NAVY MIL-S-85334-1980 SEALING COMPOUND NONCURING LOW CONSISTENCY SILICONE GROOVE INJECTION FOR INTEGRAL FUEL TANKS《积分油缸槽注入有机硅低一致性不可恢复密封胶》.pdf
《NAVY MIL-S-85334-1980 SEALING COMPOUND NONCURING LOW CONSISTENCY SILICONE GROOVE INJECTION FOR INTEGRAL FUEL TANKS《积分油缸槽注入有机硅低一致性不可恢复密封胶》.pdf》由会员分享,可在线阅读,更多相关《NAVY MIL-S-85334-1980 SEALING COMPOUND NONCURING LOW CONSISTENCY SILICONE GROOVE INJECTION FOR INTEGRAL FUEL TANKS《积分油缸槽注入有机硅低一致性不可恢复密封胶》.pdf(31页珍藏版)》请在麦多课文档分享上搜索。
1、MIL-S-5334 0 W 7777706 0333777 T W MIL-S-85334 (AS) 21 May 1980 MILITARY SPECIFICATION SEALING COMPOUND, NONCURING, LOW CONSISTENCY, SILICONE, GROOVE INJECTION, FOR INTEGRAL FUEL TANKS This spec2fication is approved for use by the Naval Air Systems Command, Department of the Navy and is available fo
2、r use by all Departments and Agencies of the Department of Defense. 1. SCOPE 1.1 Scope. This specification establishes the requirements for one type of inert, permanently mastic silicone type sealing compound modified with a flow control additive, or sealing or resealing integral fuel tanks on milit
3、ary aircraft. 2. APPLICABLE DOCUMENTS 2.1 Issues of documents. The following documents of the issue in effect on date of invitation or bids or request for proposal from a part of this specification to the extent specified herein. SPECIFICATIONS FEDERAL L-P-378 -Plastic Sheet and Strip, Thin gauge, P
4、olyolefin QQ-A-250/4 -Aluminum Alloy 2024, Plate and Sheet QQ-A-250/ 12 -Aluminum Alloy 7075, Plate and Sheet TT-E- 75 1 -Ethyl Acetate, Technical Beneficial comments (recommendations, additions, deletions) and any pertinent data which may be of use in improving this document should be addressed to:
5、 Engineering Specifications and Standards Department (Code 9321), Naval Air Engineering Center, Lakehurst, NJ 08733, by using the self-addressed Standardization Document Improvement Proposal (DD Form 1426) appearing at the end of this document or by letter. FSC 8030 Provided by IHSNot for ResaleNo r
6、eproduction or networking permitted without license from IHS-,-,-FEDERAL (Continued) TT-1-735 TT-M-261 TT-N-9 7 TT-S-735 TT-T-548 PPP-B-566 PPP-B-636 PPP- C- 9 6 MILITARY MIL-6-5541 MIL-T-5624 MIL-S-6758 MIL-P-7105 MIL-S-7720 MIL-5-7742 / MIL-P-19468 MIL- C- 27 7 25 MIL-P-387 14 MIL-C-81706 2 ,y*; M
7、IL- C - 8 7 9 6 2 -Isopropyl Alcohol 1 -Methyl-Ethyl-Ketone, Technical -Naphtha, Aromatic -Standard Test Fluids, Hydrocarbon -Toluene; Technical -Box, Folding, Paperboard -Box, Shipping, Fiberboard -Cans, Metal, 28 Gauge and Lighter -Chemical Conversion Coatings on Aluminum and Aluminum Alloys -Turb
8、ine Fuel, Aviation, Grades JP-4 and JP-5 -Steel, Chrome - Molybdenum (4130) Bars and Reforging Stock (Aircraft Quality) -Pipe Threads, Taper, Aeronautical National Form, Symbol ANPT, General Requirements for -Steel, Corrosion Resistant (18-8) Bars, Wire and Forging Stock (Aircraft Quality) -Screw Th
9、reads, Standard, Optimum Selected Series, General Specification for -Plastic Rod Polytetrafluoroethylene, Molded and Extruded “Coating, Corrosion Preventive, For Aircraft Integral Fuel Tanks -Packaging and Packing of Two-Component Materials in Semkits -Chemical Conversion Materials for Coating . Alu
10、minum and Aluminum Alloys - -Cloths, Cleaning, for Aircraft Fuel Tanks rl Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-STANDARDS FEDERAL FED-STD-791 -Lubricants, Liquid Fuels and Related Products, Methods of Testing MILITARY MIL-STD-105 -Sampling
11、Procedures and Tables for Inspection by Attributes MIL-STD-129 -Marking for Shipment and Storage (Copies of specifications, standards, drawings and publications required by contractors in connection with specific procurement func- tions should be obtained from the procuring activity or as directed b
