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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...
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JP2011510861A |
A wing-engine combination includes: a wing with a main wing and an engine with a premixing chamber, a combustion chamber and a hot-air space, which includes: an engine bleed-air duct, which extends along the wingspan direction and along ...
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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...
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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...
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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...
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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...
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JP2011504844A |
An energy supply system for operating at least one air conditioning system of an aircraft, comprises at least one air line network and at least one electric line network. The air line network is connected to the air conditioning system a...
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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...
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JP4633063B2 |
A cooling air supply system for an aircraft is configured to supply cooling air from the surroundings of the aircraft to at least two devices requiring cooling air (38, 44, 56) within the aircraft. The cooling air supply system includes ...
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JP4630286B2 |
A method and a device for air-conditioning aircraft cabins proposes that the impulse of an air jet ( 26 ) injected into the cabin is altered, dependent upon a temperature measured.
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JP4630287B2 |
A device for temperature control in an aircraft cabin includes a first supply control arrangement and a first pressure control arrangement. The first supply control arrangement includes an air duct and a valve arrangement that controls a...
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JP4625053B2 |
An environmental control system includes an air cycle machine (ACM) (26) mounted adjacent an air-liquid heat exchanger (58) through a diffuser (90) that contains a diffuser plate (92) having a spike (96). The diffuser plate receives airf...
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JP4617469B2 |
The invention relates to floor heating for an aircraft which has a floor (20) made up of heatable panels (18). In order to be able to heat up the panels (18) in an energy-saving way, the same are provided with hollow chambers (26) which ...
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JP4614970B2 |
Method for controlling the temperature of feed air injected into at least one cabin zone of a passenger aircraft, the temperature of injected feed air being controlled for each cabin zone dependent on the deviation of the injection tempe...
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JP4614972B2 |
A ram air channel (10) for the supply of ambient air in an aircraft includes a first air inlet (12) and a main flow channel (16) which extends downstream of the first air inlet (12). In order to guarantee that the systems on board the ai...
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JP4614971B2 |
The invention proposes that a camera (18) takes a technical picture of an air outlet valve (10) of an aircraft, and the picture taken of the outlet valve (10) is displayed on a picture display unit (20), for example in the cockpit of the...
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JP4614969B2 |
A cooling system for the cooling of heat producing devices in an aircraft is designed with a central cold producing device, at least one cold consumer and a cold conveyance system which connects the cold producing device and the cold con...
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JP4610568B2 |
A device for temperature regulation of sections of the interior of an aircraft includes a controlled mixer valve for the mixing of engine bleed air and air that is cooler than the engine bleed air in order to obtain pre-tempered mixed ai...
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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...
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JP4589396B2 |
An Environmental Control System comprises an air cycle machine (26) having a first turbine (22), a second turbine (24), and a compressor (20) mounted between the first turbine (22) and second turbine (24). It further comprises a RAM air ...
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JP4575380B2 |
A mixer includes a fresh air tube defining a passage having an inlet receiving conditioned air from an air conditioning pack. The fresh air tube includes an outlet providing mixed air to a cabin of the aircraft. An outer tube at least pa...
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JP2007516895T5 |
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JP4538005B2 |
The invention relates to a device (10) for heating an aircraft cabin and comprises a first hot air supply line (12) that leads to an air conditioning unit (14), a flow control valve (16) that is disposed in the first hot air supply line ...
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JP4537399B2 |
A mixer includes a fresh air tube defining a passage having an inlet receiving conditioned air from an air conditioning pack. The fresh air tube includes an outlet providing mixed air to a cabin of the aircraft. An outer tube at least pa...
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JP4537106B2 |
A manifold (48) for an air generation unit (10) comprises a manifold (48) having opposing first passages (90) and opposing second passages (92). A condenser inlet passage (94) in fluid communication with said opposing first passages (90)...
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JP2010528222A |
The pump has a pneumatic actuator (10) arranged on a high pressure air supplying pipe (2). A power circuit is arranged between a pressure source and a pressurization pipe (14), and delivers controlling pressure to a controlling chamber (...
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JP4510634B2 |
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...
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JP4509110B2 |
A cabin pressure control system and method extends the cabin pressure control logic beyond the original maximum certified altitude of the aircraft, without having to update the control logic. Thus, the control system provides an independ...
