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Patent Searching and Data


Matches 701 - 750 out of 1,599

Document Document Title
JP2017504010A
[Means for Solution] A flow indicating device of a respirator in which a flow of respiratory gas is shown is provided with structure in a lead pipe for supplying gas which can be breathed, and structure receives change as a result of exi...  
JP2017503571A
[Means for Solution] It is a system and a method of supplying oxygen to a passenger of an airplane, and is a source of oxygen supply, A system and a method have a controller which adjusts a flow of oxygen from a source of oxygen supply t...  
JP6073139B2  
JP2017502880A
The air-drying system for OBOGS is provided. The system concerned is provided with the bypass valve which has an opened state and a closed state. The bypass valve concerned carries out a fluid free passage with the air entrance which pro...  
JP6067847B2  
JP6050516B2  
JP6043314B2  
JP2016205810A
To provide a system and method for estimating a fouling condition of a heat exchanger of an environmental control system (ECS) for an aircraft.A method and apparatus for estimating a fouling state of a heat exchanger 102 of an aircraft. ...  
JP2016203881A
To provide a duct structure for sufficiently discharging a flow joined in a substantially right angle duct connection section and jetted to the outside of a duct to the outside of an aircraft through an air pressure control port.A duct s...  
JP6032980B2  
JP6027193B2  
JP2016533948A
The present invention relates to a system provided with a control unit (1*5) which carries out drive control of at least one air vent (1*8; 2*1; 3*1) automatic in the car. An air vent (1*8; 2*1; 3*1) has a plurality of parts (3*3, 3*4, 3...  
JP2016175481A
To provide a water flow-in prevention device which can more sufficiently prevent flowing of water into an aircraft at emergency landing on water, and which actuates more stably.A device 10 for preventing flowing of water into an aircraft...  
JP6002069B2  
JP2016172549A
To provide a method and system for an air management system (AMS).The AMS includes a jet pump assembly including a motive air inlet, a plurality of suction inlets, and a single outlet. The AMS also includes a supply piping arrangement in...  
JP2016526987A
[Means for Solution] A self-support type respirator used in the case of fire extinguishing is provided with the following. A hood which covers a wearer's head, A film which seals a hood and makes a respiratory room inside a hood, A sourc...  
JP2016155494A
To secure, even when a mechanism for cooling instruments equipped in a cockpit of an aircraft, flowing of air for cooling the instruments to an allowable temperature or less.An aircraft 1 comprises: a cockpit 2 with the inside pressurize...  
JP2016155537A
To balance weight and complexity with comfort in addressing needs for a quiet, relatively uniform, and generally unobtrusive air flow into a cabin for passenger comfort.Aircraft, air conditioning systems 12 and air diffusers 14 that may ...  
JP5976802B2  
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  

Matches 701 - 750 out of 1,599