1、AECMA Technical Report Rapport Technique AECMA AECMA Fach bericht Edition approved for publication 28 June 2002 TR 7000-9 Edition 1 June 2002 Extra copies can be supplied by B.N.A.E. Technopolis 54 - 199, rue Jean-Jacques Rousseau Non-metallic Material Domain 92138 ISSY - LES - MOULINEAUX CEDEX - FR
2、ANCE PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES - STANDARDIZATION 1 AEEmksTfifl Gulledelle 94 - B-1200 Brussels - Tel. + 32 2 775 81 10 - Fax. + 32 2 775 81 11 - www.aecma-stan.org Supersedes prEN 7000-9 Edition PI September 1998 ENGLISH VERSION Aerospace se ri es Non-metallic mat
3、erials Rules for the drafting and presentation of material standards Part 9: Paints and varnishes Srie arospatiale Luft- und Raumfahrt Matriaux non-mtalliques Nichtmetallische Werkstoffe Rgles pour la prparation et la prsentation des normes de matriaux Partie 9 : Peintures et vernis Regeln fr die Er
4、stellung und die Gestaltung von Werkstoffnormen Teil 9: Farben und Lacke This Technical Report was drawn up by the Non-metallic Material Domain of AECMA-STAN. The reason which led to the publication of the document as a Technical Report is explained in the foreword. Copyright Association Europeene d
5、es Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 2 TR 7000-9: 06-02 Foreword The main task of AECMA-STAN is to prepare EN standards. In exceptional circumstances, however, the publ
6、ication of a Technical Report of one of the following types may be proposed : - type I, the subject is still under technical development requiring wider exposure ; - type 2, a Technical Committee has collected data of a different kind from that which is normally published as a European Standard. The
7、 Non-metallic Material Domain decided to publish this document in the form of a Technical Report of type 2 in order to facilitate the updating of this document. Contents Page O 3 I 2 3 Definitions, symbols and abbreviations . 3 4 Annex A (normative) Annex B (normative) Annex C (informative) Example
8、8 Rules for the drafting and presentation Table AI - Characteris Table BI - Characteristic numbers applicable to Tables 2 to 4: General requirements Other requirements . . 6 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for Resa
9、leNo reproduction or networking permitted without license from IHS-,-,-Page 3 TR 7000-9: 06-02 O Introduction This standard is part of the series of TR non-metallic materials standards for aerospace applications. The general organisation of this series is described in EN 4385. This document is a lev
10、el 2 document as defined in EN 4385. It shall be used in conjunction with TR 7000-1. 1 Scope This standard specifies the rules for drafting and presentation of EN aerospace series non-metallic material standards for paints and varnishes for aerospace applications. 2 Normative references This Europea
11、n standard incorporates by dated or undated reference provisions for other publications. These normative references are cited at the appropriate places in the text and the publications are listed hereafter. For dated references, subsequent amendments to or revisions of any of these publications appl
12、y to this European Standard only when incorporated in it by amendment or revision. For undated references, the latest edition of the publication refered to applies. EN 4385 Aerospace series - Non-metallic materials - General organisation of standardisation - Links between types of standards 1) TR 70
13、00-1 Aerospace series - Non-metallic materials - Rules for the drafting and presentation of material standards - Part 1 : General rules 2) 3 Defini tions, symbols and abbreviations See TR 7000-1. 4 Rules for the drafting and presentation NOTE standardisation EN products. The examples given below are
14、 only intended to illustrate the rules, and may not correspond to real 4.1 Title See TR 7000-1 and annex C of this standard. The following are example of descriptions which shall be used; these examples may be supplemented by other descriptions as required by the relevant Project Team. 1) Published
15、as AECMA Prestandard at the date of publication of this standard 2) Published as AECMA Technical Report at the date of publication of this standard Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or netwo
16、rking permitted without license from IHS-,-,-Page 4 TR 7000-9: 06-02 1 Type of paint: - Polyurethane - EPOXY - Acrylic - Fluorocarbon - Polysulphide 2 Additional information: - Single component - Two (or more) components - Cold curing - Hot curing 3 Intended application: - Flexible exterior finish -
