NAVY MIL-C-46563 A-1963 CATAPULT AIRCRAFT EJECTION SEAT M3A1 METAL PARTS ASSEMBLY《航空器座椅弹射器M3A1型金属部件组件》.pdf
《NAVY MIL-C-46563 A-1963 CATAPULT AIRCRAFT EJECTION SEAT M3A1 METAL PARTS ASSEMBLY《航空器座椅弹射器M3A1型金属部件组件》.pdf》由会员分享,可在线阅读,更多相关《NAVY MIL-C-46563 A-1963 CATAPULT AIRCRAFT EJECTION SEAT M3A1 METAL PARTS ASSEMBLY《航空器座椅弹射器M3A1型金属部件组件》.pdf(19页珍藏版)》请在麦多课文档分享上搜索。
1、IMfLC-46563A (MU) 31 JANUARY 1963 SUPERSEDING MIL-C-46563(0rd) 9 AUGUST 1961 MILITARY SPECIFICATION CATAPULT, AIRCRAFT E JECTICON SEAT, M3A1 METAL PARTS ASSEMBLY 1. SCOPE 1.1 This is the applicable detail specifica- tion for Catapult, Aircraft Ejection Seat, M3A1, Metal Parts Assembly. The assembly
2、will ultimately be loaded and used in con- junction with other propellant actuated de- vices in aircrew emergency escape systems. 2. APPLICABLE DOCUMENTS 2.1 The following documents of the issue in effect on date o$ invitation for bids or re- quest for proposal, form a part of the speci- fication to
3、 the extent specified herein. SPECIFICATIONS MILITARY .MILt-A-2550 - Ammunition and Spe- cial Weapons, Gen- eral Specification for. MIL-1-45208 -Inspection Require- ments, General Specification for, STANDARDS MILITARY MIL-STD-105 - Sampling Procedures and Tables for In- spection by Attri- butes. MIL
4、STD-109 - Quality Assurance Terms and Defini- tions. MIL-STD-413 - V is u al Inspecti on Guide for Rubber O-Rings. MIGSTD-639 - Surface Roughness Values Preferred for Army Ordnance Materiel. DRAWINGS MUNITIONS COMMAND F8593636 - Catapult, Aircraft Ejection Seat, M3A1, Metal Parts Assembly. F8797431
5、- Ammunition Contain- er, Fiber M304 or Catapult, Aircraft Ejection Seat, M3A1. - Box, Packing, Ammu- nition for Catapult, Aircraft Ejection Seat, M3A1. F8797432 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-C-46563A MIL-C46563A (MU) IEL-869363
6、6 - Index to Inspection Equipment List for Catapult, Aircraft Ejectionseat, M3A1, Metal Parts Assembly. (Copies of specifications, standards and drawings required by suppliers in connection with specific procurement functions should be obtained from the procuring activity or as directed by the contr
7、acting officer.) 3. REQUIREMENTS 3.1 General. Materials, parts and assem- blies shall comply with the requirements specified on the applicable drawings, ref- erenced specifications and the following : 3.2 Initial production sample. Unless other- wise directed by the contracting officer, an initial p
8、roduction sample shall .be required. 3.3 Material. The contractor shall be re- sponsible for selecting from the classification list contained in the raw material specifica- tion the surface and physical condition of the raw material intended for use in manu- facture. 3.4 Physical properties. Physica
9、l proper- ties required by the drawing shall be uni- form throughout each part within specified tolerances. Requirements for all alloy steel parts shall be achieved by qenching and tempering. 3.5 Hydrostatic pressure. The components listed below shall withstand the correspond- ing internal pressure
10、as indicated in table I for a period of 16 seconds, minimum, with- out application of any external load and shall show no evidence of leakage or mechanical failure (see 6.1). TABLE I Component Hydrostatic preaeure (psi minimum) Outside Tube 2600 Telescoping Tube 3200 Inside Tube 3200 3.6 Shear pin s
11、trength, After application of protective finish, the pin shall shear when a load of 400 plus or minus 50 pounds is applied at the steady rate of 26 inches per minute. 3.7 Structural strength. The metal parts assembly shall be capable of withstanding each test load for 16 seconds, minimum, as indicat
12、ed in table II, The maximum allow- able change between mounting points, result- ing from each load application shall not ex- ceed the values indicated in table II. A pre- load OP 500 pounds shall be utilized prior to each test load application. TABLE II Test loads (including pre-load) min. Change be
