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National Stock Number: 2840-01-311-9987
Federal Supply Class: 2840
National Item Identification Number: 013119987
Description: INSULATION BLANKET,THERMAL,AIRCR
Detail: A FLEXIBLE COVERING, FABRICATED FROM APPROPRIATE INSULATING MATERIALS, DESIGNED TO REDUCE THERMAL RADIATION IN THE HOT SECTION OF AN ENGINE, GAS TURBINE, AIRCRAFT. SEE ALSO SHIELD, HEAT, AIRCRAFT GAS TURBINE ENGINE.
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Manufacturer Information:
1608M64 | 07482 | GENERAL ELECTRIC COMPANY | 1608M64P01 | 07482 | GENERAL ELECTRIC COMPANY | 1608M64P03 | 07482 | GENERAL ELECTRIC COMPANY | 42H30995-3 | 22013 | TIGHITCO INC. | 8-980206-1 | 54787 | THERMAL STRUCTURES, INC | 1608M64P01 | 54787 | THERMAL STRUCTURES, INC |
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Techincal Specification:
CRITICALITY CODE JUSTIFICATION | AGAV | PART NAME ASSIGNED BY CONTROLLING AGENCY | INSULATION BLANKET, RELIEF VALVE | MATERIAL | STEEL CORROSION RESISTING SUPPORT | SPECIAL FEATURES | AFTER CLEANING AND DEGREASING NO SHARP EDGES PERMITTED PRIOR TO APPLICATION OF GE RTV 106 (SILICONE RUBBER); .06-.18" THICK | SUPPLEMENTARY FEATURES | NO AIR FLOW INSIDE OF BLANKET; MEAN TEMPERATURE AT 1300 DEGREES FAHRENHEIT; MAXIMUM DENSITY OF INSULATION SHALL BE 12LBS/FT(3RD POWER);WRINKLES, CREASES AND DENTS ARE PERMITTED PROVIDING THERMAL REQUIREMENTS OF THE INSULATION BLANKET ARE MET; DENTS SHALL NOT DECREASE INSULATION BLANKET THICKNESS BY MORE THAN 50%; LOCALIZED LOSS OF RIGIDIZING OR GROOVING PATTERN IS PERMISSIBLE IN AREAS OF FORMING; ANY TYPE OF RIGIDIZING OR GROOVING PATTERN IS ACCEPTABLE; MAXIMUM CONTINUOUS OPERATION HOTSIDE TEMPERATURE TO BE 2200 DEGREES FAHRENHEIT FOR 15 MINUTE MAXIMUM | SURFACE TREATMENT | SILICON OVERALL | TEMP RATING | 1300.0 FAHRENHEIT |
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