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WO/2014/158280A2 |
A cooling system for an aircraft includes a first cooling circuit having a first evaporator and a second evaporator, and a second cooling circuit having a third evaporator and a fourth evaporator. One of the first and second cooling circ...
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WO/2014/149271A1 |
There is provided an air duct assembly. The air duct assembly has a deformable duct preform having securing portions formed along opposing longitudinal edges. Each securing portion has a flange portion and a radius portion. The air duct ...
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WO/2014/142727A1 |
A climate control system (1), intended to be temporarily connected to at least one aircraft (2), when the aircraft is on the ground, with which handled air with at least one flexible conduit (23) is supplied to the aircraft's cabin from ...
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WO/2014/143194A1 |
A cooling system includes a heat exchanger (210) through which a refrigerant flows, and which rejects heat to a fluid, an evaporator (208), a first circuit having an expansion device (214), a second circuit having an expansion machine (2...
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WO/2014/137515A1 |
A method and apparatus for an air circulation system. The apparatus comprises a suite and a circulation unit. The suite has walls extending upward from a floor of the passenger cabin without reaching a ceiling of the passenger cabin. The...
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WO/2014/135844A1 |
A heat exchanger assembly (201) comprises: a hot fluid flow channel (210); a cold fluid flow channel (220); and a heat exchanger (230) disposed between the channels. The heat exchanger comprises a heat sink (240) and a thermoelectric dev...
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WO/2014/127899A1 |
The invention relates to a hybrid component and a method for producing the same. The hybrid component according to the invention comprises a base (2) having at least one portion that is a laminate (3) produced from a plastic foam and a f...
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WO/2014/131061A1 |
An aircraft comprises composite skin (120) having an opening, and a ventilation conduit (120) having an end portion (132) that extends to the opening in the composite skin. The conduit is made of metal except for the end portion (132), w...
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WO/2014/076391A1 |
The invention relates to an air conditioning system for the pressurized cabin of an aircraft. The system (1) comprises an air intake module (3) that is designed to draw in ambient air external to the aircraft, an air compression module (...
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WO/2014/072619A1 |
The invention relates to a method and to a device for determining, in real time, the flow rate of air collected from an aircraft engine (39) by a system (1) for collecting air from the engine, comprising: acquisition means (33) for acqui...
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WO/2014/070545A1 |
An air vehicle power and thermal management system (10) includes an aircraft controller (20) structured to distribute power provided by a gas turbine engine (36) between a cooling system (22) and an electrically powered load (14). The co...
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WO/2014/048731A1 |
The invention relates to a device for cooling a component (2) in a vehicle by means of a cooling air flow (4), wherein the device has at least one air inlet (11) and at least one air outlet (12), which are arranged such that the cooling ...
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WO/2014/044981A1 |
The invention relates to a body panel (1) for a transport vehicle — in particular for an aircraft — including a supporting plate (2) and a heat-exchange device (6), said supporting plate forming (2) on the outer surface (4) thereof f...
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WO/2014/041291A1 |
The invention relates to a method for supplying non-propulsive power of an aircraft, comprising driving a shaft (13) of a system (1) for controlling the environment of the aircraft by a combination of energy sources selected from: an aux...
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WO/2014/033052A1 |
Disclosed is a humidification device comprising a stacking unit with membranes which are permeable to water vapour, and with support frames which are stacked on top of one another and between which the membranes are clamped. An air inflo...
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WO/2014/033051A1 |
A moistening device has at least one stacking unit which contains a plurality of water-permeable membranes which are each enclosed at the edges by a frame. The frame is formed by a film composite with a lower film and an upper film, betw...
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WO/2014/030024A1 |
The present disclosure relates to a pre-cooler system comprising a pre-cooler (112) for cooling hot bleed air from an engine, and a bypass valve (204) for diverting at least a portion of the hot bleed air to bypass the pre-cooler (112). ...
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WO/2014/012746A1 |
The invention relates to an aircraft galley (1) comprising at least one cooling compartment (2) for receiving a container for foods and/or drinks to be cooled, characterized in that at the back of the galley (1) at least one first panel ...
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WO/2014/012742A1 |
The invention relates to an aircraft galley (1) comprising at least one cooling compartment (2) for receiving a container for foods and/or drinks to be cooled, characterized in that at the back of the galley (1) at least one panel (3) wi...
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WO/2014/001304A1 |
The present invention pertains to a heated floor panel (10) for an airborne vehicle (20) and an airborne vehicle having at least one heated floor panel. The floor panel comprises a controller housing (9), a first heated panel (6) configu...
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WO/2013/192047A1 |
An aircraft emergency oxygen dispensing device (19) includes an oxygen storage vessel (12) having a frangible pressure seal (14), and a manifold (16), a pressure regulator (18), one or more flow control valves (20) connected to the oxyge...
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WO/2013/180994A1 |
Provided herein is a hybrid system (100) for generating oxygen on¬ board an aircraft for passengers and/or flight crew to breath. The system includes a first chemical oxygen generator component (112) configured to promptly supply oxygen...
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WO/2013/176996A1 |
The present invention provides a system and method for supplying and managing oxygen suited for use on-board an aircraft for providing breathable oxygen to pilots and cockpit crew. Components of the system work together to optimize oxyge...
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WO/2013/149936A1 |
A Heat exchanger (100, 200, 300) comprises a plurality of heat transfer modules (10, 20, 30, 40) which are disposed side by side so as to define a multilayer body (102, 202, 302) of the heat exchanger (100, 200, 300), wherein each heat t...
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WO/2013/135534A1 |
The invention relates to a valve (10) for controlling the internal pressure in a cabin of an aircraft, comprising a first flap (12) and a second flap (14), which are supported in a frame (16), wherein the flaps (12, 14) control a fluid f...
