Aerospace series - Preparation of carbon fibre reinforced resin panels for test purposes

This standard describes the preparation of panels with any desired fibre orientation of unidirectional orientated carbon fibre or fabric with thermosetting resins.
The purpose of this standard is to describe recommended processes for the preparation of the panels from which test specimens subsequently are machined.
Standard specimens prepared in this manner may be used either for evaluating the components i.e. the carbon reinforcement, finishes, resins, catalysts, curing agents, etc. or for verifying the overall quality of the finished products.

Luft- and Raumfahrt - Herstellen von CFK-Prüfplatten

Diese Norm beschreibt die Vorbereitung von Platten mit jeglicher gewünschter Faserausrichtung aus gleichgerichteten Kohlenstofffasern oder  gewebe mit wärmehärtbaren Harzen.
Der Zweck dieser Norm besteht in der Beschreibung von empfohlenen Prozessen für die Vorbereitung von Platten, aus denen nachfolgend Probekörper maschinell hergestellt werden.
Auf diese Art und Weise hergestellte genormte Probekörper können entweder zur Bewertung der Bestandteile, d. h. der Kohlenstofffaserverstärkung, Oberflächen, Harze, Katalysatoren, Härtungsmittel, usw. oder zur Verifizierung der Gesamtqualität der fertigen Erzeugnisse verwendet werden.

Série aérospatiale - Préparation de panneaux à base de résine et fibres de carbone destinés à l'élaboration d'éprouvettes

Aeronavtika - Priprava smolnih plošč, ojačenih z ogljikovimi vlakni, za namene preskušanja

General Information

Status
Published
Publication Date
20-Aug-2013
Withdrawal Date
27-Feb-2014
Technical Committee
ASD-STAN - Aerospace
Drafting Committee
ASD-STAN/D 4 - Metallic
Current Stage
6060 - Definitive text made available (DAV) - Publishing
Start Date
21-Aug-2013
Completion Date
21-Aug-2013

Overview

EN 2565:2013 is a European standard published by CEN that defines the recommended processes for preparing carbon fibre reinforced resin panels specifically for aerospace testing purposes. It covers panels made with unidirectional carbon fibre or fabric impregnated with thermosetting resins. The primary focus of this standard is to ensure consistent, reproducible preparation of test panels from which specimens are machined. These specimens are then used to evaluate various components such as carbon reinforcements, finishes, resins, catalysts, and curing agents, or to verify the quality of finished aerospace products.

This standard supports quality assurance and material characterization in aerospace manufacturing, emphasizing panel preparation techniques to meet stringent testing requirements.

Key Topics

  • Scope of Application
    Preparation of panels with any desired unidirectional fibre orientation, using either wet lay-up or prepreg methods, for subsequent machining of test specimens.

  • Preparation Methods

    • Method A: Wet lay-up technique involving impregnation of carbon fibres with liquid resin containing catalyst or curing agent, followed by molding under specific temperature and pressure.
    • Method B: Use of prepreg carbon fibre material molded at elevated temperature and pressure.
  • Equipment Requirements
    Includes hydraulic or mechanical presses with precise temperature and pressure controls, autoclaves with vacuum capabilities, measuring instruments (rulers, micrometers, balances), and cutting tools.

  • Materials
    Metal lay-up plates, metal cover plates, pressure retaining rings, release films (e.g., PVF, PTFE), breather materials, absorption fabrics for excess resin, sealing tapes, and edge materials suitable for curing temperatures.

  • Working Procedure
    Conditioning of materials at 23 ± 2 °C and 50 ± 5% relative humidity, controlling resin content, lay-up sequence, curing cycles with temperature and pressure management, post-curing cooling, and panel labelling.

  • Quality Control
    Measurement of panel dimensions-length, width, thickness-with specified accuracy. Determination of fibre content by volume and weight using resin digestion, detection of porosity and defects via ultrasonic inspection.

  • Reporting
    Documentation of production data including ply details, materials, equipment specifics, curing parameters, dimensional measurements, fibre content, porosity levels, and any special notes.

Applications

  • Aerospace Material Testing
    EN 2565 panels serve as the baseline for producing standardized test specimens, enabling reliable assessment of aerospace-grade carbon fibre composites.

  • Quality Assurance in Composite Manufacturing
    Ensures that test panels accurately reflect the intended fibre orientation, resin content, and curing quality, which is critical to verifying batch consistency and product compliance.

  • Research & Development
    Provides a controlled method to prepare panels for evaluating new resin systems, catalysts, or curing techniques applicable in aerospace composites development.

  • Certification and Compliance
    Assists manufacturers and certification bodies in validating that carbon fibre reinforced panels meet rigorous aerospace material standards through standardized preparation and testing.

Related Standards

  • EN 2564 - Aerospace series - Carbon fibre laminates - Determination of fibre, resin, and void contents.
    Complements EN 2565 by providing methods to quantify constituent content in prepared panels.

