NAVY MIL-P-81958-1974 PRESSURE RELIEF DEVICES OVERPRESSURIZATION PREVENTION WHEEL TIRE AIRCRAFT《飞机车轮 轮胎防超压的降压装置》.pdf
《NAVY MIL-P-81958-1974 PRESSURE RELIEF DEVICES OVERPRESSURIZATION PREVENTION WHEEL TIRE AIRCRAFT《飞机车轮 轮胎防超压的降压装置》.pdf》由会员分享,可在线阅读,更多相关《NAVY MIL-P-81958-1974 PRESSURE RELIEF DEVICES OVERPRESSURIZATION PREVENTION WHEEL TIRE AIRCRAFT《飞机车轮 轮胎防超压的降压装置》.pdf(15页珍藏版)》请在麦多课文档分享上搜索。
1、7 MIL-P-81958 I6 W 9999906 0205307 9 W Type I II III rv V MIL-PA1958 (AS) 16 January 1974 Tire Working Pressure Range (Pew 80-129 130-199 200-284 285-399 400-579 MILITARY SPECIFICATION PRESSURE RELIEF DEVICES, OVERPRESSURIZATION PREVENTION, WHEEL/TIRE, AIRCRAFT This specification has been approved b
2、y the Naval Air Systems Command, Department of the Navy. 1. SCOPE 1.1 Scope - This specification covers the requirements for an overprersuurization relief device to replace standard Inflation valves for air- craft pneumatic tribeless wheel/tires. 1.2 Classification 2.1 Government documents normally
3、furnished - The following douuments of the issue in effect on date of invftatfon for bids or request for proposal, form a part of the specification to the extent specified herein. SPE CTFICATIONS Federal QQ-P-416 Plating, Cadmium (Ele c trodepos f tea) PPP-B-566 Boxes, Folding, Paperboard PPP-B-636
4、Box, fiberboard pTiG-1 , THIS DOCUMENT CONTAINS I PAGES. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-. MIL-P-81758 Lb 77777Ob 0205308 b .3 SPECIFICATIONS Mili- MIL-P-116 MIL-S-8 879 Preservation, Methods of Screw Threads, Controlled Radius Root w
5、ith Increased Minor Diameter, General Specification for STANDARDS MiIitarp MIL-STD-129 Markfng for Shipment and Storage MIL-STD-143 Specifications and Standards, Order of Precedence for the Selection of MIL-STD-810 Environmental Test Methods MIL-STD-8 8 9 Dissimilar MetalB Mi333649 Bosse8, Fluid Con
6、nection-Internal Straight Thread (Copies of specifications, standards, drawtngs, and publications required by suppliera In connection with specific procurement functions should be obtained from the procuring activity or as directed by the contractfng officer. ) 3, REQUIREMENTS 3.1 Qualification - Th
7、e pressure relief devices furnished under this specification shall be products which are qualified for listing on the appli- cable qualified products list, at the time set for opening of the bids (See 4.3.1 and 6.3). 3.1.1 Retention of qualification - To maintain status on a Qualified Products List,
8、 oertlfication shall be submitted at two year intervals to indicate continued compliance with the requirements of this specifiaation (See 4.3.2 and 6.3). 3.2 Selection of speciffcations and standards - Specifications and standards for necessary commodities and services not specified herein shall be
9、selected in accordance with MIL-STD-143. 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-P-81958 (AS) 3.3 Materials - Materials shail conform to the applicable specffi- cations. Materials for which there are no applicable specifications, or whi
10、ch are not specifically described herein, shall be of the best quality, of the lightest practical weight and suitable for the purposes intended. Materials used shall be compatible with titanium, magnesium, aluminum, steel, and plastic wheel ma- teriais. 3.3.1 Dissimilar metals - Unless suitably prot
11、eoted against electro- lytic corrosion, disaimilar metals, as defined in MIL-STD-889 shall not be used in intimate contact with each other. 3.3.2 Phtfntr - Ail ateel except corrosion resisting steel shall be cadmiam plated in accordance with Type II, Class 2 plating of QQ-P-416. 3. 3.3 Age - Elastom
