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JP2004071764 |
To provide an electronic device cooler which is smaller, lighter in weight and has a higher cooling capacity than a conventional product.In the electronic device cooler comprising cooling parts 11, 12 and an electronic device which is co...
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JP2004066923 |
To provide a light air conditioner for an aircraft, having small volume, and capable of reducing power consumption and air resistance of an aircraft body during flight.This air conditioner 10 for the aircraft is provided with an outside ...
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JP2003312595 |
To provide an air conditioner for an aircraft capable of effectively using oxygen enriched air from an air separation part, reducing an engine load, performing a fail-safe function at the time of fixing of a flow control valve of engine ...
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JP2003312596 |
To provide an air conditioner for an aircraft capable of effectively using oxygen enriched air from an air separation part, reducing an engine load, and exerting a sufficient air-conditioning function at the time of descent of the aircra...
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JP2003312594 |
To provide an air conditioner for an aircraft capable of effectively using oxygen enriched air from an air separation part, reducing an engine load, performing a fail-safe function, and allowing a proper operation according to a flight c...
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JP2003300498 |
To provide an air conditioner for an aircraft capable of effectively using not only nitrogen enriched gas but also oxygen concentrated air exhausted from an air separating part, and capable of preventing the expansion of the force of a f...
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JP2003291894 |
To provide an air conditioner for aircraft, which effectively uses not only nitrogen enriched gas but also oxygen concentrated air being exhausted from an air separation part, and prevents ill effects caused by the breakage of the air se...
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JP2003240615 |
To provide a flow sensing venturi device wherein replacement of a sensor is simplified.This flow sensing venturi device 10 includes a venturi body 16 and a manifold 18 mounted thereon. The manifold 18 is thermally isolated from the ventu...
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JP2003240375 |
To make high-pressure air supplied to an air separator and the like on a machine.This air cycle type air conditioner is an air conditioner provided with a an heat-exchanger and an air cycle machine for supplying air-conditioned air from ...
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JP2003231500 |
To provide a reservoir tank provided with a liquid level detector for preventing erroneous detection of a liquid level.The reservoir tank RT is composed by laying a partition plate SP bored with pores H in an interior of a tank T at an i...
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JP2003214187 |
To provide an air bleeding system utilizing the tangential velocity component of the air flowing out from a rear edge of an upstream blade.This air bleeding system used in a gas turbine engine, comprises a plurality of vanes (blades) 10,...
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JP2003207221 |
To provide an environment control system (ECS) for supplying the adjusted air to a closed space.This environment control system 10 comprises one or more liquid circulation sub-systems 14a, 14b and an air circulation (ACM) subsystem 12. T...
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JP2003205899 |
To avoid reduction of effective cabin volume and shorten air conditioning piping by rationally arranging an air conditioner of an airplane.A carry-through 12 integrally connecting spars 11 of left and right main wings WL and WR of the ai...
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JP2003185278 |
To provide an air conditioning system for an airplane which feeds a prescribed amount of air to a cabin even if reducing an engine bleed air flow and lowering a penalty to the engine.A turbine 13 is driven by engine bleeding, the turbine...
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JP2003160098 |
To provide an air conditioner for aircraft which improves comfort by maintaining proper temperature, humidity, and oxygen concentration in a cabin and prevents a fuel fire from occurring without increasing an engine load.Extracted air fr...
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JP3419003 |
PURPOSE: To easily draw around a pressure governed air supply line by effectively utilizing energy provided in bled high temperature high pressure air, and decreasing a temperature of air which passes through the pressure governed air su...
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JP2003097733 |
To increase productivity and reliability of leak property at a closing position by loosening strictness of a design tolerance for a positive breaking type exhaust port for air appropriate, in particular, to an air plane.This positive shu...
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JP2003081194 |
To provide an air-conditioning system for aircraft with suppressing the occurrence of pressure loss and a reduction in the amount of an engine bleed air to be taken into the air-conditioning system and removing dust from the engine bleed...
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JP2003081195 |
To provide an air-conditioner for aircraft with securing the amount and pressure of an air to be introduced into an air separating unit without increasing the load of an engine, contributing to preventing the occurrence of a fuel fire an...
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JP2003042578 |
To provide an air conditioning system for an aircraft which prevents a bleed air channel from being blocked due to icing in a condenser without taking engine bleed air as high temperature air into the air conditioning system. The system ...
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JP2003034298 |
To provide an air conditioning system for aircraft which can perform air conditioning without deteriorating engine performance when air conditioning in the air frame of the aircraft is performed. The air conditioning system SYS for the a...
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JP2003034299 |
To provide an air conditioning system for aircraft which can perform air conditioning without deteriorating engine performance when air conditioning in the air frame of the aircraft is performed. The air conditioning system SYS for the a...
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JP2002321697 |
To provide an air-conditioning system for an aircraft capable of reducing the required bleed quantity of an engine, dropping the temperature of obtained cold air, saving energy, reducing a size, weight and cost.Moisture is separated from...
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JP2002310551 |
To provide a cooling system with cold storage function in which the high output circuit part of an aircraft can be cooled without causing abrupt increase in engine bleed air or power consumption.The high output circuit part 2 is cooled b...
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JP2002191714 |
To suppress a fire in a sealed space extending to a hardly unlimited period of time.In this method to extinguish a fire which brakes out in a sealed space, especially in the cabin or the cargo section of an airplane, by feeding nitrogen ...
