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Patent Searching and Data


Matches 901 - 950 out of 1,610

Document Document Title
JP4781590B2  
JP2011525407A
The aircraft emergency oxygen supply system includes one or more sources of supplemental breathable oxygen, one or more inlet valves for one or more breathing devices, connected to the inlet valves, and one or more cabin air pressure tra...  
JP2011525452A
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 ...  
JP2011524300A
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...  
JP4758480B2  
JP2011523610A
A system (10) for ventilation of an aircraft area (32, 34) comprises a ram-air duct (12) with an air inlet (14), a first ram-air duct branch (16) and a second ram-air duct branch (18) allowing for being flowed parallel to the first ram-a...  
JP2011521828A
Device for exhaust air cooling of aircraft air-conditioning systems comprising a bypass channel that bypasses an aircraft air-conditioning system arranged downstream of a ram air channel with a ram air inlet channel portion, and merges i...  
JP2011521831A
At least one rum air-intake in which the present invention has at least one rum air breathing opening, It has at least one secondary air breathing opening which has an interval kept from a rum air-intake, and at least one flap attached s...  
JP2011521841A
A cooling system (10) for cooling a heat-loaded device (14) in a vehicle, particularly an aircraft, comprises a cooling circuit (12), through which flows a heat transfer fluid and which is thermally coupled to the heat-loaded device (14)...  
JP4732364B2  
JP4732520B2  
JP4715984B2  
JP4707121B2  
JP2011111016A
To more efficiently suppress inconvenience that heat exchange efficiency is lowered through the deposition of freezed moisture content on an inlet side surface of a low temperature gas flow passage of a core part by a simple structure in...  
JP2011516344A
The present invention relates to a defrosting system for airplanes which has at least one air delivery means for sending air to at least one heat source and a portion in which an airplane should be defrosted. As compared with a prior art...  
JP2011516344T
The present invention relates to the defrosting system for airplanes which has at least one air delivery means for sending air to at least one heat source and the portion in which an airplane should be defrosted. As compared with a prior...  
JP4686038B2  
JP4680987B2  
JP4673856B2  
JP4673917B2  
JP2011511731A
An aircraft fuel cell system (10) includes a fuel cell (12a, 12b, 12c, 12d) which has an oxidant inlet (14a, 14b, 14c, 14d) for supplying an oxygen-containing medium to the fuel cell (12a, 12b, 12c, 12d). An oxidant supply line (16) has ...  
JP4669481B2
In a cooling system (10) for cooling heat-generating installations (44, 46, 48) in an aircraft, with a refrigerating installation (12), at least one refrigeration consumer (44, 46, 48) and a refrigeration transport system (14) connecting...  
JP2011510861A
They are wings and an engine connection object provided with wings (W) which have a wing (W1), and an engine (E) which has a 予混合 chamber (E1), a combustion chamber, and high temperature air space (E2), a) An engine 抽気 suction s...  
JP2011509863A
An air conditioning system for an aircraft for the individual air conditioning of regions of a cabin of an aircraft includes a central air conditioning device, which provides a pressurized and temperature-controlled central air flow. A p...  
JP2011045711A
To provide a fire suppression system configured to minimize environmental load.The fire suppression system 20 includes a main gas container 22 and a second gas container 24 containing inert gas. The gas container 22 communicates with a m...  
JP2011506185A
An aircraft cooling system (10) comprises a cooling element (12), which comprises a housing (14), a cooling air inlet (18) formed in the housing (14) and a plurality of heat exchangers (32, 34, 36, 38), which are disposed on lateral surf...  
JP2011506190A
The invention relates to a cabin system for an aircraft fuselage, having one or more lining components for interior lining, and optionally one or more cabin equipment components, wherein the lining component can be installed either separ...  
JP4633063B2  
JP2011031781A
To provide a heat exchanger which can let gas circulating in a duct spread to the corners of an inlet surface in a reduced size.The heat exchanger 7 includes: a plurality of high temperature channels 16 for communicating a high temperatu...  
JP2011504773A
The present invention relates to Testa (100) for examining the reliability of the cockpit oxygen distribution circuit (1) which has a plurality of component parts (20, 30, 40, 50) which secure the supply of oxygen to the member of the co...  
JP2011504844A
The present invention relates to an energy supply system which operates at least one air-conditioning system (26) of an airplane in at least one air line network and at least one electric line network, An air line network is connected to...  
JP2011031780A
To provide a heat exchanger for an aircraft which can prevent an iced component from accumulating in a low temperature channel.The heat exchanger for the aircraft 7 includes: a core 10 having a plurality of high temperature channels 16 f...  
JP4630286B2  
JP4630287B2  
JP4625053B2  
JP4617469B2  
JP4614970B2  
JP4614972B2  
JP4614971B2  
JP4614969B2  
JP4610568B2  
JP2011500411A
The system has a control device (26) arranged to ensure that air provided by an air supply device (18) enters into airplane region to be aerated e.g. airplane passenger cabin (12), via an air inlet (24) with velocity and temperature. The...  
JP2010540310A
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...  
JP4589396B2  
JP2010535664A
The invention relates to a valve for controlling a fluid flow from a first environment to a second environment, having a frame for disposing a separating element in the region of an opening, said element separating the first environment ...  
JP4575380B2  
JP2007516895A5  
JP2007516895T5  
JP2010533096A
An aircraft cockpit that includes comfort and/or security adjustable equipment in which the adjustments are controlled by an adjustment management system so that, by the unique selection of a position desired by the pilot from at least t...  
JP2010208488A
To achieve efficient thermal control by a simple configuration and an improved degree of freedom of an attachment arrangement including design. An aerial 11 is arranged on an outer wall of a flight vehicle body 10, and a pressurized cham...  

Matches 901 - 950 out of 1,610