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Document Title |
JPS59216717A |
PURPOSE: To make it possible to control the temperature of a passenger's compartment to a suitable temperature in accordance with the opinion of the minority and as well the number of passengers, by providing such an arrangement that the...
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JPS59216720A |
PURPOSE: To aim at carrying out suitable temperature control in such a casethat the desiring of passengers cannot be exhibited, by determining a desired control temperature in accordance with the desired compartment temperatures of passe...
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JPS5941437B2 |
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JPS5941438B2 |
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JPS59101139U |
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JPS5960100U |
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JPS58500393A |
A life support system is provided for users located within enclosed areas to supply them with fresh air from a location exterior of the enclosed area, and is particularly adapted for use in emergency circumstances such as when fire and s...
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JPS5831236A |
PURPOSE: To decrease the quantity of cooling air to be taken in, and to economize combustion by disposing heat pipes into an introducing pipe to the primary heat exchanger of high-pressure high-temperature air extracted from an engine an...
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JPS5756661B2 |
An air cycle air conditioning system has an air expansion turbine arranged to deliver air through an outlet formed by a wall having an outer surface that defines in part passage means through which supply air flows to the turbine. Heat f...
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JPS5789089U |
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JPS5758598A |
The unit comprises a prime mover 4 (auxiliary engine), a variable geometry compressor 22, and controlled emission turbine 24 which is shaft-coupled to the compressor and cooperating with the compressor to form an environmental control un...
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JPS5649620B2 |
A highly efficient novel catalyst composition for ozone removal is made from (a) metallic silver deposited on a relatively high surface area copper substrate and (b) a composite of a relatively high surface area zirconia and oxides of ma...
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JPS5645768Y2 |
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JPS56501439A |
A cartridge for a catalytic ozone converter comprising an aluminum honeycomb core, a tubular metal shell surrounding the core and affixed thereto, metal rib support members fastened to the shell and to the honeycomb core, and a catalytic...
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JPS56501398A |
Method for controlling humidity levels of internal ambient air for aircraft, utilizing air water separation devices for dehumidification strategically located so as to dehumidify ambient air prior to exhausting the air overboard from the...
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JPS56116600A |
This invention relates to an airconditioning system to provide environmental control for an aircraft's cabin or cockpit. The system cooling cycle includes in combination: a rotary power supply and a turbomachine which includes a power co...
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JPS565697Y2 |
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JPS5559100A |
Respirable gas for the cabins of aircraft with an oxygen concentration depending on the flight altitude is produced from compressed air by a controlled adsorptive removal of nitrogen. Alternating cycles change from an adsorption phase wh...
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JPS5486200A |
A system to pressurise the cabins of aircraft for high-altitude flights includes the circuit with a section through which all the air must pass. This section has a porous structure and presents a large surface area. The latter is coated ...
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JPS5474500U |
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JPS5465167A |
The concentration of ozone in air present in or fed to a confined space (e.g. the passenger space of an aircraft) is reduced by monitoring the concentration of ozone in the space or in a line through which air is fed thereto and feeding ...
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JPS5451200A |
PURPOSE: To prevent wrong operation due to the temperature rise of heating machine on a flying body, by injecting a coolant into a container containing the heating machine and by installing a valve which is opned when the pressure in the...
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JPS5419078A |
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JPS5418599A |
A plurality of aspirating ejector nozzles are fed with primary fluid which is admitted successively past a modulating valve and throttling orifice to the inlet ports of the nozzles with a portion of the primary fluid being arranged for b...
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JPS5417297A |
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JPS5417298A |
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JPS549899A |
An aircraft cabin pressure control system regulates cabin pressure as a function of outside ambient pressure in accordance with the equation WHERE K1, K2 and K3 are constants, Pa is atmospheric pressure, and Pc is the desired value of re...
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JPS5320107Y2 |
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JPS5360300U |
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JPS52130833U |
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JPS5151014A |
A lightweight, high-strength duct comprised of two thin annular tubes, one fitted within the other, the outer tube having spaced annular stiffening beads extending radially outwardly therefrom, and one of the tubes being vented to preven...
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JPS5041680Y1 |
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JPS5011097B1 |
1,217,196. Flying suits pressure control. VAPOR CORP. 26 July, 1968 [29 Nov., 1967], No. 35808/68. Heading B7U. [Also in Division F2] In a pressure regulator, which in use is designed to. pressurize the suits of aircraft personnel, contr...
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JPS5012157Y1 |
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JPS4980887A |
An oxygen regulator wherein oxygen under pressure passes into a mixing chamber through a first inlet port and a first valve, controlled by a first pressure differential, and ambient air passes into the mixing chamber through a second inl...
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JPS4872900A |
An apparatus for maintaining electronic equipment in an airplane below a certain temperature. The apparatus comprises an elongate cylindrical container with pointed end sections removably mounted on the container. A tank is located along...
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JPS4848366A |
1376448 Purifying air BENDIX CORP 2 Nov 1971 [2 Nov 1970] 50922/71 Heading C1A [Also in Division F4] An air conditioning system for an aircraft comprises a filter A for removing solid and liquid particles, a filter B containing activated...
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JPS4818797B1 |
1,128,936. Pressurizing aircraft. UNITED AIRCRAFT CORP. 26 June, 1967 [11 July, 1966], No. 29415/67. Heading F4V. [Also in Division G1] The air pressure inside an aircraft cabin is automatically regulated by an electric control system fe...
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JPS4113227Y1 |
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