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Matches 851 - 900 out of 1,580

Document Document Title
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...  
JP4897833B2  
JP4879188B2  
JP2012030776A
To provide a cooling device for fluid, capable of minimizing influences by external environments.The cooling device includes: a heat exchanger configured such that fluid is introduced therein to be heat-exchanged with a refrigerant, and ...  
JP2012025382A
To improve cooling performance of a ram air fan (RAF) motor 20 in an aircraft environmental control system.A ram air fan device 10 is provided for making up for ram air, for example, when an aircraft is on the ground. The device includes...  
JP4869400B2  
JP2012020728A
To improve the cooling performance of a cabin air compressor (CAC) motor 28 in an environmental control system for an aircraft.A cabin air compressor apparatus includes: a cabin air compressor (CAC) 12 which is a centrifugal compressor; ...  
JP2012020167A
To provide an oxygen conservation method for use on an aircraft in the event of a loss in cabin pressure.The oxygen conservation method delivers allotments of oxygen and times the delivery of such allotments to each passenger so as to ma...  
JP2012500748A
The invention relates to an air conditioning system for a transportation means, having multiple zones to be air-conditioned, which may be variably air-conditioned by means of processed supply air in combination with individual trim air c...  
JP2012500146A
A combination ventilation and stowage bin system including at least one support duct defining an inlet for receiving conditioned air from a supply duct and an outlet for directing air into a passenger compartment, and a stowage bin for s...  
JP2011529821A
In order to increase the air humidity in a cabin region (10) of an aircraft equipped with a plurality of seats (16; 28), a device (12; 14) is provided, comprising a plurality of humidifying units (26) arranged in each case in spatial ass...  
JP2011529418A
A heat exchanger for an outer skin of an aircraft comprises at least one feed line for a coolant, at least one discharge line for the coolant and at least one bundle of coolant channels through which coolant flows, wherein in the case of...  
JP4832070B2  
JP2011529010A
The air-conditioning system of an airplane cabin has the air conditioning unit connected with the central mixer for the air supply to a central mixer, the -- being connected with a central mixer, in order that 1 re-circulation system may...  
JP2011529011A
The system (10) for discharging re-recirculating air from an airplane cabin has a plurality of discharge devices (12a*12j) distributed and arranged along one certain airplane cabin field (14). One control device (16) is set up in usual o...  
JP4820420B2  
JP4820417B2  
JP4809893B2
The electromechanical regulator for passenger oxygen is a hybrid oxygen regulator that provides for electronic or mechanical regulation of oxygen flow. The electronic portion of the regulator consists of an inlet solenoid valve, an outle...  
JP2011527252A
The system (10) for cooling an airplane field has an air conditioning unit (12a, 12b) for supplying cold air, a recirculating air conveying machine (20a, 20b), and a mixing chamber (18). The mixing chamber concerned can supply recirculat...  
JP2009525218A5  
JP4791532B2  
JP4787832B2  
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  

Matches 851 - 900 out of 1,580