ARMY MIL-I-8474 C-1983 INSPECTION OF ALUMINUM ALLOY PARTS ANODIZING PROCESS FOR《用于铝合金零件测试的阳极化处理》.pdf
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1、X0 DELIVERAELE DATA REQUIEiEC BY THIS DGCUMNT KC.L-I-8474C 31 August 1983 SUPERSEDING MIL-I-8474B(MR) 26 May 1965 MILITARY SPECIFICATION INSPECTION OF ALUMIKUM ALLCY FARTS, ILNODIZING PFGCESS FCR This specification is approved for use by all fepartnents and Agencies of the Department of Defense 1. S
2、COPE. 1.1 Scope. This specification covers the use of a chromic acid anodizinc; process for surface inspection for cracks, laps and other defects in parts of alutainum alloy compositions for which the process is compatible. 2. WPLICABLE DOCUMENTS 2.1 Gover ment docurtlent s. 2.1.1 Specifications, st
3、andards, and handbooks. Unless otherwise specifiec3, the following specifications, standards, and handbooks of the issue listed in that issue of the Department of Defense Index of Specifications and Standars (DoDISS). specified in the solicitation form a part of this specification to the extent spec
4、ified herein. r Beneficial comments (recommendations, additions, deletions) and any pertinent data uhich may be of use in improving this document should be addressed to: Ijirector, US Army Materials and Mechanics Research Center, ATTN: DRXKR-SMS, Watertown, MA 02172 by using the self-addressed Stand
5、ardization Document Improvement Proposal (DD Form 1426) appearing at the end of this document or by letter. / AREA MFFP / “ “ Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-I-8C74C S PECIFI CAT IONS MIL-A-8625 - Anodic Coatings, for Aluminum and
6、 Aluminum Alloys (Copies of specifications, standards, handbooks, drawings, and publications required by manufacturers in connection with specific acquisition functions should be obtained from the contracting activity or as directed by the contracting officer. 1 2.2 Order of precedence. In the event
7、 of a conflict between the text of this specification and the references cited herein, the text of this specification shall take precedence. 3. REQUIREMENTS 3.1 Material. The materials shall De as specified herein. When materials are used that are not specifically des.ignated, they shall be entirely
8、 suitable for the purpose. 3.2 Anodic film. The anodic film shall confornl to all the requirements for type I coatings of MIL-A-8625 when tested as specified in 4.3, except for the eollowing : 3.2.1 Rinse. After anodizing, parts shall be rinsed in water for the minimum period necessary to remove sur
9、face chromic acid. The tenperature of the rinse shall not .be higher than the temperature of the anodizing solution. . 3.2.2 Drying. Following the rinse, the parts shall be maintained at room temperature for a minimum o 2 hours, or they shall be maintained for a minimum period of 1./2 hour at 2500 i
10、- 250F. In either case the parts shall be racked or stared in such a manner that the ai.r has free access to the surfaces to be inspected. Air circula.tion, not to exceed 50 linear feet per xinute, may be used to aid in drying. 3.3 Air agitation. Air agitation of the bath shall not De used when part
11、s are in the bath. 3.4 Inspection. Inspection of the ancdized parts shall be by visual . examination of the surface for indications of cracks, forging laps or other defects. 3.5 Indications. Voids in the metal which comrzunicate with the outer surface appear as directional stains of chromic acid. De
12、fects which do not contain voids appear as a directional etch on the surface. Insufficient rinsing in cold water produces stains which may be confused with defects. Stains from insufficient rinsing follow drain patterns, whereas stains from. flaws follow the lines of the defects. 2 Provided by IHSNo
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