  • EN 2743 - Aerospace series - Fibre reinforced plastics - Standard conditioning procedures prior to testing unaged materials.
    Specifies the environmental conditioning requirements referenced in EN 2565 for consistent material preparation.

  • Additional Aerospace Composite Standards
    Standards governing testing methods, material specifications, and quality assurance processes for fibre-reinforced polymer composites used in aerospace.


By adhering to EN 2565:2013, aerospace manufacturers and testers can achieve reproducible, high-quality carbon fibre reinforced resin panels essential for robust material testing, product qualification, and ensuring top-tier composite performance in aerospace applications.

Frequently Asked Questions

EN 2565:2013 is a standard published by the European Committee for Standardization (CEN). Its full title is "Aerospace series - Preparation of carbon fibre reinforced resin panels for test purposes". This standard covers: This standard describes the preparation of panels with any desired fibre orientation of unidirectional orientated carbon fibre or fabric with thermosetting resins. The purpose of this standard is to describe recommended processes for the preparation of the panels from which test specimens subsequently are machined. Standard specimens prepared in this manner may be used either for evaluating the components i.e. the carbon reinforcement, finishes, resins, catalysts, curing agents, etc. or for verifying the overall quality of the finished products.

This standard describes the preparation of panels with any desired fibre orientation of unidirectional orientated carbon fibre or fabric with thermosetting resins. The purpose of this standard is to describe recommended processes for the preparation of the panels from which test specimens subsequently are machined. Standard specimens prepared in this manner may be used either for evaluating the components i.e. the carbon reinforcement, finishes, resins, catalysts, curing agents, etc. or for verifying the overall quality of the finished products.

EN 2565:2013 is classified under the following ICS (International Classification for Standards) categories: 49.025.40 - Rubber and plastics. The ICS classification helps identify the subject area and facilitates finding related standards.

EN 2565:2013 is available in PDF format for immediate download after purchase. The document can be added to your cart and obtained through the secure checkout process. Digital delivery ensures instant access to the complete standard document.

Standards Content (Sample)


2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.SUHVNXãDQMDLuft- and Raumfahrt - Herstellen von CFK-PrüfplattenSérie aérospatiale - Préparation de panneaux à base de résine et fibres de carbone destinés à l'élaboration d'éprouvettesAerospace series - Preparation of carbon fibre reinforced resin panels for test purposes49.025.99Drugi materialiOther materialsICS:Ta slovenski standard je istoveten z:EN 2565:2013SIST EN 2565:2014en01-marec-2014SIST EN 2565:2014SLOVENSKI
STANDARD
EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 2565
August 2013 ICS 49.025.40 English Version
Aerospace series - Preparation of carbon fibre reinforced resin panels for test purposes
Série aérospatiale - Préparation de panneaux à base de résine et fibres de carbone destinés à l'élaboration d'éprouvettes
Luft- and Raumfahrt - Herstellen von CFK-Prüfplatten This European Standard was approved by CEN on 8 May 2013.
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-CENELEC 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-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, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and United Kingdom.
EUROPEAN COMMITTEE FOR STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION EUROPÄISCHES KOMITEE FÜR NORMUNG
Management Centre:
Avenue Marnix 17,
B-1000 Brussels © 2013 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 2565:2013: ESIST EN 2565:2014

4.1.2 Autoclave of any dry heat type with the following requirements: a) as 4.1.1 (a); b) a heat up speed of at least 3 °C/min; c) capable of maintaining the required pressure to an accuracy of 10 kPa over the period of time required for curing of the resin; d) vacuum pumps capable of applying a vacuum equal to at least 80 kPa. 4.1.3 Ruler for measuring length and width to an accuracy of 0,5 mm 4.1.4 Micrometer screw type with an accuracy of 0,01 mm for measuring the thickness
4.1.5 Balance with an accuracy of 0,01 g 4.1.6 Cutting device such as a knife with a sharp blade 4.2 Materials 4.2.1 Metal lay-up plate of 500 mm × 500 mm × 7 mm or any other suitable dimensions agreed upon between the parties concerned. 4.2.2 When necessary, metal cover plate of 300 mm × 300 mm × 7 mm or any other suitable dimensions agreed upon between the parties concerned. 4.2.3 Where required, rubber pressure retaining rings resistant to a temperature at least 20 °C higher than the actual curing temperature. 4.2.4 Release film resistant to a temperature at least 20 °C higher than the actual curing temperature, such as polyvinylfluoride (PVF), polytetrafluoroethylene (PTFE) or PTFE coated fabric. 4.2.5 When necessary, perforated release film resistant to a temperature at least 20 °C higher than the actual curing temperature, such as PTFE or PTFE coated fabric. 4.2.6 Pressure blanket material with the
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