NAVY MIL-M-81288-1966 MOUNTING BASES FLEXIBLE PLASTIC FOAM《柔软的塑料泡沫安装基地》.pdf
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1、MILITARY SPECIFICATION MOUNTING BASES, FLEXIBLE PLASTICFOAM This specification has been approved by the Bureau of Naval Weapons, Department of the Navy 1. SCOPE 1.1 Scope - This specification covers the design and performance of mounting bases using flexible plastic foam to absorb shock and vibratio
2、n energy. 2. APPLICABLE DOCUMENTS 2.1 General - The documents listed in 6.5 of the issue in effect on the date of invitation for bids form a part of this specification to the extent specified herein. 3. REQUIREMENTS 3.1 Preproduction - This specification makes provision for preproduction testing. 3.
3、2 Materials - In the selection of materials, fulfillment of major design and performance objectives shall be the prime consideration. 3.2.1 Plastic Foam - The plastic foam used for the resilient medium for shock and vibration energy absorption shall be in accordance with MIL-F-8133L See 6.0. 3.2.2 C
4、orrosion Resistance - All metals shall be of corrosion-resistant types or shall be processed to resist corrosion and be entirely adequate for the intended purpose. 3.2.3 Dissimilar Metals - Protection of dissimilar metal combinations shall be in accordance with MIL-STD-454, Requirement 16. 3.2.4 Fin
5、ishes - Parts fabricated from aluminum alloys 3003, 5052, 6053, 6061, 6063, or 7072 shall be cleaned with a deoxidizing solution other than Caustic dip and may be used with or without other surface treatment. Other alloys shall be anodized in accordance with MIL-A- 8625. - I FSC-5340 4 Provided by I
6、HSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-= MIL-M- 81288 (WP) 3.2.5 Adhesives - The adhesive used to secure the foam shall be Goodyear Aircraft Company, Pliobond #30 or approved equivalent. Preparation of the surfaces and the bonding procedure recommended b
7、y the adhesive manufacturer shall be followed. 3.3 Design and Construction - The mounting base shall conform with all the requirements for design, construction and workman- ship, specified herein. 3.3.1 Total Weight - The total weight of the mounting base shall be the minimum required to pass the te
8、sts specified herein consistent with good design. 3.3.2 Mechanical Interference - The design must minimize projections of the equipment and rack below the top surface of the foam. See 3.4.1.3(2). 3.3.3 Safety Wiring - Safety wiring, passing through holes provided for the purpose in the thumb nuts or
9、 wing nuts of the fastener assembly and in the mounting base, shall be used to prevent loosening thereof under vibration. Safety wiring may be eliminated if suitable automatic locking devices are used. proven adequate to the satisfaction of the U. S. Naval Air Development Center (NAVAIRDEVCEN) . Suc
10、h devices, if used, must be - 3.3.4 Bonding Jumpers - Bonding jumpers shall be provided for an electrical conducting path around the plastic foam isolation element and other mating parts. The bonding jumpers shall be braided beryllium copper, or phosphor-bronze silver-plated, or cadmium-plated metal
11、 strip having a width-to-length ratio of not less than 1 to 5. A minimum of two bonding jumpers, preferably located externally at diagonally opposite corners of the mounting base, shall be provided. Bonding jumpers shall be of such length and resilience so as not to have any effect on the natural re
12、sonance of the mounting system. 3.3.5 Distribution of Load - The total load (including cables and connectors) shall be uniformly distributed over the entire foam pad. Compression of foam shall be no more than 10% of its free height. by the desired natural frequency and satisfactory shock isolation,
13、but in no instance shall it be less than 0.1 lb. per square inch nor greater than 0.5 lb. per square inch. Applied weight per square inch of foam shall be determined Foam - The foam shall be applied to the metal sur- - 3.3.6 -faces of the mounting base in a manner such that bulging or shrinking The
14、outer edge of the foam shall not be closer than does not result. 2 . r. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-M-81288 53 7793306 OLL0127 2 MIL-M- 81288(WP) 1/16 inch from the radii of all curved surfaces such as the top and bottom plate
15、. All external surfaces of the foam shall be smooth and continuous. 3.3.6.1 Sealing - All outer surfaces of the foam shall not be coated or sealed in any way. 3.3.7 Motion Limiting Devices - Motion limiting devices shall not be used. 3.4 Performance - 3.4.1 Static Parameters - 3.4.1.1 Loaded Height
16、- When the mounted unit is examined as specified in paragraph 4.5.2.1, the maximum loaded height shall be 1.563 inches. The total load (including connectors and cables) shall be uniformly distributed over the entire foam pad in such a manner that the mounted unit is parallel to its mounting surface
17、11/16 inch. 3.4.1.2 Electrical Bonding - When measured as specified in paragraph 4.5.2.2, the d-c resistance shall not exceed six milliohms. 3.4.1.3 Sway Space - When tested as specified in paragraph 4.5.2.3, the mounted unit shall meet the following requirements: (1) No part of the equipment or moc
18、k-up shall move from its normal position by more than the amount shown on Figure 1. (2) There shall be no contact between non-resilient members. (3) There shall be no failure of, or damage to, the mounting base. 3.4.2 Dynamic Parameters - 3 .f: .2.1 Vibration - (see paragraph 4.5.3.1). 3.4.2.1.1 Iso
19、lation Efficiency - When the mounted unit is tested as specified in paragraph 4.5.3.1.1, the transmissibility along each axis shall not exceed that shown on Figure 2. 3.4.2.1.2 Fatigue - When the mounted unit is tested as specified in paragraph 4.5.3.1.2, there shall be no evidence of mounting base
20、Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-damage, nor shall there be repetitive bouncing between mounting base members normally not in contact. Transmissibility at resonance shall not exceed five. 3.4.2.1.3 Isolation Efficiency After Fatigue (S
21、ee Paragraph 4.5.3.1.3) - The requirements of paragraph 3.4.2.1.1 shall apply. MIL-M-81288 53 W 7779706 OLL0130 7 W 3.4.2.2 - Shock - (See Paragraph 4.5.3.2). 3.4.2.2.1 Service Shock - When the-mounted unit is tested as specified in paragraph 4.5.3.2.1, there shall be no tearing of foam, evidence of
22、 adhesive failure, bending or distortion. 3.4.2.2.2 Shock Transmissibility - When the mounted unit is tested as specified in paragraph 4.5.3.2.2, the shock transmissibility shall not exceed 90 per cent. 3.4.2.2.3 Crash Safety - When the mounted unit is tested as specified in paragraph 4.5.3.2.3, tea
23、ring of the foam and distortion of the sheet metal shall be permitted, but the mockup must remain captive. 3.4.2.2.4 Integrity - When the mounted unit is tested as specified in paragraph 4.5.3.2.4, tearing of the foam and distortion of the sheet metal shall be permitted. However, the mock-up must re
24、main captive, and there shall be no evidence that the adhesive is failing. 3.5 Standard Conditions - The following conditions shall be used to establish normal performance characteristics under standard conditions and for making laboratory tests: Temperature Alt it ude Vibration Humid it y Room Ambi
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