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Patent Searching and Data


Matches 701 - 750 out of 1,579

Document Document Title
JP2016524508A
[Means for Solution] An advanced latch of a main door (22) of an oxygen container for airplane emergencies, A main door (22) is opened by it being manually released by a manual release actuator pin (52), moving a main door (22) to an int...  
JP2016523621A
In the hood possessing the reservoir for oxygen (3) which was closed by a flexible envelope (2) and removable stopper (5), and is provided with the exit orifice (4) connected with the inner side capacity room of an envelope (2), The rese...  
JP2016138555A
To provide a fan rotor for preventing undesired frequency vibration at a rotor and in a blade of the rotor.This invention provides a fan rotor 300 of a ram fan of an aircraft environment control system. The rotor 300 has a central body 3...  
JP2016522772A
[Means for Solution] A wall attachment storage compartment for cabins of an airplane (10) is provided with a case (14) which has the wall which turned to back attached to a wall which turned to the front of an indoor building. A storage ...  
JP5965320B2  
JP5961583B2  
JP2016520406A
The inner side capacity room of a flexible envelope (2) and this envelope is equipped with the exit orifice (4) which is carrying out the opening, The reservoir for pressurization oxygen (3) is in the respiratory protection hood in which...  
JP2016124544A
To provide a water injector for an aviation cooling system.A water injector 45 for an aviation cooling system includes a body 60 having a first end 62, a second end 63, and an intermediate portion 64 extending therebetween. A conduit 68 ...  
JP2016109694A
To conveniently measure performance of an aircraft air conditioning system.A measurement apparatus for an aircraft air conditioning system comprises: a sound receiver and a sound processor. The sound processor processes the running noise...  
JP2016060211A
To provide an aircraft vapor cycle device that can reduce the weight and size thereof for mounting on an aircraft.The aircraft vapor cycle device 100 includes: a container-like mixing part 20 for mixing ventilation air 12 taken from the ...  
JP2016060485A
To provide a system for efficiently cooling a passenger compartment by applying air cooled in a heat exchanger from a galley compartment to the passenger compartment when the demand for cooled air in the galley compartment is reduced.A c...  
JP2016055863A
To provide an improved air generation unit for aircraft.An air generation unit 1 for an aircraft 100 comprises air supply means 2 and a control unit 3. The air supply means 2 is constituted so as to supply air to an air-conditioning syst...  
JP2016052821A
To make it possible to efficiently cool an aircraft electrically-driven unit by air refrigerant.Heat exchangers 17, 31 are disposed to be adjacent to electrically-driven units 19, 33, respectively so that air (ventilation air or air outs...  
JP5897482B2  
JP2016508466A
The present invention relates to structure (3) which supplies electric power for emergencies to an airplane (1), and an airplane (1) is, It has a pressurization cabin (10), at least one main engine, and auxiliary power unit (APU), and is...  
JP2016508465A
The present invention relates to structure (3) which feeds air into an auxiliary power unit (2) of a pressurization cabin (10) and an airplane (1) provided with an auxiliary power unit (2), and is structure, Having a valve (31) which inh...  
JP2016033006A
To provide methods of producing an aircraft noise-damping panel which is not bulky but lightweight, withstands an operating temperature range of the aircraft, and has no lack of relevant frequencies.A panel includes a structural substrat...  
JP2016033005A
To provide a new aircraft with an improved air conditioning and/or ventilating system.The invention relates to an aircraft 1 with a fuselage 2 that comprises a framework structure 5 having at least one hollow frame 5a that is integrally ...  
JP2016506496A
[Means for Solution] It is a passive gas sensor for reading and sending out gas pressure of a system distantly, and is a hollow cylinder body, It is the antenna combined with the leg which for Distribution is carried out in the direction...  
JP2016506328A
It is an air-conditioning system for a cabin where an airplane was pressurized, and the system (1) is, An air drawing-in module (3) constituted so that it might draw circumference air from the exterior of an airplane, A point of having a...  
JP5873493B2  
JP2016026950A
To provide an aircraft environment conditioning system capable of detecting device failure.An aircraft environment conditioning system having an air cycle machine, which decreases a temperature and a pressure of airflow including high te...  
JP2016020198A
To detect catastrophic system failure that can result in a cabin smoke event.An aircraft environmental conditioning system 100 is disclosed that includes an air cycle machine for conditioning an airflow comprising hot compressed air by r...  
