NAVY MIL-C-85614 A-1990 COATING FASTENER (TITANIUM AND CRES ALLOYS) ALUMINUM PIGMENTED ORGANICALLY BONDED (FOR ALL THREADED AND UNTHREADED FASTENERS)《有机物覆盖(有线和无线的紧固件)的铝涂料外壳紧固件(钛和 合.pdf
《NAVY MIL-C-85614 A-1990 COATING FASTENER (TITANIUM AND CRES ALLOYS) ALUMINUM PIGMENTED ORGANICALLY BONDED (FOR ALL THREADED AND UNTHREADED FASTENERS)《有机物覆盖(有线和无线的紧固件)的铝涂料外壳紧固件(钛和 合.pdf》由会员分享,可在线阅读,更多相关《NAVY MIL-C-85614 A-1990 COATING FASTENER (TITANIUM AND CRES ALLOYS) ALUMINUM PIGMENTED ORGANICALLY BONDED (FOR ALL THREADED AND UNTHREADED FASTENERS)《有机物覆盖(有线和无线的紧固件)的铝涂料外壳紧固件(钛和 合.pdf(10页珍藏版)》请在麦多课文档分享上搜索。
1、- - i- . MIL-C-8562LIA HF 7797706 0433372 3 I NOT MEASUREMENT SENSITIVE I MI L-C-856 1 4A 27 February 1990 SUPERSEDING MI L-C-85614(AS) 30 June 1989 MILITARY SPECIFICATION COATING, FASTENER (TITANIUM AND CRES ALLOYS), ALUMINUM PIGMENTED, ORGANICALLY BONDED (FOR ALL THREADED AND UNTHREADED FASTENERS)
2、 This specification is approved for use by all Departments and Agencies of the Department of Defense. 1. SCOPE * 1.1 Scope. This specification covers the acceptance requirements for an aluminum pigmented, organically bonded coating applied at temperatures not greater than 450F to al 1 threaded and u
3、nthreaded fasteners made from titanium and corrosion resi stant steel alloys. 2, APPLICABLE DOCUMENTS 2.1 Government documents. 2.1.1 Specifications and standards. The following specifications and standards form a part of this document to the extent specified herein. otherwise specified, the issues
4、of these documents are those listed in the issue of the Department of Defense Index of Specifications and Standards (DODISS) and supplement thereto, cited in the sol i ci tation (see 6.2). Unless SPECIFICATIONS FEDERAL QQ-A-22 5 Aluminum Alloy Bar, Rod and Wire QQ-P-416 Plating, Cadmium (Electrodepo
5、sited) MILITARY MIL-A-8625 Anodi c Coati ngs for Al umi num and Al urni num Al loys Benef i c i al comments , ( recomme ndat i ons , add i ti on s , de 1 et i ons 1 and any pert i nen t data which may be of use in improving this document should be addressed to the Naval Air Engineering Center, Syste
6、ms Engineering and Standardization Department (SESD) (Code 531, Lakehurst, NJ 08733-5100, by using the self-addressed Standardization Document Improvement Proposal (DD Form 1426) appearing at the end of this document or by letter. AMSC NIA FSC MFFP DISTRIBUTION STATEMENT A: Approved for public relea
7、se; distribution is unlimited. 0 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-C-85614A flF 9799906 0413373 5 H MIL-C-85614A SPECIFICATIONS (Continued) MI L-S-5000 MIL-S-8879 Steel, Chrome-Ni ckel-Molybdenum (E4340) Bars and Reforging Stock Scr
8、ew Threads, Control 1 ed Radi us Root wi th Increased Minor Diameter, General Specification for MI L-R-81294 Remover, Paint, Epoxy and Polyurethane Systems MI L-H-83306 MI L-L-87 1 32 MI L-T-81533 STANDARDS Hydraulic Fluid, Fire Resistant, Phosphate Ester Base, Ai rcraft Lubricant, Cetyl Alcohol, 1
9、Hexadeconal, Appli- cation to Fasteners Trichloroethane 1,1,1 (Methylchloroform) Inhibited Vapor Degreasing MI LI TARY MI L-STD-6866 Inspection, Penetrant, Method of (Unless otherwise indicated, copies of federal and military specifications, standards, and handbooks are available from the Naval Publ
10、ications and Forms Center, (ATTN: NPODS), 5801 Tabor Avenue, Philadelphia, PA 19120-5099.) * 2.2 Non-Government publications. The following documents form a part of this document to the extent specified herein. Unless otherwise specified, the issues of the documents which are DoD adopted are those l
11、isted in the issue of the DoDISS cited in the solicitation. Unless otherwise specified, the issues of documents not listed in the DODISS are the issues of the documents cited in the solicitation (see 6.2). AMERICAN SOCIETY FOR TESTING AND MATERIALS (ASTM) ASTM B 287 Acetic Acid, Spray (FOG) Testing
