EN 3672:2016
(Main)Aerospace series - Shank nuts, self-locking, in heat resisting nickel base alloy NI-P101HT (Waspaloy), silver plated, for 30° swage - Classification: 1 210 MPa (at ambient temperature) / 730 °C
Aerospace series - Shank nuts, self-locking, in heat resisting nickel base alloy NI-P101HT (Waspaloy), silver plated, for 30° swage - Classification: 1 210 MPa (at ambient temperature) / 730 °C
This European Standard specifies the characteristics of self-locking shank nuts in NI-P101HT, silver plated, for use in 30° cone holes, for aerospace applications.
Classification: 1 210 MPa /730 °C).
Luft- und Raumfahrt - Einnietmuttern, selbstsichernd, aus hochwarmfester Nickelbasislegierung NI-P101HT (Waspaloy), versilbert, für 30° Aufweitung - Klasse: 1 210 MPa (bei Raumtemperatur) / 730 °C
Série aérospatiale - Écrous à sertir, à freinage interne, en alliage résistant à chaud à base de nickel NI-P101HT (Waspaloy), argentés, pour sertissage 30° - Classification: 1 210 MPa (à température ambiante) / 730 °C
Aeronavtika - Zakovičene matice, samovarovalne, iz toplotnoodporne zlitine na nikljevi osnovi NI-P101HT (Waspaloy), posrebrene, za odprtine 30° - Klasifikacija: 1210 MPa (pri sobni temperaturi)/730 °C
Ta evropski standard določa lastnosti samovarovalnih zakovičenih matic po NI-P101HT,
posrebrenih, za uporabo v odprtinah 30° v aeronavtiki.
Klasifikacija: 1210 MPa 1)/730 °C 2).
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Standards Content (Sample)
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Luft- und Raumfahrt - Einnietmuttern, selbstsichernd, aus hochwarmfester Nickelbasislegierung NI-P101HT (Waspaloy), versilbert, für 30°C Aufweitung - Klasse: 1 210 MPa (bei Raumtemperatur) / 730°CSérie aérospatiale - Écrous à sertir, à freinage interne, en alliage résistant à chaud à base de nickel NI-P101HT (Waspaloy), argentés, pour sertissage 30°C - Classification: 1 210 MPa (à température ambiante) / 730°CAerospace series - Shank nuts, self-locking, in heat resisting nickel base alloy NI-P101HT (Waspaloy), silver plated, for 30°C swage - Classification: 1 210 MPa (at ambient temperature) / 730°C49.030.30MaticeNutsICS:Ta slovenski standard je istoveten z:EN 3672:2016SIST EN 3672:2017en,fr,de01-marec-2017SIST EN 3672:2017SLOVENSKI
STANDARDSIST EN 3672:20081DGRPHãþD
SIST EN 3672:2017
EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 3672
December
t r s x ICS
v {ä r u rä u r Supersedes EN
u x y tã t r r zEnglish Version
Aerospace series æ Shank nutsá selfælockingá in heat resisting nickel base alloy platedá for
u r ¹C swage æ ClSérie aérospatiale æ Écrous à sertirá à freinage interneá en alliage résistant à chaud à base de nickel NIæP s r sHT
y u r ¹C
Luftæ und Raumfahrt æ Einnietmutterná selbstsicherndá aus hochwarmfester Nickelbasislegierung NIæP s r sHT This European Standard was approved by CEN on
v March
t r s xä
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 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:
Avenue Marnix 17,
B-1000 Brussels
9
t r s x CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Membersä Refä Noä EN
u x y tã t r s x ESIST EN 3672:2017
EN 3672:2016 (E) 2 Contents
Page European foreword . 3 1 Scope . 4 2 Normative references . 4 3 Required characteristics . 4 4 Designation . 6 5 Marking . 6 6 Technical specification . 6 Annex A (informative)
Standard evolution form . 7
SIST EN 3672:2017
EN 3672:2016 (E) 3 European foreword This document (EN 3672:2016) 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 June 2017, and conflicting national standards shall be withdrawn at the latest by June 2017. Attention is drawn to the possibility that some of the elements of this document may be the subject of patent rights. CEN [and/or CENELEC] shall not be held responsible for identifying any or all such patent rights. This document supersedes EN 3672:2008. According to the CEN-CENELEC Internal Regulations, t
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