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WO/2013/124344A1 |
The invention relates to an aircraft oxygen emergency device comprising a chemical oxygen generator (10), an oxygen supply line including a first line section (21) connecting said chemical oxygen generator with a flow regulator unit (20)...
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WO/2013/120764A1 |
A ventilation system (1) for an interior room (510) is provided, having a first air suction device (10), a second air suction device (20), a suction volume control device (30), a first air conduction pipe (11), a second air conduction pi...
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WO/2013/109332A1 |
A ventilation system for ventilating a passenger compartment of an aircraft is disclosed herein. The ventilation system includes, but is not limited to, a nozzle that is adapted to be mounted proximate an interior of the aircraft and tha...
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WO/2013/092727A1 |
A mixing device (10) that is particularly suitable for use in an aircraft air-conditioning system comprises a cold air supply line (12) adapted to supply cold air to the mixing device (10). A first recirculation air supply line (14) is a...
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WO/2013/092728A1 |
A storage assembly (10), which is in particular suitable for use in a cooling system designed for an operation with a two-phase coolant medium, comprises a storage container (12) with a receiving area (14) for receiving a coolant medium ...
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WO/2013/087813A1 |
A mixer assembly (10) for an air-conditioning system comprises a recirculation air line (12) and an air-conditioning air line (16). A first mixing region (20), is connected to the recirculation air line (12) and to the air-conditioning a...
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WO/2013/087534A1 |
Stated are a passenger compartment with an air distribution system for a means of transport (e.g. aircraft) and a corresponding method for regulating an air outlet temperature. In this arrangement the passenger compartment comprises a mu...
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WO/2013/083436A1 |
The present invention relates to a heating system (10) for an aircraft or spacecraft with a control device (5) which comprises at least one power line data transmission transceiver (5a; 5b) and one sensor controller (7), and at least one...
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WO/2013/079454A1 |
An on board inert gas generation system for an aircraft receives air from a relatively low pressure source such as low pressure engine bleed air or ram air and passes it to a positive displacement compressor (40) to increase the pressure...
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WO/2013/079100A1 |
An aircraft comprises a turbine engine (104) suspended from a wing (102) by means of a pylon (105). Compressed hot air is bled off from the turbine engine (104). A bleed air duct (209) in the wing (102) conveys the compressed hot air tow...
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WO/2013/075795A1 |
The invention relates to an arrangement for heating a portion of the cabin floor (1) in an aircraft cabin, said cabin floor (1) having an accessible upper face (O) and a lower face (U) which lies opposite the upper face. The arrangement ...
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WO/2013/072603A1 |
The invention relates to the optimised recovery of energy in an aircraft, at altitude and on the ground, using a single architecture. To this end, the invention aims to recover thermal energy from the exhaust. An architecture for the rec...
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WO/2013/067886A1 |
A refrigeration system (200) for aircraft is provided, which includes: a first stage heat exchanger (102) for receiving hot bleed air from an engine; a second stage heat exchanger (106) with an inlet communicated with an outlet of the fi...
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WO/2013/039904A1 |
An aircraft crew cabin rest area that is formed between the aircraft galley and a console, or between any two aircraft monuments, utilizing special folding and extendible doors and specialized locking means.
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WO/2013/023649A1 |
The invention relates to a device for conditioning of cabin air from a cabin space of an aircraft that has at least one lithium air battery (106), having a first feed line (101) by means of which ambient air can be delivered to the batte...
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WO/2012/164214A1 |
A system for conditioning the air of a passenger compartment (1) of an aircraft, the system comprising an air supply circuit connecting at least one exterior air inlet (E) to at least one air distribution outlet (S) opening into the comp...
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WO/2012/125895A1 |
An aircraft engine includes a precooler disposed within a nacelle. The precooler defines an ambient air passage and a bleed air passage. Air passes through the precooler from an ambient air inlet to an ambient air outlet. Bleed air passe...
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WO/2012/114022A1 |
The invention relates to an aircraft including at least one wall (66) defining a first area (I) of the aircraft that is thermally insulated from the outside of the aircraft, and a second area (E) of the aircraft that is not thermally ins...
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WO/2012/100542A1 |
Disclosed is a dehumidification system for use in an airplane, comprising： a cooling assembly (1) having an air inlet port (11) for a first round of dehumidification and an air outlet port (12) for the first round of dehumidification, ...
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WO/2012/095291A1 |
The invention describes a method and a device for determining an air mass flow flowing through a ram air channel (128). Disposed in the ram air channel (128) is a feed device (130) that is adapted in a first operating state of the ram ai...
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WO/2012/095646A1 |
A turboprop-powered medium altitude long endurance aircraft, comprising: a gas turbine engine (8); heat scavenging apparatus (44), for example a thermal blanket comprising capillary tubing,arranged to scavenge heat from the gas turbine e...
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WO/2012/095645A1 |
A method and apparatus for a turboprop-powered medium altitude long endurance (MALE) aircraft, comprising: a heat exchanger (51) comprising a heat-storage material, for example a heat-storage wax; and an air recirculation path (26); wher...
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WO/2012/045832A1 |
An air conditioning system (2) for an aircraft comprises at least one air conditioning pack (4) which for the purpose of heat dissipation can be connected to at least one cooling air inlet (42) of the aircraft and is designed to cool air...
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WO/2011/147977A9 |
A system (32) for air conditioning an aircraft cabin comprises at least one cooling circuit (40, 42), at least one compressed-air line (33) and at least one compressor (36) for compressing air. The cooling circuit (40, 42) is connected t...
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WO/2012/025687A2 |
The invention relates to limiting the specific consumption of an aircraft by matching the sizing of the power supply to the actual power needs of the cabin pressure control system, and more generally to that of the aircraft. According to...
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