EN 2101-1991 en Chromic Acid Anodizing of Aluminium and Wrought Aluminium Alloys《航空航天系列 铝合金和锻铝合金铬酸阳极化》.pdf
《EN 2101-1991 en Chromic Acid Anodizing of Aluminium and Wrought Aluminium Alloys《航空航天系列 铝合金和锻铝合金铬酸阳极化》.pdf》由会员分享,可在线阅读,更多相关《EN 2101-1991 en Chromic Acid Anodizing of Aluminium and Wrought Aluminium Alloys《航空航天系列 铝合金和锻铝合金铬酸阳极化》.pdf(15页珍藏版)》请在麦多课文档分享上搜索。
1、EUROPEAN STANDARD EN 2101 NORME EUROPENNE EUROPISCHE NORM July 1991 UDC : 669.71 5.691.51546.766-32:629.7 Key words : Aircraft industry, aluminium, aluminium alloys, rolled products, anodizing, chromic acid, setting- up conditions, quality assurance, corrosion resistance, inspection. English version
2、 Aerospace series Chromic acid anodizing of aluminium and wrought aluminium alloys 1 Srie arospatiale Luft- und Raumfahrt von Aluminium und . Anodisation chromique C hromsaure- Anodicieren alliages da luminium corroys Aluminium-Knetlegierungen de laluminium et des This European Standard was accepted
3、 by CEN on 1990-06-28. CEN members are bound to comply with the requirements of CEN Internal Regulations which stipulate the conditionsfor giving this European Standard the status of a national standardwithout any alteration. Up-to-date lists and bibliographical references concerning such national s
4、tandards may be obtained on application to the CEN Central Secretariat 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 noti
5、fied to CEN Central Secretariat has the came status as the official versions. CEN members are the national standards organizations of Austria, Belgium, Denmark, Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxemburg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and United
6、Kingdom. CEN European Committee for Standardization Comit Europen de Normalisation Europisches Komitee fr Normung Central Secretariat : Rue de Stassart, 36, B-1 O50 Bruxelles _p CEN 1991 Copyright reserved to all CEN members Ref. Nr EN 2101 : 1991 E a- 0 CEN EN*ZLOL 91 W 3404589 0035328 3 mi Content
7、s Scope and field of application Purpose of anodizing References Material categories Supporting jig Processing sequence Quality assurance Designation r: 4 4 4 5 5 5 7 ie Annex A - Surface preparation recommendations 11 Annex B - Inspection of the absorbing ability by anthraquinone 13 violet drop tes
8、t Annex C - Inspection of corrosion resistance by repeated 14 immersion test in salt solution - - . .,y, Page 3 EN 2101:1991 This European Standard has been prepared by the European Association of Aerospace Manufacturers ( AEC MA) e 6- After inquiries and votes carried out in accordance with the rul
9、es of this Association, this Standard has successively received the approval of the National Associations and the Official Services of the member countries of AECMA, prior to its presentation to GEN. According to the Common CEN/CENELEC Rules, the following countries are bound to implement this Europ
10、eanStandacd: Austria, BelGun, Damark, Finland, France, Gemmy, c;reece, ce land, rel land, Italy, Luxerg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and Mted Kingdan. - CEN EN*2101 92 3909589 0035330 3 ml Page 4 EN 2101:1991 I 1 Scope and field of application This standard specifies th
11、e required characteristics for the performance of chromic acid anodizing with or without sealing as well as quality assurance of the coating obtained. It applies to parts in aluminium and wrought aluminium alloys of category 1 and 2 (see clause 4) used in aerospace construction when reference is mad
12、e to this standard. . 2 Purpose of anodizing 2.1 Type A : Unsealed anodizing It is used either as a surface preparation before paint application or as a preparation to a macrographic examination (structural condition, presence of metallurgical defects). 2.2 It is intended for corrosion protection. I
13、t shall be with or without colouring and used with or without additional painting. i . Type B : Sealed anodizing 3 References IS0 1463-1 982 IS0 2085-1 976 IS0 2106-1 982 IS0 21 43-1 981 IS0 2360-1 982 IS0 2376-1 972 IS0 3768-1 976 EN 2334 Metallic and oxide coatings - Measurement of coating thickne
14、ss - Microscopical method Anodizing of aluminium and its alloys - Check of continuity of thin anodic oxide coatings - Copper sulphate test Anodizing of aluminium and its alloys - Determination of mass per unit area (surface density) of anodic oxide coatings - Gravimetric method Anodizing of aluminiu
15、m and its alloys - Estimation of loss of absorptivepower of anodic oxide coatings after sealing - Dye spot test with prior acid treatment - Non-conductive coatings on non-magnetic basis metals - Measurement of coating thickness - Eddy current method Anodization (anodic oxidation) of aluminium and it
16、s alloys - Insulation check by measurement of breakdown potential .- Metallic coatings - Neutral salt spray test (NSS test) Aerospace series - Acid chromate pickle for aluminium alloys 1). _ - - 1) In preparation at the date of publication of this standard. _ _. . . . . - 4 Material categories 4.1 C
17、ategory 1 Pure aluminium, clad alloys, alloys characterised by the absence of copper or with a copper content limited to 1 %. r?. 4.2 Categoly2 Non-clad alloys containing 1 % copper : _ - - - . . - Category 2 A : solution heat treated, quenched and naturally aged condition - Category 2 B : solution
18、heat treated, quenched plus artificially aged condition. 5 Supporting jig The supporting jig (e.g. in aluminium alloy or titanium) shall provide effective electrical contact with the parts, This contact is preferably achieved at several points to ensure better current distribution. . 6 Processing se
19、quence 6.1 Cleaning (see annex A) The cleaning methodused shall be appropriate for the contamination experienced on the materials treated. Solvent degreasing followed by cleaning in an alkaline bath is generally the most effective method. 6.2 Pickling (see annex A) The pickling operation shall remov
20、e natural oxides in order to obtain correct anodizing; it shall neither dearade the metallurgical properties of the material nor the material fatigue behaviour, nor initiate pitting. - It shall not degrade the dimensional tolerances and surface roughness specified. As a general rule, pickling is con
21、ducted in a sulphuric-chromic acid bath, but in exceptional cases, for certain alloys of category 2, alkaline pickling may be used. I. CEN EN*ZI,OI, m 4015 001,5332 5 mI Page 6 EN 2101:1991 - Chlorides : 200 mg/l expressed as NaCI, - Sulphates : 500 mg/l expressed as H2SO4. I The chromic acid anodiz
22、ing bath shall be made up with deionized water of a resistivity of more than 105 n.cm unless sufficiently pure ordinary water is available. 6,3 Rinsing All rinsing operations before anodizing shall be effective and complete. For example, they may be performed by immersion followed by running water s
23、pray. It is recommended that rinsing in ordinary water is followed by rinsing in deionized or distilled water. I 6.4 Anodizing + The control system shall make it possible to maintain the treatment temperature within a tolerance of f 2 OC in a suitably agitated bath. 6.4.1 Electrolyte Aqueous solutio
24、n of chromic acid(99,5 % min, Cros) at a concentration of 30 g/l to 150 g/l to which certain additional agents such as oxalic acid may be added. 6.4.2 Treatment conditions The anodizing parameters (temperature, voltage, time) shall be adapted to the material and its category in accordance with the b
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