AECMA PREN 3837-1996 Aerospace Series Paints and Varnishes Nature and Method for Surface Preparation of Test Pieces in Aluminium Alloys Edition P 1《航空航天系列.漆和清漆用于铝合金试样表面准备种类和方法》.pdf

《AECMA PREN 3837-1996 Aerospace Series Paints and Varnishes Nature and Method for Surface Preparation of Test Pieces in Aluminium Alloys Edition P 1《航空航天系列.漆和清漆用于铝合金试样表面准备种类和方法》.pdf》由会员分享，可在线阅读，更多相关《AECMA PREN 3837-1996 Aerospace Series Paints and Varnishes Nature and Method for Surface Preparation of Test Pieces in Aluminium Alloys Edition P 1《航空航天系列.漆和清漆用于铝合金试样表面准备种类和方法》.pdf（6页珍藏版）》请在麦多课文档分享上搜索。

1、AECMA STANDARD NORME AECMA AECMA NORM Edition approved for publication prEN 3837 Edition P 1 November 1996 Comments should be sent within six months C7 Chairman after the date of Dublication to PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES (AECMA) Gulledelle 94 - B-1200 BRUXELLES - T

2、el. (32) 2 775 81 10 - Fax. (32) 2 775 81 11 ICs : Descriptors : ENGLISH VERSION Aerospace series Paints and varnishes Nature and method for surface preparation of test pieces in aluminium alloys Srie arospatiale Peintures et vernis Nature et mthodes de prparation de surface des prouvettes en alliag

3、es daluminium Luft- und Raumfahrt Lacke und Anstrichstoffe Oberflchenvorbereitungstyp und methoden fr Proben aus Aluminiumlegierungen This “Aerospace Series“ Prestandard has been drawn up under the responsibility of AECMA (The European Association of Aerospace Industries). It is published on green p

4、aper for the needs of AECMA-Members. It has been technically approved by the experts of the concerned Technical Committee following comment by the Member countries. Subsequent to the publication of this Prestandard, the technical content shall not be changed to an extent that interchangeability is a

5、ffected, physically or functionally, without re-identification of the standard. After examination and signature of the AECMA Standard Checking Centre (NPS) and formal agreement of the Official Services of the Member countries it will be submitted as a draft European Standard to CEN (European Committ

6、ee for Standardization) for formal vote. 1996-1 1-29 AECMA Gulledelle 94 Mr Wrigth I 8-1 200 BRUXELLES I aecrna 1996 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license

7、 from IHS-,-,-Page 3 prEN 3837 : 1996 1 Scope This standard defines the nature of and the surface preparation method for test pieces in aluminium alloys intended for testing paints and varnishes used for aerospace applications. 2 Normative references This European Standard incorporates by dated or u

8、ndated reference provisions from 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 apply to this European Standard only whe

9、n incorporated in it by amendment or revision. For undated references the latest edition of the publication referred to applies. IS0 3270 EN 2090 EN 2092 EN 2101 EN 2334 EN 2437 EN 2696 EN 2709 Paints and varnishes and their raw materials - Temperatures and humidities for conditioning and testing Ae

10、rospace series - Aluminium alloy 2024-T3 - Clad sheet and strip - 0,4 5 a I6 mm 1) Aerospace series - Aluminium alloy AL-P7075- - T6 or T62 - Clad sheet and strip - 0,4 mm 5 a 56 mm Aerospace series - Chromic acid anodizing of aluminium and wrought aluminium alloys Aerospace series - Chromic-sulphur

11、ic acid pickle of aluminium and aluminium alloys 1) Aerospace series - Chromate conversion coatings (yellow) for aluminium and aluminium alloys 2) Aerospace series - Aluminium alloy AL-P7075- - T6 or T62 - Sheet and strip - 0,4 mm I a I6 mm Aerospace series - Aluminium alloy 2024-T3510 - Bar and sec

12、tion - 1,2 I (a or D) I 150 mm - With peripheral coarse grain control 1) 3 Nature and size of test pieces Unless specifically defined, test pieces in aluminium alloys are described in table 1. Unless otherwise specified in the test or product standard, the dimensions of the test pieces shall be : le

13、ngth : 125 mm width : 80 mm. 4 Method of preparing the surface Three processes surface treatments are applicable to aluminium alloys used in aeronautics : - process A: sulfochromic pickling in accordance with EN 2334 : - process B: chromic acid anodizing, sealed or not, in accordance with EN 2101 ;

14、- process C: chemical chromatation conversion in accordance with EN 2437. Each series gives the order and the nature of the different operations to be carried out (treatment, rinsing, stoving). Annexes A and B give the degreasing procedures before treatment. Process A is the “reference“ treatment. T

15、he choice of the treatment, processes B and/or C, is the result of an agreement between the interested parties or is imposed by the product specification. 1) Published as AECMA Standard at the date of publication of this standard 2) In preparation at the date of publication of this standard Copyrigh

16、t 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 4 prEN 3837 : 1996 5 Application of coating Coating shall be applied within 16 h after the end of the trea

17、tment and in conformity with the product specification and the suppliers instructions. After applying the paint and prior to testing, the test pieces shall be kept in a room in conformity with IS0 3270 for the time specified in the material standard. Table : Synoptic table of test pieces I Nature I

18、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 5 prEN 3837 : 1996 6 The locally applicable regulations and laws shall be observed. Health, safety

19、 and environmental aspects 7 Designation EXAMPLE : EN3837A IT Number of this standard I Process (see 4) 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、-1012311 OOL3OLB 035 Page 6 prEN 3837 : 1996 Annex A (informative) SOLVENT DEGREASING This operation can be carried out : - in vapour phase ; - in liquid phase using a paint brush and a cloth that leaves no lint. Solvents used : - stabilized trichloroethylene (vapour phase) ; - standard quality perc

21、hlorothylene (vapour phase) ; - stabilized trichloroethane 1, 1, 1 (vapour or liquid phase) ; - other degreasing agent required by the customer. NOTE 1 : The possible ink markings on the surface of the sheets and extruded section shall be eliminated with denaturated alcohol. NOTE 2 : A regular film

22、of water shall cover the pieces after rinsing, otherwise degreasing shall be repeated. 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-,-,-.- LO12311 00130

23、19 T7L Page 7 prEN 3837 : 1996 Annex B (informative) CHEMICAL DEGREASING Examples of bath composition and treatment parameters Bath composition : - anhydrous sodium carbonate Nazco3 - anhydrous sodium phosphate Na3P04 - liquid silicate of sodium (r = 1,331 NapSiO3 - deionized water. Treatment parame

24、ters : - temperature - immersion time - air or mechanical stirring. : (40 I 1) g/l : (20 f 1) g/l : (1 f 0,l) g/l : (60 f 2) OC : (4f 1) min NOTE : A regular film of water shall cover the pieces after rinsing, otherwise degreasing shall be repeated. 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-,-,-