SIST EN 2243-1:2006
(Main)Aerospace series - Non-metallic materials - Structural adhesives - Test method - Part 1: Single lap shear
Aerospace series - Non-metallic materials - Structural adhesives - Test method - Part 1: Single lap shear
The objective of this standard is to establish the test methods for defining the strength of suitable structural adhesives in metal to metal single lap shear, at ambient and other temperatures.
Luft- und Raumfahrt - Nichtmetallische Werkstoffe - Strukturelle Klebstoffe - Prüfverfahren - Teil 1: Bestimmung der Bindefestigkeit von einschnittig überlappten Klebungen im Zugversuch
Diese Norm legt die Prüfverfahren zur Bestimmung der Bindefestigkeit von strukturellen Klebstoffen an einschnittig überlappten Metallklebungen im Zugversuch bei Raumtemperaturen und anderen Temperaturen fest
Série aérospatiale - Matériaux non-métalliques - Systeme d'adhésifs structuraux - Méthodes d'essai - Partie 1 : Essais de cisaillement d'un joint a recouvrement simple
Aeronavtika – Nekovinski materiali – Konstrukcijska lepila – Preskusna metoda – 1. del: Strig enojnega prekritja
General Information
Standards Content (Sample)
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Aerospace series - Non-metallic materials - Structural adhesives - Test method - Part 1: Single lap shearAeronavtika – Nekovinski materiali – Konstrukcijska lepila – Preskusna metoda – 1. del: Strig
enojnega prekritjaSérie aérospatiale - Matériaux non-métalliques - Systeme d'adhésifs structuraux - Méthodes d'essai - Partie 1 : Essais de cisaillement d'un joint a recouvrement simpleLuft- und Raumfahrt - Nichtmetallische Werkstoffe - Strukturelle Klebstoffe - Prüfverfahren - Teil 1: Bestimmung der Bindefestigkeit von einschnittig überlappten Klebungen im ZugversuchTa slovenski standard je istoveten z:EN 2243-1:2005SIST EN 2243-1:2006en49.025.50ICS:SLOVENSKI
STANDARDSIST EN 2243-1:200601-julij-2006
EUROPEAN STANDARDNORME EUROPÉENNEEUROPÄISCHE NORMEN 2243-1November 2005ICS 49.025.50 English VersionAerospace series - Non-metallic materials - Structural adhesives- Test method - Part 1: Single lap shearSérie aérospatiale - Matériaux non-métalliques - Systèmed'adhésifs structuraux - Méthodes d'essai - Partie 1 :Essais de cisaillement d'un joint à recouvrement simpleLuft- und Raumfahrt - Nichtmetallische Werkstoffe -Strukturelle Klebstoffsysteme - Prüfverfahren - Teil 1:Bestimmung der Bindefestigkeit von einschnittigüberlappten Klebungen im ZugversuchThis European Standard was approved by CEN on 30 September 2005.CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this EuropeanStandard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning such nationalstandards may be obtained on application to the Central Secretariat or to any CEN member.This European Standard exists in three official versions (English, French, German). A version in any other language made by translationunder the responsibility of a CEN member into its own language and notified to the Central Secretariat has the same status as the officialversions.CEN members are the national standards bodies of Austria, Belgium, Cyprus, Czech Republic, Denmark, Estonia, Finland, France,Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Slovakia,Slovenia, Spain, Sweden, Switzerland and United Kingdom.EUROPEAN COMMITTEE FOR STANDARDIZATIONCOMITÉ EUROPÉEN DE NORMALISATIONEUROPÄISCHES KOMITEE FÜR NORMUNGManagement Centre: rue de Stassart, 36
B-1050 Brussels© 2005 CENAll rights of exploitation in any form and by any means reservedworldwide for CEN national Members.Ref. No. EN 2243-1:2005: E
EN 2243-1:2005 (E) 2 Contents Page Foreword.3 1 Scope.4 2 Normative references.4 3 Test samples.4 4 Surface preparation.5 5 Bonding.5 6 Storage of test samples after bonding.5 7 Cutting and preparation of test pieces.5 8 Test conditions.6 9 Method of test.6 10 Calculation of results.6 11 Test report.7
EN 2243-1:2005 (E) 3 Foreword This European Standard (EN 2243-1:2005) has been prepared by the European Association of Aerospace Manufacturers - Standardization (AECMA-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 AECMA, 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 May 2006, and conflicting national standards shall be withdrawn at the latest by May 2006. 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, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom.
EN 2243-1:2005 (E) 4 1 Scope The objective of this standard is to establish the test methods for defining the strength of suitable structural adhesives in metal to metal single lap shear, at ambient and other temperatures. 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. EN 2087, Aerospace series – Aluminium alloy AL-P2014A – T6 or T62 – Clad sheet and strip – 0,4 mm ≤ a ≤ 6 mm.1)
EN 2088, Aerospace series – Aluminium alloy AL-P2014A – T4 or T42 – Clad sheet and strip – 0,4 mm ≤ a ≤ 6 mm. 1) EN 2090, Aerospace series – Aluminium alloy AL-P2024- – T3 – Clad sheet and strip – 0,3 mm ≤ a ≤ 6 mm. 1) EN 2092, Aerospace series – Aluminium alloy AL-P7075- – T6 or T62 – Clad sheet and strip – 0,4 mm ≤ a ≤ 6 mm. EN 2334, Aerospace series – Chromic-sulphuric acid pickle of aluminium and aluminium alloys. EN 2497, Aerospace series – Dry abrasive blasting of titanium and titanium alloys. EN 2
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