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JP2002127994 |
To eliminate problems in an air conditioner in an aircraft provided with an air cycle system and a vapor cycle system in which supply of prepressure air into a cabin is performed by the air cycle system, and in which cooling to electroni...
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JP2002130860 |
To provide an air conditioner equipped with a condenser capable of being cooled without employing cooling air from a turbine.In the air cycle type air conditioner, a thermo-module 82 consisting of the assembly of Peltier elements is arra...
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JP2002119605 |
To provide an oxygen mask storage box which can facilitate the storage of a mask without obstructing the releasing of the mask.This oxygen mask storage box is equipped with a housing 10 and a door 12. In this case, the housing 10 include...
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JP2002115926 |
To solve the problems of prior art such that cooling of a condenser of an aircraft is achieved with two-step adiabatic expansion of air taken into a cabin, so that power recovery with each expansion is required to result in increased bla...
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JP2002114198 |
To easily open a part of a door in the inspection work with respect to a storage box for storing an oxygen mask for passenger of an airplane.This oxygen mask storing box comprises a housing 10 closed by the door 12, and a piping accommod...
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JP2002096799 |
To reduce the consumption of engine fuel needed for air conditioning.An exhaust turbine 11 driven by introduction of exhaust from a pressurized cabin 2 is added to an air cycle machine 6 consisting of an extraction turbine 5 and a compre...
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JP2002087392 |
To provide an air-conditioning system having reduced cooling energy for cooling a water vapor corresponding to the humidity of a cooled air.An engine bleed air 1 is previously cooled by an outside air 2 in driving a turbine 6 and a sucti...
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JP2002061975 |
To provide an air conditioner for a transporting machine capable of alleviating an engine load by supplying cooling air of a necessary amount to a living room or the like and reducing a gas extraction of the engine.The gas extraction out...
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JP2002002596 |
To suppress the amount of engine bleeding air even when requiring a large amount of ventilating air.Engine bleeding air BA is inducted into a turbine T to drive an air cycle machine ACM, and the pressure of outside air is raised by using...
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JP2001348000 |
To provide a low cost nitrogen separator preventing deterioration of airframe performance caused by increase in engine bleed air quantity and improving a mounting property from reduction of size and weight by improving a nitrogen separat...
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JP2001328596 |
To provide an air conditioner for aircraft reduced in bleeding amount from an engine, outside air intake amount and weight as much as possible to reduce fuel consumption.A condenser 20 and a heat exchanger 16 are serially arranged in a p...
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JP2001296070 |
To provide an air conditioning system for a transport airplane performing the prevention of the freeze of pipes strong against breakdowns (redundant) by operating a high-output cooling system to use the lowest air flow rate and prepare t...
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JP2001294028 |
To provide an air-conditioning system capable of adjusting a fresh air amount taken inside the system by engine air bleeder in accordance with the number of passengers. When the number of passengers is inputted in a controller 17, a nece...
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JP2001253397 |
To provide an environment control device enhancing fuel consumption through a reduction in amount of bleed air, and exhibiting the desired cooling capability by means of a simple arrangement.Air in a cabin 2 is taken out and only oxygen ...
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JP3218688 |
PURPOSE: To effectively lower a temperature of the air to be supplied to a room to be air conditioned by a simple structure. CONSTITUTION: Part of the air of a room 1 to be air conditioned is discharged to a circulation air exhaust passa...
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JP2001213398 |
To provide an air conditioner for an aircraft permitting operation with little fuel consumption while satisfying air-conditioning conditions required under the total operating conditions of the aircraft.The bleed air flow of fresh air ex...
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JP3206891 |
To provide a curtain type smoke separating device in a passenger airplane in which smoke separating effect can be surely achieved at a smoke separating boundary set in a passenger room. A curtain type smoke separating device comprises a ...
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JP3206893 |
To lead the smoke or the smell of tobacco together with air blown from an air supply grill to the rear part in a plane even if a passenger smokes at a seat below the air supply grill by blowing the air from the right and left air supply ...
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JP3197497 |
To provide an indoor smoke separation mechanism of a negative pressure type and a smoking both in an aircraft which can simply ensure a smoking place. A smoking booth obtained by applying an indoor smoke separation mechanism of a negativ...
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JP2001074333 |
To simplify the constitution by omitting the process to evaporate water, in a heat pump utilizing the heat of condensation of steam. A cycle system 12 is constituted by connecting a steam separator 20, a compressor 30, and a main heat ex...
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JP2001074320 |
To provide a cooling system, permitting an aircraft, cooling mounted electronic instruments employing a refrigerant, to cool them even upon staying on the ground. A skin condenser 5 of vapor cycle cooling system(VCS) employing a refriger...
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JP2001071999 |
To meet the requirements for air-conditioning under all operating conditions of an aircraft, to operate an air-conditioning unit at reduced fuel consumption, and to reduce the weight of the unit. In this unit, air exhausted out of a pres...
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JP2001010596 |
To provide an air conditioner for aircraft capable of efficiently air- conditioning without any large load on an engine.The air extracted from an engine fan 1 through a switching regulating valve 2 is compressed by an electric compressor...
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JP2001010595 |
To provide a cooling system for an electronic apparatus on board an aircraft easy in maintenance of a vapor cycle cooling system(VCS).A skin heat exchanger 3 mounted on an outer shell 3a of a pod on board an aircraft takes in cold outsid...
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JP2000356358 |
To achieve uniform floor surface temperature by at least regionally incorporating a foil heater into a plate structural member and providing a thermal conductive upper cover plate.A plate structural member 1 comprises a honeycomb core 2 ...
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