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Patent Searching and Data


Matches 801 - 850 out of 1,582

Document Document Title
JP5190057B2  
JP2013512821A
It is a power generator. A thermoelectrical device is connected with an airplane ブリード system in order to generate electricity using a difference in temperature between ram air and bleed air.  
JP2013510042A
The airplane system for the improvement in cooling efficiency includes at least one air-conditioning pack (44) which has at least one air compression equipment (50) in which the electric power supply is carried out by at least one power ...  
JP5165737B2  
JP5162576B2  
JP3182131U
[Subject] A heat exchanger which prevents beforehand generating of fault which freezing moisture adheres to the front of a low-temperature gas passage of a capacitor or the surface near the inlet section, and takes up a low-temperature g...  
JP5156706B2  
JP5134371B2  
JP5121148B2  
JP5122465B2  
JP5116839B2  
JP2013001396A
To provide a performance detection method of an oxygen system for the aircrew and the system.This method includes: the step of obtaining an oxygen pressure of an oxygen cylinder 101 in an oxygen system for the aircrew 100, an atmospheric...  
JP2012255613A
To effectively increase the temperature of air in the inlet of a turbine without causing the lowering of a force for driving a compressor by a turbine, and the deterioration of a cooling capacity.The air conditioner includes: an air cycl...  
JP5106549B2  
JP2012532051A
A method and a system for an integrated エゼクタ valve assembly are provided. The 1st valve assembly constituted by integrated エゼクタ valve assembly so that a flow of fluid with comparatively lower pressure from the 1st inlet p...  
JP2012240526A
To solve problems that negative effects may occur in health of passengers/crew or static electricity may arise to cause electronic device malfunction owing to drying of air within a cabin, and further weight limit violation or fuel consu...  
JP5087091B2  
JP5084720B2  
JP5080537B2  
JP5074200B2  
JP5073657B2  
JP2012220996A
To provide a pressure regulator capable of avoiding the occurrence of variation in a pressure regulation performance of each pressure regulator due to a difference in fine machining accuracy.A pressure regulator V includes: a valve body ...  
JP2012218531A
To provide an air conditioning system for an aircraft, for preventing a trouble such that large drag is generated in an airframe of an aircraft as a large amount of ram air is supplied to a primary heat exchanger and a secondary heat exc...  
JP5059946B2  
JP2012201176A
To enable such aviation that a helicopter can avoid collision with an obstacle even in a state where the helicopter approaches the obstacle.In a helicopter 10, the location of the helicopter itself is detected on the basis of a received ...  
JP2012180086A
To provide a compressor bleed air supply system that reduces the amount of compressed air used by a precooler and the weight of the precooler.The precooler 7 for cooling compressor bleed air 38 for an environmental control system 6 inclu...  
JP2012176716A
To defog a target area within a window with a little quantity of hot air.A defogging device includes gas piping 21 in which a hot-air gas flows from a hot air source. Inside a window pane 2, there are formed: a cavity portion 27 spreadin...  
JP2009525212A5  
JP2012518567A
A system for cooling a region in an airplane has a mixed chamber (18), The mixed chamber is connected to a device (20a, 20b) which carries air through which it re-circulated for supplying air which was connected to an air conditioning me...  
JP2009531215A5  
JP4989463B2  
JP2012135737A
To achieve a constitution, in a static mixing mechanism arranged in piping, which can reduce pressure loss and further reduce length dimensions in a flow passage direction while achieving sufficient stirring performance in a limited inst...  
JP4976421B2  
JP4972652B2  
JP2012126392A
To provide an aircraft configuration that improves air flow control in the aircraft sidewall volume.An aircraft fuselage sidewall may include the aircraft sidewall volume and a flow controller. The aircraft sidewall volume may be delinea...  
JP3176710U
[Subject] According to the necessity for a use, a module type air-conditioning (AC) system provided with composition which can be changed on the spot is provided so that an independent air style or its both sides of a single air style or...  
JP3176326U
[Subject] In an expansion turbine used for an air harmony device for airplanes, deposition of ice to an expansion turbine exit or a turbine blade is prevented. [Means for Solution] An air harmony device for airplanes of this design suppl...  
JP4954212B2  
JP2012512787A
Air treatment catalyst systems and methods for treating the air in the aircraft cabin environment are provided. The catalyst system and method remove ozone, volatile organic compounds, NOx and other pollutants. The catalyst system used t...  
JP2012092973A
To provide an actuator cylinder of an accumulator system, which provides a significant reduction of overall length to thereby enable compact packaging.The accumulator system 26 includes: an accumulator cylinder 28; and an actuator cylind...  
JP2012092994A
To more effectively suppress failure of reduction in heat exchange efficiency caused by adhesion of frozen moisture on a surface on a low temperature gas flow passage inlet side of a core part, by a simple configuration.This air conditio...  
JP4932725B2  
JP4926978B2  
JP2012509216A
Leak is detected in an urgent ventilation method of an airplane cabin (12) around an air mixer (24) of an airplane air-conditioning system (16). An urgent air flap (38) which bars air exchange between an airplane field (40) which adjoins...  
JP4912359B2  
JP2012508135A
The first valve (14) that the present invention is arranged in a body field (28) of the first airplane, and functions as an exhaust valve of an airplane cabin pressure control system at the time of normal operation, Air is supplied to a ...  
JP2012066755A
To provide an airplane with deodorizing and disinfecting functions that can efficiently make environments in the airplane comfortable.A static atomizing apparatus 11 generating charged microparticle water by applying a high voltage to a ...  
JP2012507424A
In order that the system (10) for cooling the heat exchanger (12) in an airplane may supply engine ブリード air to a process air line (28), the first end has the process air line (28) connected to the engine (16) of an airplane. The ...  
JP4906225B2  
JP2012506815A
The air-conditioning system (10) of an airplane cabin (12) has the air conditioning unit connected to the above-mentioned central mixer (16), in order to supply the air of desired low temperature to a central mixer (16). For a start, a r...  

Matches 801 - 850 out of 1,582