prEN 3542
(Main)Aerospace series - Inserts, screw threads, helical coil, self-locking, tanged insertion drive, in heat resisting nickel base alloy NI-PH2801 (Inconel X750)
Aerospace series - Inserts, screw threads, helical coil, self-locking, tanged insertion drive, in heat resisting nickel base alloy NI-PH2801 (Inconel X750)
This document specifies the characteristics of inserts, self-locking, helical coil, tanged insertion drive, with MJ screw threads in NI-PH2801 material, for aerospace applications.
Maximum test temperature: 550 °C.
Luft- und Raumfahrt - Draht-Gewindeeinsätze, MJ-Gewinde, spriralförmig gewunden, selbstsichernd, Einsteckantrieb mit Zapfen, aus hochwarmfester Nickelbasislegierung NI-PH2801 (Inconel X750)
Série aérospatiale - Inserts, filets de vis MJ, bobine hélicoïdale, autobloquants, entraînement par insertion à brides, en alliage à base de nickel résistant à la chaleur NI-PH2801 (Inconel X750)
Aeronavtika - Vložki s spiralnim navojem, samozapiralni, za ročno vstavljanje, iz toplotno odporne zlitine na nikljevi osnovi Ni-PH2801 (Inconel X750)
General Information
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Standards Content (Sample)
SLOVENSKI STANDARD
01-februar-2022
Aeronavtika - Vložki s spiralnim navojem, samozapiralni, vgrajeni pogon s tangenti
(tanged insertion drive ), iz toplotnoodporne zlitine na nikljevi osnovi Ni-PH2801
(Inconel X750)
Aerospace series - Inserts, screw threads, helical coil, self-locking, tanged insertion
drive, in heat resisting nickel base alloy NI-PH2801 (Inconel X750)
Luft- und Raumfahrt - Draht-Gewindeeinsätze, MJ-Gewinde, spriralförmig gewunden,
selbstsichernd, Einsteckantrieb mit Zapfen, aus hochwarmfester Nickelbasislegierung
NI-PH2801 (Inconel X750)
Série aérospatiale - Inserts, filets de vis MJ, bobine hélicoïdale, autobloquants,
entraînement par insertion à brides, en alliage à base de nickel résistant à la chaleur NI-
PH2801 (Inconel X750)
Ta slovenski standard je istoveten z: prEN 3542
ICS:
49.030.30 Matice Nuts
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.
DRAFT
EUROPEAN STANDARD
NORME EUROPÉENNE
EUROPÄISCHE NORM
December 2021
ICS 49.030.30 Will supersede EN 3542:2018
English Version
Aerospace series - Inserts, screw threads, helical coil, self-
locking, tanged insertion drive, in heat resisting nickel
base alloy NI-PH2801 (Inconel X750)
Série aérospatiale - Inserts, filets de vis MJ, bobine Luft- und Raumfahrt - Draht-Gewindeeinsätze, MJ-
hélicoïdale, autobloquants, entraînement par insertion Gewinde, spriralförmig gewunden, selbstsichernd,
à brides, en alliage à base de nickel résistant à la Einsteckantrieb mit Zapfen, aus hochwarmfester
chaleur NI-PH2801 (Inconel X750) Nickelbasislegierung NI-PH2801 (Inconel X750)
This draft European Standard is submitted to CEN members for enquiry. It has been drawn up by the Technical Committee ASD-
STAN.
If this draft becomes a European Standard, 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.
This draft European Standard was established by CEN 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, Turkey and
United Kingdom.
Recipients of this draft are invited to submit, with their comments, notification of any relevant patent rights of which they are
aware and to provide supporting documentation.
Warning : This document is not a European Standard. It is distributed for review and comments. It is subject to change without
notice and shall not be referred to as a European Standard.
EUROPEAN COMMITTEE FOR STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION
EUROPÄISCHES KOMITEE FÜR NORMUNG
CEN-CENELEC Management Centre: Rue de la Science 23, B-1040 Brussels
© 2021 CEN All rights of exploitation in any form and by any means reserved Ref. No. prEN 3542:2021 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 Required characteristics . 5
4.1 Configuration — Dimensions — Tolerances — Masses . 5
4.2 Material . 7
4.3 Material identification . 7
5 Designation . 9
6 Marking . 9
7 Technical specification . 9
8 Quality management systems . 9
Bibliography . 10
European foreword
This document (prEN 3542:2021) 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 Nation
...
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