oSIST prEN 2002-001:2024
(Main)Aerospace series - Metallic materials - Test methods - Part 1: Tensile testing at ambient temperature
Aerospace series - Metallic materials - Test methods - Part 1: Tensile testing at ambient temperature
This document specifies the requirements for the tensile testing of metallic materials at ambient temperature for aerospace applications.
It is applied when referred to in the EN technical specification or material standard unless otherwise specified on the drawing, order or inspection schedule.
Luft- und Raumfahrt - Metallische Werkstoffe - Prüfverfahren - Teil 001: Zugversuch bei Raumtemperatur
Diese Norm legt die Anforderungen für den Zugversuch bei Raumtemperatur von metallischen Werkstoffen für An¬wendungen in der Luft- und Raumfahrt fest.
Diese Norm ist anzuwenden, wenn in den technischen Lieferbedingungen einer EN-Norm oder in einer EN Werkstoffnorm darauf verwiesen wird, sofern nicht anders auf der Zeichnung, Auftrags- oder Prüfliste fest¬gelegt.
Série aérospatiale - Matériaux métalliques - Méthodes d'essais applicables - Partie 1 : Essais de traction à température ambiante
No Scope available
Aeronavtika - Kovinski materiali - Preskusne metode - 1. del: Natezni preskus pri temperaturi okolice
General Information
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Standards Content (Sample)
SLOVENSKI STANDARD
01-november-2024
Aeronavtika - Kovinski materiali - Preskusne metode - 1. del: Natezni preskus pri
temperaturi okolice
Aerospace series - Metallic materials - Test methods - Part 1: Tensile testing at ambient
temperature
Luft- und Raumfahrt - Metallische Werkstoffe - Prüfverfahren - Teil 001: Zugversuch bei
Raumtemperatur
Série aérospatiale - Matériaux métalliques - Méthodes d'essais applicables - Partie 1 :
Essais de traction à température ambiante
Ta slovenski standard je istoveten z: prEN 2002-001
ICS:
49.025.05 Železove zlitine na splošno Ferrous alloys in general
49.025.15 Neželezove zlitine na Non-ferrous alloys in general
splošno
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.
DRAFT
EUROPEAN STANDARD
NORME EUROPÉENNE
EUROPÄISCHE NORM
September 2024
ICS 49.025.05; 49.025.15 Will supersede EN 2002-001:2005
English Version
Aerospace series - Metallic materials - Test methods - Part
1: Tensile testing at ambient temperature
Série aérospatiale - Matériaux métalliques - Méthodes Luft- und Raumfahrt - Metallische Werkstoffe -
d'essais applicables - Partie 1 : Essais de traction à Prüfverfahren - Teil 001: Zugversuch bei
température ambiante Raumtemperatur
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, Türkiye 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
© 2024 CEN All rights of exploitation in any form and by any means reserved Ref. No. prEN 2002-001:2024 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 Health and safety . 10
5 Principle of tensile testing . 10
6 Testing requirements . 10
6.1 Resources . 10
6.1.1 Equipment/plant . 10
6.1.2 Materials/reagents . 11
6.1.3 Qualification of personnel . 11
6.2 Test samples/test pieces . 11
6.2.1 Shape and dimensions . 11
6.2.2 Product types . 12
6.2.3 Preparation of test pieces . 12
6.3 Testing procedure . 12
6.3.1 Determination of the cross-sectional area . 12
6.3.2 Marking the original gauge length (L ) . 13
6.3.3 Method of gripping . 13
6.3.4 Extensometer . 13
6.3.5 Temperature of test . 13
6.3.6 Speed of testing . 13
6.3.7 Young’s modulus of elasticity (E), selection of test method . 15
6.4 Determination and expression of test results . 16
6.4.1 Determination of Young’s modulus of elasticity (E) . 16
6.4.2 Determination of proof stress (R ) . 16
p
6.4.3 Determination of tensile strength (R ) . 17
m
6.4.4 Determination of percentage elongation after fracture (A or A ) . 17
L
6.4.5 Determination of percentage reduction of area after fracture (Z) . 17
7 Test report . 18
Annex A (normative) Test pieces to be used for sheets and strips with thickness less than
or equal to 8 mm . 20
Annex B (normative) Non-machined test pieces to be used for bars, sections and wires with
a diameter or thickness less than or equal to 8 mm . 22
Annex C (normative) Machined test pieces to be used for bars, sections, plates and wires
with diameter or thickness greater than 8 mm and for forgings and castings . 23
Annex D (normative) Test pieces to be used for tubes . 26
Bibliography . 28
European foreword
This document (prEN 2002-001:2024) has been prepared by ASD-STAN.