17、 Flexible interior finish - Primer - Chemical resistant finish - Chromate free primer - Fuel tank primer - IR absorbing 4.2 Contents See TR 7000-1 and annex C of this standard. 4.3 Clause O: Onwards See TR 7000-1 and annex C of this standard. 4.4 General requirements See TR 7000-1. 4.4.1 The charact
18、eristic numbers applicable to Table 1 are given in annex A of this standard. All of the characteristics given in Table 1 are mandatory and shall be completed in accordance with TR 7000-1 and annex C of this standard. Table 1 - General requirements 4.4.2 Tables 2 to 4 See TR 7000-1 and annex C of thi
19、s standard. The characteristic numbers applicable to tables 2 to 4 are given in annex B of this standard. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,
20、-,-Page 5 TR 7000-9: 06-02 Characteristic number 1 .o01 Annex A (normative) Characteristics Material description Table AI - Characteristic numbers applicable to Table 1 : General requirements 1 .o02 1 .O03 Formulation Form and method of production 1 .O04 I .O05 Technical specification Grade 1 .O06 1
21、 .O07 1 .O08 Service temperature Visualkolour Freedom from defects 1 .o09 1.010 Application Storage 1.011 1.013 Shelf life Processing condition I .O93 1 .O94 I 1 .O97 I Flash point Quality assurance certificate Designation 1 .O95 1 .O96 Packaging Identification marking 1 .O98 1.999 Health, safety an
22、d environment Notes Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 6 TR 7000-9: 06-02 31 Annex B (normative) Table BI - Characteristic numbers ap
23、plicable to Tables 2 to 4: Other requirements Characteristic number 1 o1 103 104 106 107 097 110 111 112 113 continued Characteristic 2 Wet chemical analysis - water content - amine value - hydoxyl value - isocyanate value - epoxyvalue - acid value - phosphoric - gas chromatography - IR spectroscopy
24、 Formulation X X Composition - volatile organic content - non-volatile matter - pigment content - fineness of grind - leachability Reactivity - reactivity (8 to + 4 h) - surfacedry - print free dry - through dry X X Rheology - viscosity (flow time) - high shear rate X Flammability Dimensional - flas
25、h point - covering capacity - volume of dry film - specular gloss - IR reflection factor - refractive index Electromagnetic - conductivity Optical properties X X x Sedimentation ix X 4 X Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECM
26、ANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 7 TR 7000-9: 06-02 Table BI (concluded) Characteristic number I I 30” I 304 Characteristic Density - hydrometer I Normal 2 X Hardness Thermomechanical r used in table(s) 3(4 XIX xT Adhesion Tensile properties Im
27、pact Tri bolog cal - tensile properties of the film - impact resistance - abrasion resistance XIX x XI Bend test - cylindrical mandrel - cupping test X X Resistance to Aeronautical fluids X Resistance to dry heat X Wet heat X Thermal cycling / shock X - humidity absorption Ageing - natural - artific
28、ial Salt spray - neutral salt X X Filiform corrosion X Alternative immersion X - sodium chloride Microbiological I Water resistance (immersion)-absorption X Notes I I I I Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleN
29、o reproduction or networking permitted without license from IHS-,-,-Page 8 TR 7000-9: 06-02 Annex C (informative) Exam p I e Example C.l EN xxxx ENGLISH VERSION Aerospace series Non-metallic materials Paints and varnishes Pol y u ret ha ne Two component - cold curing Flexible exterior finish Srie ar
30、ospatiale Matriaux non-mtalliques Peintures et vernis Polyurthane Deux composants - polymrisation froid Finition extrieure flexible Luft- und Raumfahrt Nichtmetallische Werkstoffe Farben und Lacke Zweikomponenten Polyurethan - Decklack Raumtemperaturhrtend Copyright Association Europeene des Constru
31、cteurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 9 TR 7000-9: 06-02 Blank page Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AE
32、CMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 10 TR 7000-9: 06-02 Example C.1 (continued) Page 3 EN xxxx O Introduction This standard is part of the series of non-metallic materials standards for aerospace applications. The general organisation of this se
33、ries is described in EN 4385. This standard is a level 3 document as defined in EN 4385. It has been prepared in accordance with TR 7000-9. I Scope This standard specifies the requirements relating to a two component, cold curing, high flexibility, polyurethane exterior finish for aerospace applicat
