ASD-STAN PREN 2334-1995 Aerospace Series Chromic-Sulphuric Acid Pickle of Aluminium and Aluminium Alloys (Edition 1)《航空航天系列 铝和铝合金的铬-硫酸酸洗 第1版》.pdf
《ASD-STAN PREN 2334-1995 Aerospace Series Chromic-Sulphuric Acid Pickle of Aluminium and Aluminium Alloys (Edition 1)《航空航天系列 铝和铝合金的铬-硫酸酸洗 第1版》.pdf》由会员分享,可在线阅读,更多相关《ASD-STAN PREN 2334-1995 Aerospace Series Chromic-Sulphuric Acid Pickle of Aluminium and Aluminium Alloys (Edition 1)《航空航天系列 铝和铝合金的铬-硫酸酸洗 第1版》.pdf(6页珍藏版)》请在麦多课文档分享上搜索。
1、AECMA PRENa2334 95 U LOL23Ll 08LOO 562 for publication 1995-1 2-29 AECMA STANDARD NORME AECMA AECMA NORM I - can be supplied by B.N.A.E. - Technopolis 54 - 199, rue Jean-Jacques Rousseau 92138 ISSY - LES - MOULINEAUX CEDEX - FRANCE prEN 2334 Edition 1 December 1995 PUBLISHED BY THE EUROPEAN ASSOCIAT
2、ION OF AEROSPACE INDUSTRIES (AECMA) Gulledelle 94 - B-1200 BRUXELLES - Tel. (32) 2 775 81 10 - Fax. (32) 2 775 81 11 ICs : 49.040.40 Descriptors : Aircraft industry, aluminium, aluminium alloys, cleaning ENGLISH VERSION Aerospace series Chromic-sulphuric acid pickle of aluminium and aluminium alloys
3、 Srie arospatiale Luft- und Raumfahrt Dcapage sulfochromique de laluminium et des alliages daluminium Beizen von Aluminium und Aluminiumlegierungen in Chromschwefelsure This “Aerospace series“ Standard has been drawn up under the responsibility of AECMA (The European Association of Aerospace Industr
4、ies). It is published on yellow paper in three equivalent versions (English, French, German). It will be submitted as a draft European Standard to CEN (European Committee for Standardization) for formal vote. I Edition aDDrOVed I The eauivalent versions in French and German languages 1 I I aecma 199
5、5 Page 3 prEN 2334 : 1995 1 Scope This standard specifies the acid chromate pickling of aluminium and aluminium alloys except those with a silicon content in excess of 2 % or a copper content in excess of 5 %. It is applicable whenever referenced. 2 Purpose of process 2.1 specimens used for qualific
6、ation and acceptance tests on adhesives, paints, sealants (treatment A). Reference surface treatment, e.g. prior to adhesive bonding or primer application to test 2.2 Final treatment for parts prior to adhesive bonding or primer application (treatment BI. 2.3 Pre-treatment before anodizing for adhes
7、ive bonding (treatment Cl. 2.4 - anodizing for other applications than adhesive bonding ; - other chemical treatments. Pre-treatment (treatment D) for : 3 Normative references This European Standard incorporates by dated or undated reference provisions from other publications. These normative refere
8、nces 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 when incorporated in it by amendment or revision. For undated references the l
9、atest edition of the publication referred to applies. EN 2000 Aerospace series - Quality assurance EN aerospace products - Approval of the quality system of manufacturers 4 Information for the processor - Designation, see 13 ; - Number of the material standard and metallurgical condition of the latt
10、er ; - Sequence of operations ; - Areas to be processed ; - Treatment. 5 Condition of parts prior to processing Fabrication of the parts shall have been completed before pickling. - AECIA PRENs2334 95 1012311 0010102 987 = Process schedule Pre-treatments Pickling Post-treatments Page 4 EN 2334 : 199
11、5 Application, see treatment A B C D 7.1 7.2 7.2 7.2 8 8 8 8 9.1 9.1 9.1 9.1 9.2 9.2 9.3 9.3 6 Process schedule 7 Pre-treatments 7.1 7.1.1 hot alkaline solution. Cleaning for treatment A (see 2.1) Vapour degreasing, solvent cleaning or alkaline cleaning with a non-etching, non-silicated 7.1.2 Water
12、rinsing and check for water break, repeat cleaning if break occurs. 7.2 7.2.1 Cleaning for treatments B, C, D (see 2.2, 2.3 and 2.4) Heavily soiled parts shall be emulsion cleaned, vapour degreased or solvent cleaned. 7.2.2 If there is a natural oxide film, carry out abrasive blasting or chemical de
13、oxidizing. When pickling does not follow immediately after these operations, the parts shall be vapour degreased or cleaned with a hot alkaline solution. 7.2.3 solution. The alkaline solution shall be corrosion inhibited and preferably of a non-silicated type. For the parts to be bonded a non-silica
14、ted alkaline solution is mandatory. After alkaline cleaning, the parts shall be thoroughly water rinsed and inspected for water break. Cleaning shall be repeated if break occurs. If there is no significant natural oxide film, parts shall be cleaned with a hot alkaline 8 Treatment Immediately after f
15、inal cleaning, the parts shall be pickled in one of the solutions specified in annex A. To ensure a well pickled surface, the following shall be observed : - excessive bath loading and shielding of parts by each other shall be avoided ; - to ensure satisfactory adhesion and durability properties for
16、 treatments A and B or to obtain a satisfactory metal removal rate, pure aluminium and certain aluminium alloys with a very low - AECIA PRENm2334 75 LOL23LL OOLOL03 813 Page 5 prEN 2334 : 1995 copper content at the surface (clad aluminium alloys, AI-Mg alloys) require additional provisions. The part
17、s in these materials shall be either suspended on supporting jigs which shall be more noble (cathodic) relative to the materials to be treated, e.g. unclad AI-Cu alloy, or coupled to auxiliary cathodes. The position of the parts (anodes) relative to the cathodic areas and the cathodic to anodic area
- 1.请仔细阅读文档,确保文档完整性,对于不预览、不比对内容而直接下载带来的问题本站不予受理。
- 2.下载的文档,不会出现我们的网址水印。
- 3、该文档所得收入(下载+内容+预览)归上传者、原创作者;如果您是本文档原作者,请点此认领!既往收益都归您。
下载文档到电脑,查找使用更方便
10000 积分 0人已下载
下载 | 加入VIP,交流精品资源 |
- 配套讲稿:
如PPT文件的首页显示word图标,表示该PPT已包含配套word讲稿。双击word图标可打开word文档。
- 特殊限制:
部分文档作品中含有的国旗、国徽等图片,仅作为作品整体效果示例展示,禁止商用。设计者仅对作品中独创性部分享有著作权。
- 关 键 词:
- ASDSTANPREN23341995AEROSPACESERIESCHROMICSULPHURICACIDPICKLEOFALUMINIUMANDALUMINIUMALLOYSEDITION1 航空航天

链接地址:http://www.mydoc123.com/p-450929.html