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JPS54126400A |
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JPS5429915B2 |
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JPS5411598B1 |
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JPS5411599B1 |
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JPS541599A |
The control system for aircraft de-icing equipment is for systems using separately switched electrically heated mats (A, B, C). Each of these has a solenoid operated switch (15, 16, 18) and is fed from the aircraft's 3-phase AC system vi...
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JPS53114199A |
PURPOSE: To provide protecting functions of respective parts of an aircraft by mounting means for stopping the operation of inverter means for supplying an electric power to the heater of a windshield glass when malfunction occurs.
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JPS5330235B2 |
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JPS5328719B1 |
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JPS5326245B2 |
The inlet spinner of a gas turbine engine is de-iced by directing a stream of heated lubricant from the lubrication system of a gas turbine engine against a generally concave heat transfer surface formed on the interior of the inlet spin...
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JPS5320637B1 |
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JPS5350544A |
A positive temperature coefficient (PTC) resistance heater assembly is used in combination with an angle of attack vane to provide automatic means for maintaining the temperature of the vane at a level which will de-ice the vane. The hea...
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JPS5312000Y2 |
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JPS52131749A |
A system for detecting ice on exterior surfaces of aircraft by transmitting a relatively low power microwave electromagnetic signal into a dielectric layer functioning as a surface waveguide, and monitoring the signals transmitted into a...
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JPS52121299A |
A system for effecting the removal of ice from external surfaces of aircraft, and particularly from helicopter rotor blades, by the transmission of microwave electromagnetic energy into the ice so that it functions as a surface waveguide...
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JPS5233722B2 |
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JPS5227520Y2 |
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JPS5220760B1 |
1325488 De-icing boots B F GOODRICH CO 25 Aug 1970 [25 Aug 1969] 40848/70 Heading B7W An inflatable laminated de-icer boot 10 mountable on an aerofoil comprises a series of selectively inflatable and deflatable tubes 12, Fig. 1, and a ma...
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JPS5263781A |
Apparatus for indicating the rate of ice accretion on a surface particularly for use in aircraft comprising a hollow housing divided internally by a resilient diaphragm into first and second chambers. A first conduit communication at one...
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JPS51147900A |
Apparatus for indicating rate of ice accretion particularly for use in an aircraft, the apparatus including test surface on which ice forms in use. First and second gas conduits are supplied with gas from a common pressure regulator the ...
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JPS5182292U |
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JPS5083991A |
1477055 Polyurethane coated ship or aircraft GOODYEAR TIRE & RUBBER CO 11 Oct 1974 [23 Nov 1973] 44188/74 Heading B2E A ship or an aircraft has an anti-icing coating of 10 to 50 mils of a polyurethane prepared from a reaction mixture whi...
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JPS5021280Y1 |
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JPS5014791B1 |
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JPS5063980A |
Ice detection equipment comprises electrical circuit means for effecting a count of a number of electrical pulses means for modifying the count depending upon the rate of production of the pulses.
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JPS5012156Y1 |
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JPS4983198A |
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JPS4920603A |
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JPS4830319B1 |
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JPS4844613A |
A spinner construction for maintaining ice accumulation thereon to an acceptably low level during operation of a gas turbine engine under icing conditions wherein a plurality of spaced fins extend from the arcuate outer surface of the sp...
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JPS4835529A |
Windscreen wiper drive mechanisms, including an electric motor that drives the rotating component of a scottish fork, a rack supported by the linear and reciprocating component of said fork, an output shaft for connection to the windscre...
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JPS44195Y1 |
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JPS4115727Y1 |
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