34、ions. 2 Normative references This European Standard incorporates by dated or undated reference, provisions from other publications. These normative references are cited at the appropriate places in the next and the publications are listed hereafter. For dated references, subsequent amendments to or
35、revisions of any of these publications apply to this European Standard only when incorporated in it by amendment or revision. For undated references the latest edition of the publication referred to applies. IS0 1517 IS0 1519 IS0 2431 IS0 281 1 IS0 2884 IS0 3675 IS0 3678 IS0 6272 IS0 9117 EN 2243-4
36、EN 2379 EN 2435 EN 2642 EN 3837 EN 3840 EN 4385 TR 7000-9 Paints and varnishes - Surace-drying test - Ballotini method Paints and varnishes - Bend test (cylindrical mandrel) Paints and varnishes - Determination of flow time by use of flow cups Paints and varnishes - Determination of density Paints a
37、nd varnishes - Determination of viscosity using rotary viscometers - Part 1: Cone-and-plate viscometer operated at a high rate of shear Crude Petroleum and Liquid petroleum Products - Laboratory determination of density - Hydrometer method Paints and varnishes - Print-free test Paints and varnishes
38、- Falling weight test Paints and varnishes - Determination of through-dry state and through-dry time - Method of test Aerospace series - Non-metallic materials - Structural adhesives - Test method - Part 4: Metal-honeycomb core flatwise tensile test Aerospace series - Fluids for assessment of non-me
39、tallic materials ) Aerospace series - Paints and varnishes - Corrosion resistant chromated two component cold curing primer ) Aerospace series - Structural adhesive systems -Adhesive film -Technical specification ) Aerospace series - Paints and varnishes - Nature and method for surface preparation o
40、f test pieces in aluminium alloys ) Aerospace series - Paints and varnishes - Technical specification ) Aerospace series - Non-metallic materials - General organisation of standardisation - Links between types of standards ) Aerospace series - Non-metallic materials - Rules for the drafting and pres
41、entation of material standards - Part 9: Paints and varnishes *) 1) Published as AECMA Prestandard at the date of publication of this standard 2) Published as AECMA Technical Report at the date of publication of this standard Copyright Association Europeene des Constructeurs de Materiel Aerospatial
42、Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 11 TR 7000-9: 06-02 3.1 Definitions 3.1.1 Sub-case numbering In the column requirement at the left hand side a sub-case number is given. The definition of these sub- case n
43、umbers is as follows: Sub-case number Definition - Technical specification 1 Test method 2 Frequency of testing 3 Sample type 4 Test piece definition 5 Conditioning of test piece 6 Testing condition 7 Acceptance criteria I NOTE 1 The absence of a sub-case indicates that the necessary information is
44、given in Table 1 of this standard, e.g. In the reference to the technical standard (characteristic 1.004). All the necessary information which does not appear is to be found in the referenced technical specification or the relevant test method. NOTE 2 In this material standard, batch acceptance test
45、 titles and sub-cases 7 acceptance criteria are highlighted in the form of a bold frame and bold characters to show that they are mandatory for routine acceptance of the material. 3.2 Symbols and abbreviations See EN 3840. 4 Requirements The required characteristics are given in: Table 1 : General r
46、equirements Table 2: Requirements in the delivery condition Table 3: Requirements as processed to characteristic number 1 .O13 Table 4: Environmental testing requirements as processed to characteristic number 1 .O1 3 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided
47、by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 12 TR 7000-9: 06-02 Non-thixotropic Example C.l (continued) Page 5 EN xxxx EN xxxx - II Table 1 - General requirements Characteristic Requirements Characteristic number 1 .o01 Mater
48、ial description Formulation Polyurethane paint - flexible exterior finish Base - hydroxyl functional resin, solvent and pigments to give the required colour, gloss and any other reflective characteristics. Activator - polyisocyanate solution Thinner - if required 1 .o02 1 .O03 Form and method of production Technical specification Two part component 1 .O04 EN 3840 1 .O05 Grade Type I - Thixotropic Type II - Non-thixotropic Class A - high gloss Class B - semi matt Class C - matt 1 .O06 Service temperature “C I 1 O0 1 .O07 Colou
