EN 2941:2008
(Main)Aerospace series - Nickel alloy rivets - Technical specification
Aerospace series - Nickel alloy rivets - Technical specification
This standard specifies the performance and test requirements for solid rivets in the nickel alloys quoted below, intended for aerospace applications. It applies wherever it is specified in the document defining the rivet.
Its use, after agreement between the customer and the supplier, for solid rivets made from other materials, requires determination, case by case, of the minimum tensile and double shear loads.
Luft- und Raumfahrt - Niete aus Nickellegierung - Technische Lieferbedingungen
Série aérospatiale - Rivets en alliage de nickel - Spécification technique
Aeronavtika - Kovice iz nikljeve zlitine - Tehnična specifikacija
General Information
Standards Content (Sample)
SLOVENSKI STANDARD
01-junij-2008
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Aerospace series - Nickel alloy rivets - Technical specification
Luft- und Raumfahrt - Niete aus Nickellegierung - Technische Lieferbedingungen
Série aérospatiale - Rivets en alliage de nickel - Spécification technique
Ta slovenski standard je istoveten z: EN 2941:2008
ICS:
49.030.60
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.
EUROPEAN STANDARD
EN 2941
NORME EUROPÉENNE
EUROPÄISCHE NORM
March 2008
ICS 49.030.60
English Version
Aerospace series - Nickel alloy rivets - Technical specification
Série aérospatiale - Rivets en alliage de nickel - Luft- und Raumfahrt - Niete aus Nickellegierung -
Spécification technique Technische Lieferbedingungen
This European Standard was approved by CEN on 12 December 2007.
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 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 Management Centre has the same status as the
official versions.
CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Cyprus, Czech Republic, Denmark, Estonia, Finland,
France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal,
Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom.
EUROPEAN COMMITTEE FOR STANDARDIZATION
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© 2008 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 2941:2008: E
worldwide for CEN national Members.
Contents Page
Foreword.3
1 Scope.4
2 Normative references.4
3 Terms and definitions .4
4 Required characteristics.5
5 Filing of documents.10
6 Certificate of conformity .10
Foreword
This document (EN 2941:2008) 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 September 2008, and conflicting national standards shall be
withdrawn at the latest by September 2008.
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.
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, Cyprus, Czech
Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia,
Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain,
Sweden, Switzerland and the United Kingdom.
1 Scope
This standard specifies the performance and test requirements for solid rivets in the nickel alloys quoted below,
intended for aerospace applications. It applies wherever it is specified in the document defining the rivet.
Its use, after agreement between the customer and the supplier, for solid rivets made from other materials,
requires determination, case by case, of the minimum tensile and double shear loads.
2 Normative references
The following referenced documents are indispensable for the application of this document. For dated
references, only the edition cited applies. For undated references, the latest edition of the referenced
document (including any amendments) applies.
ISO 2859-1, Sampling procedures for inspection by attributes — Part 1: Sampling schemes indexed by
acceptance quality limit (AQL) for lot-by-lot inspection.
EN 2002-001, Aerospace series — Metallic materials — Test methods — Part 001: Tensile testing at ambient
temperature.
1)
EN 2002-7, Aerospace series — Metallic materials — Test methods — Part 7: Hardness test.
2)
EN 2305 , Nickel base alloy NI-P11 — 540 MPa ≤ R ≤ 620 MPa — Bars and wires for rivets — Aerospace
m
3)
series.
4)
EN 3238, Aerospace series — Metallic materials — Test method — Shear test for wires and rivets.
EN 4371, Aerospace series — Heat resisting alloy NI-PD9001 (NiCu31) — Non heat treated — Bar for
1)
rivets — D ≤ 10 mm.
EN 4372, Aerospace series — Heat resisting nickel alloy with copper NI-PD9001 (NiCu31) — Wire for solid
1)
rivets — D ≤ 10 mm.
3 Terms and definitions
For the purposes of this document, the following terms and definitions apply.
3.1
batch
for all tests, inspections and supplies, a batch of rivets is defined as follows: finished rivets of the same form,
diameter and length, manufactured by the same process, made from one material, batch from the same heat
treatment furnace with the same surface treatment, and deriving from the same wire coil and the same place
of manufacture
The maximum mass of each batch is limited to 25 kg.
1) Published as ASD Prestandard at the date of publication of this standard.
2) Inactive for new designation, see EN 4371 and EN 4372.
3) Published as ASD Standard at the date of publication of this standard.
4) In preparation at the date of publication of this standard.
3.2
rivet wire samples
for the test, each rivet batch shall be accompanied by rivet wire samples taken from each end of the coil used
to manufacture the batch. The samples shall be submitted to the same heat treatment as the rivets of that batch
3.3
rivet samples
...
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