................................. 5 2 Normative references .................................................................................................................................. 5 3 Terms and definitions ................................................................................................................................. 5 4 Requirements ................................................................................................................................................. 5

SIST EN 3220:2019

EN 3220:2019 (E) 3 European foreword This document (EN 3220:2019) 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 October 2019, and conflicting national standards shall be withdrawn at the latest by October2019. 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 national standards organizations of the following countries are bound to implement this European Standard: 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 the United Kingdom. SIST EN 3220:2019

EN 3220:2019 (E) 4 Introduction This document is part of the series of EN metallic material standards for aerospace applications. The general organization of this seri

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