12、ASTM D 740 Methyl Ethyl Ketone (Application for copies should be addressed to the American Society for Testing and Materials, 1916 Race Street, Philadelphia, PA 19103-1187.) 2.3 Order of precedence. In the event of a conflict between the text of this document and the references cited herein, the tex
13、t f this document takes precedence. Nothi ng in thi s document, however, supersedes appl i cable 1 aws and regulations unless a specific exemption has been obtained. 3. REQUIREMENTS subjected to first article Inspection in accordance with 4.3 - .3.1 First article. When specifled (see 6.21, a sample
14、shall be 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,- MIL-C-85bL4A MF W 9977906 0433374.7 m MI L-C-85614A 3.2 Materials. The materials used shall be such as to produce organically bonded aluminum coatings which conform to this specification. 3.
15、3 Equipment and processes. The equipment and processes shall be caDable of wovidinq a uniform coating in accordance with the requirements of thi s speci fi cat ion. - 3.3.1 Cleaning. Before coating, fasteners shall have clean surfaces with no evidence of erosion, pitting or intergranular attack. 3.3
16、.1.1 Coating process. The coating may be applied directly to the fastener surface, or the fastener may have a chemical conversion or mechanical pretreatment. function. below the minimum tempering temperature of the fastener, and shall not be greater than 425F. Pretreatment shall not be deleterious t
17、o the fastener or its The cure temperature of the coating shall be not greater than 50F 3.4 Appearance. The coating shall be smooth and of uniform thickness and color. It shall be free of pin holes, porosity, blisters, nodules, pits or other harmful imperfections. the thread surfaces, and under the
18、head. * 3.6 Thickness. The coating thickness shall be 0.0002 to 0.0005 inches (see 4.5.1). Coating is not required inside lightening holes in the head or point end, inside wrenching features, inside lockwire holes, or on breakaway devices (lock bolt pull stems, etc.). 3.5 Areas of deposit. As a mini
19、mum, the coating shall cover the shank, 3.7 Adhesion. After being subjected to the test specified in 4.5.2, the coating shall be continuously bonded to the fastener and shall not display loss of adhesion or separation from the fastener when examined at a magni f i cation of 4X. 3.8 Fluid resistance.
20、 The coating shall be immersed in hydraulic fluid conforming to MIL-H-83306 for 30 days (720 hours). The coating shall show no evidence of blistering or loss of adhesion. Coating shall be not less than 4H pencil hardness prior to immersion and not less than 2H pencil hardness subsequent to immersion
21、 (see 4.5.3). 3.9 Paint remover resistance. The coated fasteners shall show no evidence of blistering or loss of adhesion when subjected to the paint remover test (see 4.5.4). 3.10 Embrittlement. Coated titanium fasteners shall display no evidence of cracking in the head-to-shank fillet or thread ar
22、eas (see 4.5.5 and table II). 3.10.1 Embrittlement test block. The test block used for the embrittlement test (see 4.5.5) shall be a 7075-T6 aluminum alloy block (UNS A970751 in accordance with QQ-A-225/9. The block thickness shall be compatible with the grip lengths of the four coated fasteners use
23、d in the test. 3.11 Corrosion protective properties of coatings. The applied coating on the countersink areas and surface areas of the 2024 aluminum alloy (UNS 3 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-C-85614A MF 7797906 0433375 7 MI L-C
24、-856 14A A920241 blocks surrounding the coated fasteners shall display no more corrosion than the corresponding areas with the cadmium plated fastener control blocks (see 4.5.6). or blistering when tested in accordance with 4.5.7. After heating, the coating shall be tested in accordance with 4.5.2 a
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