After enquiries and votes carried out in accordance with the rules of this Association, this document has
received the approval of the National Associations and the Official Services of the member countries of
ASD-STAN, prior to its presentation to CEN.
This document is currently submitted to the CEN Enquiry.
This document will supersede prEN 2002-001:2019.
The main changes with respect to the previous edition are as follows:
— prEN 2002-001 (P5), 03/2019:
o overall editorial improvements;
o subclause 6.3.6.2:
• 0,003 to 0,007 (0,3 % to 0,7 %) per min., a strain rate of 0,005 (0,5 %) per min is preferred;
• changed to: “The test shall be performed at a strain rate as required in Table 2 and
Table 3”.
The strain-rate, mentioned in 6.3.6.2, of 0,003/min to 0,007/min is too low. ASTM B557 and
EN 485-2 work with a rate of stress application of maximum 12 MPa/s. For aluminium with an
E-Modulus of about 72 000 MPa this results to a strain-rate of 0,01/min. All testing machines
work with a stressing rate in this range of 12 MPa/s. So consequently, beginning with leaving
the Hooke's line (linear relationship between stress and strain) up to achieving the yield
strength R significant higher strainrates of 0,04/min to 0,05/min at simultaneously
p0,2
significant decreasing stressing rates are determined;
o subclause 6.3.6.3: if the test is to be continued to fracture, the strain rate of the parallel length
may be increased beyond the proof stress but shall not exceed a value of 0,1 (10 %) per min.
Changed to: “If the test is to be continued to fracture, the strain rate of the parallel length may
be increased beyond the proof stress but shall not exceed a value required in Table 2 and
Table 3”.
The strain-rate, mentioned in 6.3.6.3, of 0,1 (10 %)/min is significantly too low. All other
relevant specifications (ASTM B557, EN 485-2 and EN 10002-1:2001) allow a strain rate up to
0,5 (50 %)/min. That means conversely, one tensile test would take five times longer by
application of EN 2002-001. The throughput of one test-machine would decrease to 1/5;
o subclauses 6.3.6.2 and 6.3.6.3: Table 2 with required test speeds implemented for the following
both groups: aluminium and aluminium alloys; engineering steels and stainless steels; all other
metallic materials.
Introduction
This document is part of the series of EN metallic material standards for aerospace applications.
The general organization of this series is described in EN 4258.
1 Scope
This document specifies the requirements for the tensile testing of metallic materials at ambient
temperature for aerospace applications.
It is applied when referred to in the EN technical specification or material standard unless otherwise
specified on the drawing, order or inspection schedule.
2 Normative references
The following documents are referred to in the text in such a way that some or all of their content
constitutes requirements 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.
EN 4259, Aerospace series — Metallic materials — Definition of general terms
EN ISO 7500-1, Metallic materials — Calibration and verification of static uniaxial testing machines —
Part 1: Tension/compression testing machines — Calibration and verification of the force-measuring
system (ISO 7500-1)
EN ISO 9513, Metallic materials — Calibration of extensometer systems used in uniaxial testing
(ISO 9513)
3 Terms and definitions
For the purposes of this document, the terms and definitions given in EN 4259 and the following apply.
ISO and IEC maintain terminology databases for use in standardization at the following addresses:
— ISO Online browsing platform: available at https://www.iso.org/obp/
— IEC Electropedia: available at https://www.electropedia.org/
3.1
test piece
portion of the test sample on which the tensile test is carried out
3.2
proportional test piece
test piece with an original gauge length (L ) having a specified relationship to the square root of the
cross-sectional area (S )
Note 1 to entry: The proportionality coefficient, K, has the internationally recognized value of 5,65 for test pieces
of circular cross-section. The gauge length of a proportional test piece is therefore equal to 5,65√(S_0). Certain
material standards use proportional test pieces with other than the 5,65 proportionality coefficient. In this case,
see A for the percentage elongation symbol used.
x
3.3
non-proportional test piece
test piece where the original gauge length is independent of the cross-sectional area
3.4
extension
increase of the extensometer gauge length (L ) at any moment during the test
e
Note 1 to entry: The unit is mm.
3.5
limit of proportionality
stress at which the stress-strain (or force-extension) relationship deviates from a straight line
Note 1 to entry: The unit is MPa.
3.6
percentage elongation
A
elongation after fracture expressed as a percentage of the original gauge
length (L ) for a proportional test piece with an origin
...
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