BS EN 2334-1997 Chromic-sulphuric acid pickle of aluminium and aluminium alloys《铝和铝合金铬硫酸液》.pdf
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1、BRITISH STANDARD AEROSPACE SERIES BS EN 2334:1997 Chromic-sulphuric acid pickle of aluminium and aluminium alloys The European Standard EN2334:1997 has the status of a British Standard ICS 49.040BSEN2334:1997 This British Standard, having been prepared under the directionof the Engineering SectorBoa
2、rd, was published underthe authority of the Standards Board and comesintoeffect on 15November1997 BSI 04-2000 ISBN 0 580 28135 3 National foreword This British Standard is the English language version of EN2334:1997. The UK participation in its preparation was entrusted to Technical Committee ACE/44
3、, Protective treatments and aircraft finishes, which has the responsibility to: aid enquirers to understand the text; present to the responsible European committee any enquiries on the interpretation, or proposals for change, and keep the UK interests informed; monitor related international and Euro
4、pean developments and promulgate them in the UK. A list of organizations represented on this committee can be obtained on request to its secretary. Cross-references The British Standards which implement international or European publications referred to in this document may be found in the BSI Stand
5、ards Catalogue under the section entitled “International Standards Correspondence Index”, or by using the “Find” facility of the BSI Standards Electronic Catalogue. NOTEUnder the AECMA part numbering system, normative references to the Parts of AECMA-originated European Standards may appear in claus
6、e2 in the form of a three-digit number e.g 001 where the BSI and CEN systems would use the form 1. It can be assumed that, wherever referenced, the three-digit and single digit forms can be used interchangeably. For the purposes of part-marking of components produced in accordance with this standard
7、, the three-digit form should be used. A British Standard does not purport to include all the necessary provisions of a contract. Users of British Standards are responsible for their correct application. Compliance with a British Standard does not of itself confer immunity from legal obligations. Su
8、mmary of pages This document comprises a front cover, an inside front cover, pages i and ii, theEN title page, pages 2 to 6 and a back cover. This standard has been updated (see copyright date) and may have had amendments incorporated. This will be indicated in the amendment table on the inside fron
9、t cover. Amendments issued since publication Amd. No. Date CommentsBSEN2334:1997 BSI 04-2000 i Contents Page National foreword Inside front cover Foreword 2 Text of EN 2334 3ii blankEUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 2334 July 1997 ICS 49.040.40 Descriptors: Aircraft industry, alum
10、inium, aluminium alloys, cleaning English version Aerospace series Chromic-sulphuric acid pickle ofaluminium and aluminium alloys Srie arospatiale Dcapage sulfochromique de laluminium et des alliages daluminium Luft- und Raumfahrt Beizen von Aluminium und Aluminiumlegierungen in Chromschwefelsure Th
11、is European Standard was approved by CEN on1996-08-04. 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
12、concerning such national standards may be obtained on application to the Central Secretariat or to any CEN member. The European Standards exist 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
13、own language and notified to the Central Secretariat has the same status as the official versions. CEN members are the national standards bodies of Austria, Belgium, CzechRepublic, Denmark, Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, S
14、weden, Switzerland and UnitedKingdom. CEN European Committee for Standardization Comit Europen de Normalisation Europisches Komitee fr Normung Central Secretariat: rue de Stassart 36, B-1050 Brussels 1997 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national
15、 Members. Ref. No. EN 2334:1997 EEN2334:1997 BSI 04-2000 2 Foreword This European Standard has been prepared by the European Association of Aerospace Manufacturers (AECMA). After inquiries and votes carried out in accordance with the rules of this Association, this Standard has received the approval
16、 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 January1998, and conflic
17、ting national standards shall be withdrawn at the latest by January1998. According to the CEN/CENELEC Internal Regulations, the national standards organizations of the following countries are bound to implement this European Standard: Austria, Belgium, CzechRepublic, Denmark, Finland, France, German
18、y, Greece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and the UnitedKingdom. Contents Page Foreword 2 1 Scope 3 2 Normative references 3 3 Purpose of process 3 4 Information for the processor 3 5 Condition of parts prior to processing 3 6 Process s
19、chedule 3 7 Pre-treatments 4 8 Treatment 4 9 Post-treatments 4 10 Required characteristics and inspection 4 11 Quality assurance 5 12 Health, safety and environmental aspects 5 13 Designation 5 Annex A (normative) 6 Table 1 3 Table A.1 Pickling solutions 6EN2334:1997 BSI 04-2000 3 1 Scope This stand
20、ard specifies the acid chromate pickling of aluminium and aluminium alloys except those with a silicon content in excess of2% or a copper content in excess of 5%. It is applicable whenever referenced. 2 Normative references This European Standard incorporates by dated or undated reference provisions
21、 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 when incorporated in it by ame
22、ndment or revision. For undated references the latest edition of the publication referred to applies. EN 2000, Aerospace series Quality assurance EN aerospace products Approval of the quality system of manufacturers. 3 Purpose of process 3.1 Reference surface treatment, e.g.prior to adhesive bonding
23、 or primer application to test specimens used for qualification and acceptance tests on adhesives, paints, sealants (treatment A) 3.2 Final treatment for parts prior to adhesive bonding or primer application (treatment B) 3.3 Pre-treatment prior to anodizing for adhesive bonding (treatment C) 3.4 Pr
24、e-treatment (treatment D) for: anodizing for other applications than adhesive bonding; other chemical treatments. 4 Information for the processor Designation, see 13 Number of the material standard and metallurgical condition of the latter Sequence of operations Areas to be processed Treatment 5 Con
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