SIST EN 2243-3:2006
(Main)Aerospace series - Non-metallic materials - Structural adhesives - Test method - Part 3: Peeling test metal-honeycomb core
Aerospace series - Non-metallic materials - Structural adhesives - Test method - Part 3: Peeling test metal-honeycomb core
This standard defines the general requirements for the determination of strength of structural adhesives by testing in peel metal to honeycomb core joints, at ambient or other temperatures.
Luft- und Raumfahrt - Nichtmetallische Werkstoffe - Strukturelle Klebstoffsysteme - Prüfverfahren - Teil 3: Trommelschälversuch für Wabenkernverbunde
Diese Norm legt allgemeine Anforderungen fest zur Bestimmung des Schälwiderstandes von strukturellen Klebstoffen in Metall auf Wabenkernverklebungen bei Raum- oder anderen Temperaturen.
Série aérospatiale - Matériaux non-métalliques - Systeme d'adhésifs structuraux - Méthodes d'essai - Partie 3 : Essai de pelage métal-nid d'abeilles
Aeronavtika – Nekovinski materiali – Konstrukcijska lepila – Preskusna metoda – 3. del: Luščilni preskus, kovina-satasto jedro
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2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Aerospace series - Non-metallic materials - Structural adhesives - Test method - Part 3: Peeling test metal-honeycomb coreSérie aérospatiale - Matériaux non-métalliques - Systeme d'adhésifs structuraux - Méthodes d'essai - Partie 3 : Essai de pelage métal-nid d'abeillesLuft- und Raumfahrt - Nichtmetallische
Werkstoffe - Strukturelle Klebstoffsysteme - Prüfverfahren - Teil 3: Trommelschälversuch für WabenkernverbundeTa slovenski standard je istoveten z:EN 2243-3:2005SIST EN 2243-3:2006en49.025.50ICS:SLOVENSKI
STANDARDSIST EN 2243-3:200601-julij-2006
EUROPEAN STANDARDNORME EUROPÉENNEEUROPÄISCHE NORMEN 2243-3October 2005ICS 49.025.50Supersedes EN 2243-3:1991
English VersionAerospace series - Non-metallic materials - Structural adhesives- Test method - Part 3: Peeling test metal-honeycomb coreSérie aérospatiale - Matériaux non-métalliques - Systèmed'adhésifs structuraux - Méthodes d'essai - Partie 3 : Essaide pelage métal-nid d'abeillesLuft- und Raumfahrt - Nichtmetallische
Werkstoffe -Strukturelle Klebstoffsysteme - Prüfverfahren - Teil 3:Trommelschälversuch für WabenkernverbundeThis European Standard was approved by CEN on 26 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 2243-3:2005: E
EN 2243-3:2005 (E) 2 Contents Page Foreword.3 Introduction.4 1 Scope.4 2 Normative references.4 3 Definitions, symbols and abbreviations.4 4 Health and safety.5 5 Principle/Technique.5 6 Resources.5 7 Test samples/Test pieces.6 8 Testing procedure.7 9 Expression of results.8 10 Designation.9 11 Test report.9
EN 2243-3:2005 (E) 3 Foreword This European Standard (EN 2243-3:2005) 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 April 2006, and conflicting national standards shall be withdrawn at the latest by April 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. This European Standard supersedes EN 2243-3:1991. 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 2243-3:2005 (E) 4 Introduction This standard is part of the series of EN non-metallic material standards for aerospace applications. The general organization of this series is described in EN 4385. This standard is a level 3 document as defined in EN 4385. 1 Scope This standard defines the general requirements for the determination of strength of structural adhesives by testing in peel metal to honeycomb core joints, at ambient or 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 ISO 7500-1, Metallic materials — Verification of static uniaxial testing machines — Part 1: Tension/ compression testing machines — Verification and calibration of the force-measuring system (ISO 7500-1:2004). EN 2090, Aerospace series — Aluminium alloy AL-P2024- — T3 — Clad sheet and strip — 0,3 mm ≤ a ≤ 6 mm.1) EN 2334, Aerospace series — Chromic-sulphuric acid pickle of aluminium and aluminium alloys. EN 4385, Aerospace series — Non-metallic materials — General organisation of standardisation — Links between types of standards.1) EN 4606, Aerospace series — Aluminium honeycomb core.2)
3 Definitions, symbols and abbreviations 3.1 Definitions Not applicable 3.2 Symbols and abbreviations For the purposes of this document, the following symbols and abbreviations apply. F peeling load (in newtons); F0 rolling load (in newtons) = Load necessary to roll up the skin;
1) Published as AECMA Prestandard at the date of publication of this standard. 2) In preparation at the date of publication of this standard.
EN 2243-3:2005 (E) 5 F1 peeling and rolling load (in newtons); W width of test piece (in centimeter); τ peeling strength (in newtons . centimetre/centimetre). 4 Health and safety This standard does not necessarily include all health and safety requirements, associated with its use. Persons using this standard shall be familiar with normal laboratory/test house practices. It is the responsibility of the user to establish satisfactory health and safety practices and to ensure conformity with any European, national or local laws/regulations. 5 Principle/Technique Not applicable 6 Resources 6.1 Apparatus All test equipment shall be calibrated at intervals not exceeding 12 months. 6.1.1 Tensile testing machine The tensile testing machine shall conform to class 1 of EN I
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