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JP4490963B2 |
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JP4487792B2 |
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JP4489776B2 |
An air conditioning pack for an aircraft provides primary and secondary heat exchangers arranged in a ram air duct. A third heat exchanger is arranged in the ram air duct and is fluidily connected to the primary and secondary heat exchan...
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JP4483150B2 |
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JP2010519119A |
The present invention relates to a fuselage of an aircraft or spacecraft, with at least one shell element and a structural element. An interspace to which air can be admitted by an air stream is provided between the at least one shell el...
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JP2010513119A |
A cooling system for an aircraft includes an air inlet through which air from the environment of the aircraft enters a ram air channel, and an air outlet through which air emerges from the ram air channel. A heat exchanger is arranged in...
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JP4453795B2 |
To provide an air-conditioning system for an aircraft capable of reducing the required bleed quantity of an engine, dropping the temperature of obtained cold air, saving energy, reducing a size, weight and cost. Moisture is separated fro...
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JP4435168B2 |
A snow filter for an airplane cabin air supply system is provided with a coned inlet screen which allows some air to pass through and some snow to be retained. The coned configuration diverts much of the air and snow toward a downstream ...
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JP4414463B2 |
A humidification apparatus which makes possible individual humidification of the air in a cabin of a passenger or cargo aircraft makes available a conditioning fluid to be ejected into the cabin from an outlet nozzle (10). The conditioni...
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JP4412562B2 |
A pair (A,B) of architectural archway members (40) for an aircraft, along the length of an aircraft fuselage (60). The archways are used to run or connect various transport elements, such as electrical wiring, water lines, and environmen...
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JP4410790B2 |
An aircraft is provided with an integrated galley refrigeration unit (30) and vehicle cabin air conditioning packet (28). A control selectively determines whether the provision of cooled air into an air cooled galley (32) takes precedent...
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JP2010502501A |
The system (100) includes a fresh-air system (110) which leads fresh air into the aircraft cabin and coupled to a circulating air system (140), such that used cabin air is led into the fresh-air system. The fresh-air system includes an a...
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JP2010501404A |
The system (10) has a cold carrier fluid circuit (24) thermally coupled to a cold producing device (12) comprising a condenser (20), and connected to a heat load (28) to carry-off the heat from the load (28). A cold carrier fluid circuit...
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JP2010501390A |
The frame element (10) has a pair of longitudinal hollow struts (12,14) that are connected together using connection struts (16,18). Each longitudinal strut has air inlet connection (12a,14a) connected to the air outlet duct of the aircr...
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JP4396971B2 |
A life-support system for an aircraft B includes a first oxygen supply apparatus A operable to provide a limited supply of first product gas being one of pure oxygen and oxygen enriched gas, to a breathing gas supply apparatus 12, 13, 14...
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JP2010500214A |
The invention relates to a storage box (13) in which is received a protective mask (4) adapted to be applied on the face of an aircraft crewmember, said storage box further comprising signaling means (19) activable upon occurrence in the...
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JP2009287522A |
To provide an improved bleed air cooling method used for a gas turbine engine.This bleed air cooler assembly 36 includes a cooler body 44 defining a fluid passage within it. The cooler body 44 is formed of two halves 58, 60 of a shell de...
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JP4381852B2 |
An air generation unit (AGU) (10) includes a pressurized air source, such as an engine providing pressurized air. First and second air cycle machines (ACM) (16, 18) are fluidly connected to the pressurized air source for receiving the ai...
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JP2009542394A |
The invention relates to a respiratory gas supply circuit (1) for an aircraft carrying passengers and crewmembers (30), comprising a source of breathable gas (R1, R2), at least one supply line (2) connected to said pressurized source, a ...
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JP2009542393A |
The invention relates to a respiratory gas supply circuit (1) for an aircraft carrying passengers and crewmembers (30), comprising a source of breathable gas (R1, R2), at least one supply line (2) connected to said pressurized source, a ...
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JP4375963B2 |
The invention relates to an apparatus, in particular for a fuel cell-powered vehicle, with a compressor (6) that compresses air, which constitutes the working medium of a cold air process air conditioning unit or heat pump. The invention...
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JP2009274593A |
To secure a flow rate of low-temperature gas while restraining a total mass of parts required for an air conditioning system at a small number of parts and a small processing manhour in an air conditioning system having a heat exchanging...
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