JP5851033B2  
JP5851412B2  
JP2016011662A
To provide an environmental control system eliminating a required heat exchanger and using less air from a higher compression location.An environmental control system includes: a higher pressure tap at a higher pressure location in a mai...  
JP5840790B2  
JP2015531721A
it is the method of supplying non-promoting power to an airplane -- shaft (13) of an environmental control system (1) of an airplane: an auxiliary power unit (4), and a starter/dynamo (18) -- and -- A method containing a step driven comb...  
JP2015531616A
An embodiment of the present invention is generally related especially with health of air for aerospace, and sterilization about health of air, and sterilization. A reaction chamber which includes the (a) entrance, an exit, and an intern...  
JP5803639B2  
JP5788915B2  
JP2015168424A
To solve the problem in which an aircraft air conditioning system is the largest energy user other than the propulsion of the aircraft itself and such wasted energy provides a harmful fuel combustion impact to the aircraft.There is provi...  
JP5778870B2  
JP2015526127A
[Means for Solution] An airplane emergency oxygen distribution apparatus (19) is provided with one or more flow control valves (20) connected to an oxygen storage container (12) which has a pressure seal (14) which can be destroyed, a ma...  
JP2015147571A
To provide a pressure equalization vent with increased airflow efficiency across the vent.A pressure equalization vent 314 for use in an aircraft assembly is provided. The pressure equalization vent includes an opening 500 having a first...  
JP2015523260A
[Subject] The present invention provides a system and a method for supplying, generating, saving and managing oxygen for which it was suitable ideal for use of an airplane on a plane, in order to supply oxygen for breathing to a passenge...  
JP2015522461A
[Subject] The present invention provides a system and a method for supply of oxygen which was suitable in order to supply oxygen for breathing to a pilot and a crew of a cockpit and to use by on a plane [of an airplane], and management. ...  
JP2015137096A
To provide a dehumidification system for a transport vehicle which prevents formation of water droplets on an aircraft structure in a cold atmosphere caused by condensation of water contained in conditioned air passing through an air dis...  
JP2015521135A
[Means for Solution] A hybrid type system (100) for generating oxygen is shown in this specification by on a plane [of an airplane] for breathing of a passenger and/or a crew member. This system is provided with an oxygen generator porti...  
JP2015114095A
To provide a method, system and device for liquid drainage.The system includes a drain tube coupled to an air distribution system, a sump coupled to the drain tube and configured to receive liquid from the drain tube, and a suction syste...  
JP2015113110A
To provide an improved aircraft system and a method for improving low inlet pressure cooling performance of an air cycle machine (ACM) pack system in a bleed air based aircraft air conditioning system, while maintaining a necessary air f...  
JP5727990B2  
JP2015051747A
To provide an aircraft cooling system capable of operating depending on a change in power consumption, while suppressing a temperature change of air supplied into an indoor space of an aircraft for which a predetermined ventilation volum...  
JP5655069B2  
JP2014231955A
To prevent degradation in heat exchange efficiency even if two heat exchangers are widely distant when a gas flow path of one of the two heat exchanger is connected to that of the other heat exchanger.A heat exchange system includes: a f...  
JP2014226981A
To provide an aircraft air conditioner capable of improving operability when being detached or reassembled from an airframe.This aircraft air conditioner 1 comprises: an evaporator 11; a condenser 12; a compressor compressing a refrigera...  
JP2014532002A
[Means for Solution] A chemical oxygen system for lavatories which provides a lavatory for airplanes with respiratory gas is provided with an oxygen generating system by which remote installation was carried out in order to supply oxygen...  
JP2014223904A
To provide a method of diagnosing a bleed air system fault in aircraft.A method includes: receiving a sensor signal from at least one of bleed air system sensors to define a sensor output 102; comparing the sensor output to a reference v...  
JP2014210239A
To provide a dehumidifier capable of melting frozen water in the dehumidifier while avoiding degradation in cooling capability, and an air conditioning system including such a dehumidifier.An air conditioning system 1 comprises a low-pre...  
JP2014527941A
The present invention relates to a valve for controlling internal pressure of a cabin of an airplane, Having the first flap (12) and the second flap (14) which were supported by frame (16), both flaps (12, 14) control a fluid style (L) t...  

Matches 701 - 750 out of 1,579