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JP4186398B2 |
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 ou...
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JP4182350B2 |
To provide an air-conditioner for an aircraft capable of preventing any increase of the concentration of carbon dioxide while suppressing discharge of water in the air in the aircraft, reducing the ventilation volume by fresh air, and en...
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JP2008272082A |
To provide an indoor environment controller for acquiring the accurate biological information of an operator operating a machine from the action of the operator during the operation and reflecting the result on an indoor environment.The ...
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JP4174605B2 |
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JP4174606B2 |
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JP4174917B2 |
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JP4173008B2 |
According to this process, there is supplied to the passengers a first fraction of air enriched in oxygen from independent supply elements, in particular high pressure cylinders ( 16 ), during a descent phase of the aircraft between a no...
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JP4172088B2 |
A cyclic circuit (20) is constructed by sequentially connecting an expander (22), a heat exchanger (30) and a compressor (21). A dehumidifying mechanism (60) is provided for dehumidifying a heat-absorbing air taken in through an inlet du...
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JP4170492B2 |
To improve fuel consumption by a method wherein a ram penalty is reduced by suppressing an introduction amount of the atmosphere. In this control device, exhaust gas 16b from a pressurized cabin 2 is mixed in the atmosphere 16a inputted ...
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JP2008222157A |
To provide a method of controlling an apparatus for separating product gas and non-product gas from air supply.The method includes sensing the oxygen concentration in the product gas produced by the apparatuses 15, 16, 17, determining an...
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JP4144475B2 |
To provide an air conditioner capable of keeping a predetermined cooling capability even if an engine extraction gas is reduced. Cooling air B4 is generated by an air cycle system 1 constituted of an air cycle machine 30 having a two-sta...
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JP4144379B2 |
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JP4144414B2 |
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JP4136809B2 |
To reduce consumption of engine fuel required for air-conditioning at a high altitude. This device is provided with an exhaust using air-conditioning system A having an air cycle machine 12 comprising a compressor 12a for compressing the...
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JP4138030B2 |
A system and method of performance testing an aircraft's oxygen supply system where demand is assured by in use performance testing and monitoring by a controller and monitor for the partial pressure of oxygen necessary to meet demand in...
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JP4122925B2 |
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JP4114277B2 |
To provide an air-conditioner for an aircraft that is light in weight and compact with high efficiency and reliability with good mileage and is possible to dehumidify and cool down to minus several dozens of degrees Fahrenheit with less ...
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JP4110667B2 |
To reduce bleed air from an engine, enhance a fuel consumption, to provide a lightweight and compact system, and enhance reliability. Bleed 1 is taken into a head exchanger 3, an evaporator 5 using a refrigerant of a VCS 51 is arranged i...
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JP4093957B2 |
A multi-phase headset ( 50 ) for aircraft crew members is provided which includes an inflatable gas mask unit ( 54 ) and a visor unit ( 56 ), supported on the head of a user ( 60 ) by mounting assembly ( 52 ). The overall headset ( 50 ) ...
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JP4082066B2 |
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JP2008094189A |
To provide a technology capable of reducing the weight, the space or the cost of an entire system, by reducing necessity of providing any special device or air source for air-conditioning, separately from a device of generating propulsio...
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JP4080037B2 |
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JP4066703B2 |
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JP4066553B2 |
A first channel (20) is formed by sequentially connecting a compressor (21), a vapor separator (55), a heat exchanger (30) and an expander (22). In the first channel (20), a room air is taken as a primary air and discharged to outdoors. ...
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JP2008056240A |
To supply air for a pre-load into an aircraft to cool, heat, and ventilate the inside of the aircraft and increasing cooling capability in the aircraft during parking effectively.This air conditioner for the aircraft is mainly composed o...
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JP2007519555T5 |
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JP2008024288A |
To provide a system for controlling a compressor flow capable of feeding the outside air of an adequate volume to a temperature control system in an air-conditioner of an airplane.An inlet 50 is configured to direct a first stream of air...