12、er components, except silicone, shall not be more than 12 months old from the cure date of manufacture to the date of deliv- ery to Government procuring activity. 3.3.4 Fungus-proof materials - Materials which are not nutrients for fungi shall be used to the greatest extent practicable. External mat
13、erials which are nutriente for fungi shall be treated with a fungicidal agent approved by the procuring activity (see 4. 6.14). 3.4 Design and construction 3.4.1 General - The devices shall be designed to function 80 86 to preclude the possibility of pressurizing an aircraft tubelesis wheel/tire bey
14、ond the specified pressure limits for the applicable tire type when using an inflation source to 5000 psig. The devices shall not permit the pressure contained in the wheevtire to exceed the rated relief pressure (see 3.4.3) at operattng tem- peratures and shall reseat automatically after relief (Se
15、e 3.4.4). They shall be designed so as to prevent the instaliation of a device with an incorrect pressure relief setting. The devices shall maintain tire pressure under aervice uge conditions. 3.4.2 Threads - The pressure relief devices shall be designed to mount on wheel bosses conforming to MS3364
16、9 and have threads in accordance with ML-S-8879 in the sizes and thread designations listed below; 3 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-P-AL758 Ib 7777906 0205310 q m MIGP- 81958 (AS) i Thread Designation I Type I I II III rv V s. 4.
17、8 Relief pressure - The devices shall be designed to relieve at the wheel/tire pressures specified below for the types indicated at operating tem- peratures of from -65F to 350aF. 1 Relief Presmre (psig) l I *15% I II I II N V 200 310 460 640 930 3.4.4 Reseating pressure - Type I devices ehall resea
18、t at 50 psig minimum following relief, Types, II, III, IV, and V shall reseat at 100 psig minimum. 3.4.5 Weight - Unless otherwise specified, the devices shall not exceed. 30 pounds each in weight (See 6.2). %4.6 Length - The devices shall not exceed 1.75 inches in overall length, including inflatio
19、n stem. 3.4.7 Environmental conditions - The device shall meet the perfor- mance requirements of this specification under the following environmental con- ditions when subjected to the tests specified herein, - 3.4.7.1 Temperatures - Design operating and nonoperating tempera- tures range from -65F t
20、o 350F and storage temperatures from -65F to 180F. 3.4.7.2 Ambient pressures - Ambient pressures to be encountered during operation range from 2.13 inches Hg to 31 nches Hg. 4 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,- . . MIL-P-81758 Lb m 9797
21、706 020531iL b m MIL-P-8195 8 (AS 3.4.7.3 Humidity - The device shall not be adversely affected by and shall hotion properly while being exposed to 95 percent rehtive humidity, including uonditions wherein condensation takes place in the form of water, fro a. Qualification inspection (See 4.3) b. Qu
22、ality conformance inspection (See 4.4) 4.3 Qualification inspection - Qualification inspection shall consist of all the examinations and tests of this specification conducted in the order listed under 4 6 and Table I. TABLE I Qualification and Quality Conformance Requirements, Tests, and Testing Seq
23、uence Examination inspec tion of Product Examination of Prep- erationfor Delivery Operation Pressure Cycling Impuleie Cy cling Relief Cycling Requirement 3.4 sect, 5 3.4.1 - 3.4 s. 4 Test Procedure 4.6.1 4.6.2 4. 6.3 4. 6.4. 1 4. 6.4.2 6 aualification X X X - X X 2ualitv Conformance Individual X X -
24、 Sampling X X X - X X Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-. MIL-P-81958 Lb 7999906 0205333 T MIL-P-81958 (AS) TABLE I (Cont. ) Qualification and Qualtty Conformance Requirements, Tests, and Testing Sequescs Examination Pressure endurance
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