13、tween mounting points, I max. 1. 2000 pounds in tension . 2. 2000 pounds in tension . 3. 8000 pounds in compression . .O05 inches .O01 inches .O05 inches ,001 inches 4. 8000 pounds in compression . 3.8 Metal parts assembly. Parts shall be combined to produce an assembly which con- forms to the requi
14、rements of the metal parts assembly drawing and the following: 3.8.1 :Torque. Torque requirements shall be as specified in table III. No loosening or de- formation shall occur upon application of the breakaway torque. Provided by IHSNot for ResaleNo reproduction or networking permitted without licen
15、se from IHS-,-,-MIL-C-46563A 33 m 7777706 0332774 3 m - - MIEC-46563A (MU) TABLE III Component A B Run-on Seating or bottoming (inch pounds) (including A) (inch pounds) Cap and Outside Tube 75 min, 550 + 50 Triinnion and Outside Tube 75 min. 550 + 50 Spacer and Telescoping Tube Block and Inside Tube
16、 75 min. Stop Ring and Trunnion 75 min. 3.8.1.1 Bottoming torque. The bottoming torque between block and inside tube and between stop ring and trunnion shall not ex- ceed the running torque by more than 50 inch pounds. 3.9 Protective finish. Protective finish shall be in accordance with the applicab
17、le specifi- cation and drawings and shall apply to all surfaces of the component regardless of con- tour configuration. 3.10 Residual magnetism. The metal parts assembly shall not deflect the indicator of the compass more than 3 degrees in either direction when passed in front of the com- pass at a
18、distance of 6 inches. 3.11 Workmanship. The requirements for workmanship are as specified on the appli- cable drawings, referenced specifications and the following : 3.11.1 Metal defects. All components shall be free from cracks, splits, cold shuts, inclu- sions, porosity or any similar defect. 3.11
19、.2 Bzc? No part shall have a bur which might interfere with the assembly or func- tion of the item or which might be injurious to personnel handling the item. 3.11.3 Foreign matter. No part or assem- bly shall contain chips, dirt, grease, rust, corrosion or other foreign matter. 4. QUALITY ASSURANCE
20、 PROVISIONS 4.1 The supplier is responsible for the per- 7 Breakaway c (inch pounde) 400 min. 400 min. 200 min. formance of all inspection requirements as specified herein. Except as otherwise speci- fied, the supplier may utilize his own or any other inspection facilities and services acceptable to
21、 the Government. Inspection records of the examination and tests shall be kept complete and available to the Govern- ment as specified in the contract or order. The Government reserves the right to per- form any of the inspections set forth in the specification where such inspections are deemed nece
22、ssary to assure supplies and services conform to prescribed requirements. 4.1.1 Quality assurame terns and defini- tions. Reference shall be made to MIL-STD- 109 to define the quality assurance terms used, 4.1.2 Inspection. Inspection shall be in ac- cordance with MIL-A-2550 and MILI- 45208, except
23、as specified herein. 4.2 Initial production sample. Prior to the initiation of regular production, the contrac- tor shall submit an initial production sample to a Government approved facility or evalu- ation. The ,sample shall consist a 5 metal parts assemblies, 10 sets of unassembled parts and fift
24、y shear pins from the same lot of shear pins tested by the contractor. The samples shall be subjected to the tests in 4.3.3. Test procedures shall ,be in accordance with 4.4, except as provided in MIL-145208. The sample shall .be manufactured in the same manner, using the same materials, equipment,
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