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JP4039105B2 |
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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JP4039107B2 |
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JP4023006B2 |
To provide an air conditioner for an aircraft satisfying the air- conditioning conditions required under the entire operating conditions of the aircraft, capable of operation with the least fuel consumption, and reducing the weight there...
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JP4023002B2 |
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JP4025198B2 |
The invention relates to a cabin pressure control system (10), a method of controlling the actual pressure inside a cabin (50) and an outflow valve (14; 15; 16; 17), especially for use in said system (10) or said method. The invention pr...
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JP4023260B2 |
To provide an air conditioning system for aircraft capable of preventing the generation of choking in a flow passage of a condenser by freezing without heating the flow passage with the bleed air of an engine. This air conditioning syste...
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JP4023018B2 |
To improve fuel consumption by suppressing an atmosphere input amount without damaging the living properties of a pressurized cabin. In this control device, since exhaust gas 16b from a pressurized chamber 2 is used as low temperature ai...
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JP3999818B2 |
A system and method for automatically controlling cabin air temperature TCBN in an aircraft having a cabin and a mixed air delivery system. The mixed air delivery system provides a flow of mixed air having an actual mixed air temperature...
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JP3970329B2 |
An integrated environmental control system is disclosed for providing conditioned supply air to loads such as a passenger cabin of an aircraft. The system comprises at least two shafts, each shaft having a fan, compressor, and turbine me...
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JP3961572B2 |
The compression molded aircraft personal service unit and integrated oxygen dispensing system module housings are formed by compression molding of a sheet molding material. The integrated oxygen dispensing system module can be mounted se...
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JP3951730B2 |
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 ...
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JP3951421B2 |
To make the air cycle system light weight while maintaining air conditioning function similar to that of a plurality of systems. Bleed air introduced through a bleed passage L1 from either of the two engine E1 and E2 is cooled by a first...
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JP3947112B2 |
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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JPWO2005057087A1 |
To provide a cooling system in which the efficiency of a refrigerator does not decrease when a predetermined temperature and humidity of a cooling chamber are obtained even when the outside air temperature or the like changes. A dehumidi...
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JP3917186B2 |
The compression molded aircraft personal service unit and integrated oxygen module housings are formed by compression molding of a sheet or bulk molding material. The integrated oxygen module can be mounted separately in the aircraft, or...
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JP3915263B2 |
To effectively save fuel consumption of a system without inviting size-enlargement and decrease in reliability. An air conditioning part 4 for supplying a pressure cabin 2 with conditioned air by controlling temperature and pressure of e...
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JP3911031B2 |
An air cycle air conditioning system comprises a first air source for supplying cooling air and a second air source for supplying high temperature system air. The system further includes a device for transferring heat from the high tempe...
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JP2007045398A |
To surely and efficiently control pressurization and control temperature in an aircraft cabin, and to supply fresh air independently of flight height.This is a method of operating an aircraft system having a first compressed air supply s...
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JP2007501041A |
The circuit has an oxygen supply line (5) connected to a pressurized oxygen source (1). A pressure regulator operates in response to a pressure control signal provided by an electronic control unit (9). A cabin pressure sensor (12) provi...
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JP2006313456A |
To provide a pressure regulator having a butterfly valve, capable of regulating a valve downstream pressure with higher accuracy.This pressure regulator 1 has the butterfly valve 3 disposed inside an intake conduit 2 and a drive part 4 o...
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JP2006524527A |
The present invention relates to a system for supplying oxygen to aircraft passengers (6,7) equipped with a PSA device having an air intake that receives compressed air from the engine (5), where the oxygen distribution line (3) is advan...
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JP2006290021A |
To provide an air cycle type air conditioning device for an aircraft having high flexibility for disposition in the aircraft and capable of effectively utilizing a limited space.Bootstrap cycle same as in the conventional air cycle machi...
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JP3837166B2 |
A bypass valve for use with a component of an air cycle machine is disclosed, wherein the component includes a conditioning member, an inlet and an outlet. The air cycle machine includes a component housing portion. The component housing...
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