12、y the contracting officer.) 2.2 Other publications. The following documents form a part of this specification to the extent specified herein. Unless otherwise indicated, the issue in effect on date of invitation for bids or request for proposal shall apply. AMERICAN SOCIETY FOR TESTING AND MATERIALS
13、 (ASTM) ASTM A108-73 -Steel Bars, Carbon, Cold-Rolled Strip ASTM D471-77 -Rubber, Property - Effect of Liquids (Applications for copies should be addressed to the American Society for Testing and Materials, 1916 Race Street, Philadelphia, PA 19103 .) CONSOLIDATED CLASSIFICATION COMMITTEE Uniform Fre
14、ight Classification Rulesd (Application for copies should be addressed to the Consolidated Classification Committee, 202 Chicago Union Station, Chicago, IL 60606.) (Technical society and technical association specifications and standards are generally available for reference from libraries. They are
15、 also distributed among technical groups and using Federal agencies.) 3. REQUIREMENTS 3.1 Qualification. The integral. fuel tank sealing compounds furnished under this specification shall be products which are qualified for listing on the applicable qualified products list at the time set or opening
16、 of bids (see 4.3 and 6.3). 3 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-3.5 MIL-S-85334 80 M 7779706 OLL1783 L M MIL-S-85334 (AS) 3.5.1 ompressive
17、 1 in 4.6.2.1. 3.5.2 Performance properties. Extrusion force. The compound shall extrude under a d of 150 to 300 pounds (65 to 135 Kg) when tested as specified Low temperature flexibility. When tested as speci- fied in 4.6.2.2, the compound shall not crack, harden or exhibit loss of adhesion. 3.5.3
18、there shal specified 3.5.4 prepared a below: Seal efficiency. When tested as specified in 4.6.2.3, be no leakage through the faying surface in excess of that in 4.6.2.3.4.1. The compound shall remain reinjectable. Injection and reinjection properties. Specimens d tested in 4.6.2.4 shall comply with
19、the requirements listed (To) Original injection time, seconds, max. - 35 - as determined - 50 to 200% of T1 (T1) Original reinjection time, seconds, max. (T ) Reinjection time after fuel/heat exposures Volume of sealant, port +/I, after - 0.5 cc minimum reinjection . 3.5.5 Large gap retention. Speci
20、mens prepared and tested as specified in 4.6.2.5 shall exhibit no sealant flow beyond the faying edge of the fixture. 3.5.6 Resistance to pressure rupture. The sealing compound when tested as specified in 4.6.2.6 shall exhibit minimum average pressure rupture as follows: Condition Control After fuel
21、 At elevated temperature 7lo1tl0C ( 1601t20F) Requirement psi .(kPa) 5.9 1.7 1.7 (40.6) 12 inches (305 mm) of Hg (11.7) 3.5 inches (90 mm) of Hg (11.7) 3.5 inches (90 mm) of Hg 3.5.7 Cold flow. The c-ange ,n height of the sealant column shall not exceed 30 percent when tested as specified in 4.6.2.7
22、. 3.6 Workmanship. The sealing compound furnished under this specification shall be formulated from highest quality components described herein to meet all the requirments of this specification. 5 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-I I 4
23、. QUALITY ASSURANCE PROVISIONS E 4.1 Responsiblity for inspection. Unless otherwise specified in the contract, the contractor is responsible for the per- formance of all inspection requirements as specified herein. Except as otherwise specified in the contract, the contractor may use his own or any
24、other facilities suitable for the performance of inspection require- ments specified herein, unless disapproved by the Government. The Government reserves the right to perform any of the inspections set forth in the specification where such inspections are deemed necessary to assure supplies and ser
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