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Patent Searching and Data


Matches 751 - 800 out of 1,580

Document Document Title
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...  
JP5610558B2  
JP2014526993A
At least one 抽気弁 (5, 5', 5") which the present invention is a system which extracts air by an airplane, and can extract a flow (F) of air by an airplane, It is related with a system provided with the 1st temperature information mod...  
JP2014184790A
To enable an air-conditioning duct for an aircraft to be reinforced by an inexpensive and relatively simple method, while suppressing an increase in weight and occupied space.A duct body 11 of an air-conditioning duct 10 for an aircraft ...  
JP2014525371A
A vent system which carries out a fluid free passage with an air condenser for sending dust air simultaneously to one or more galley foodstuffs and drink 保管隔 rooms and which can be reconstructed can be reconstructed so that it may ...  
JP5591397B2  
JP2014165365A
To provide a drip-proof air-cooled cooling structure of a housing which improves the cooling performance and environment resistance of an electronic apparatus disposed in the housing.A drip-proof air cooled cooling structure of a housing...  
JP5559806B2  
JP2014516858A
Air passenger compartment (1) Air supply circuit which is an air-conditioning system of 用 and it connects to at least one air distribution exit (S) which carries out the opening of at least one exterior air entrance (E) into a compartm...  
JP5542138B2  
JP5474021B2  
JP2014054969A
To provide an air conditioning system minimizing an engine bleeding amount without an influence of the engine bleeding amount on a cooling capability of cooling conditioned air used to cool electronic equipment having an increasing heati...  
JP5449291B2  
JP2014043148A
To efficiently adjust a flow rate irrespective of the high-low level of input side fluid pressure in an air conditioner for controlling the flow rate of piping by using a butterfly valve.In a sealed control chamber 2, an input port 3, a ...  
JP2014019174A
To provide a device to prevent water from flowing into an aircraft through a pressure control valve at the time of emergency landing on the water without requiring operation by a pilot.A closing lid 6 is installed to close a duct 2 of a ...  
JP5395069B2  
JP2014000947A
To prevent foreign objects from entering an air unit of an aircraft.A system for preventing foreign objects from entering an air unit of an aircraft is provided including a reverse J-tube (48) mounted on a wall of a ram air header. A fir...  
JP5385127B2  
JP2013252851A
To provide an environmental control system which reduces the amount of external air flowing into a cabin while meeting the minimum flow rate regulations per each occupant, improves airflow and air quality in the cabin, reduces pollutants...  
JP5373894B2
The system has pipes (2-4) for conveying gas from a source (1) to a work place (5) i.e. gas outlet. A flow rate determining device (7) determines gas mass flow in the pipes. A pressure determining device (9) determines static pressure in...  
JP5368452B2
An outflow valve for an aircraft has a frame for arrangement in an opening of an outer shell of the aircraft, a first flap pivotably arranged in the frame for controlling a flow cross-section of at least one first inflow opening and at l...  
JP2013248934A
To provide a water separator to be used in an aircraft air conditioning system, in order to solve the following problems: a conventional water separator has long piping, so that air flow resistance and pressure loss are increased due to ...  
JP2013247215A
To provide a liquid cooling system of airborne electrical components in which the flow rate of cooling liquid being supplied to airborne electrical components is optimized by a simple method.The liquid cooling system of airborne electric...  
JP2013244751A
To reduce air resistance during flight while preventing occurrence of a surging phenomenon of a fan for driving a drive shaft of an air cycle machine by securing cooling performance in flying in high altitude.In an air-conditioning syste...  
JP5361915B2
Disclosed are a cooling device (200) for high temperature fluid, a flight vehicle (100) having the same and a cooling method for high temperature fluid, the cooling device (200) including a heat exchanger configured such that fluid is in...  
JP5358682B2
The invention relates to an air duct (10) for supplying ambient air in an aircraft, comprising an air inlet (12), a flow duct portion (16) extending downstream of the air inlet (12) and a feed device (22) that is devised to feed ambient ...  
JP5343511B2
To suppress inconvenience that a low temperature air flow passage is closed through the deposition of a freezed moisture content on an inlet side surface of a low temperature gas flow passage of a core part without preparing a particular...  
JP2013512821A5  
JP5336077B2
An existing cooling system (2) has a heat exchanger arranged in a ram-air cooling channel (3) that serves as a cooling sink. An integrated cooling system (8) integrated in the existing cooling system has a heat exchanger (9) integrated i...  
JP2013210998A
To provide a velocity mapping system comprising a sensor system and an airflow mapper.A sensor system 204 is configured to generate data 232 about a velocity 218 of airflow 214 for a location in a duct system 216. An airflow mapper 206 i...  
JP2013538153A
the present invention more generally adapts sizing of the power supply to the power demand of an airplane to the actual power demand of a cabin pressure control system -- the ratio of an airplane -- it is related with restricting an amou...  
JP5295114B2
The arrangement has pipelines (1, 2) connected to turbines (Ta, Tb), and arranged downstream from the turbines. An outlet of a heat exchanger (11) is connected to a pipeline (4), and feeds temperature-reduced fresh air to the pipeline (4...  
JP5286361B2  
JP3185900U
[Subject] A draining mechanism which enables discharge of water satisfactorily at the time of un-operating of air-conditioning is provided without enlarging a path of a ドレン hole for drainage provided in a channel of an air-conditio...  
JP2013533167A
The invention relates to a valve (10) for controlling the internal pressure p in a cabin of an aircraft, comprising a first flap (11) and a second flap (12), wherein the flaps (11, 12) control a pressure-changing fluid flow (L) between t...  
JP5269780B2  
JP5258776B2  
JP2013147244A
To supply clean cooling air to interior components of a ram air fan.A particle separator includes a first housing 44 and a second housing 46. The first housing extends along an axis from an open proximal end 52 to an open distal end 54. ...  
JP2013530077A
[Means for Solution] An indoor ceiling panel system is provided with a ceiling panel attached to a ceiling field, the 1st air current inclination panel in the 1st flank of a ceiling field which forms an air current passage, and the 2nd a...  
JP2013144540A
To provide an environmental control system and a speed sensor module in the system.An environmental control system includes an air cycle machine 100 for conditioning an interior space with cooling air, a speed sensor module 105 having a ...  
JP2013126840A
To provide an air conditioning system that properly cools an engine bleed air in an easy structure.An air conditioning system includes: an air cycle machine ACM that includes first and second turbines 4 and 5 and a compressors 3; a boots...  
JP5212986B2  
JP2013119078A
To improve the water removal efficiency of a water separator for separating water by swirling the water in gas.The water separator includes a gas inlet pipe 2; a swirling current generation element 3 formed in the inlet pipe; a disk-like...  
JP2010533096A5  
JP5208817B2  
JP5205362B2
Methods and systems for providing secondary power to aircraft systems. In one embodiment, an aircraft system architecture for providing power to an environmental control system includes an electric generator operably coupled to a jet eng...  
JP5204772B2  
JP2013103716A
To configure an aircraft air conditioning system so as to reduce the energy required for an aircraft.The aircraft air conditioning system 10 includes: a first compressed air supply source 12 including a compressor 14, a motor 16 and a tu...  

Matches 751 - 800 out of 1,580