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WO/2013/072603 |
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/2013/067886 |
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/2013/039904 |
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/2013/023649 |
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/2012/164214 |
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/2012/152934 |
The invention discloses a panel for being detachably arranged between a skin of a means of transport such as, e.g., an aircraft, a motor coach, a railway car or a ship cabin and an interior lining of the means of transport, wherein said ...
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WO/2012/125895 |
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/2012/114022 |
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/2012/100542 |
Disclosed is a dehumidification system for use in an airplane, comprisingļ¼ 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/2012/095645 |
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/2012/095646 |
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/2012/095291 |
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/2012/084209 |
A supply system (10) with a plurality of consumers (20a, 20b, 20n), which can be supplied with a minimum volumetric flow by the supply system (10) to ensure their operational function, wherein the supply system (10) exhibits: a network o...
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WO/2012/079756 |
A method for controlling an aircraft air conditioning system comprises the steps of detecting an operating state of an air conditioning unit (27) of the aircraft air conditioning system and controlling the temperature of a process air ma...
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WO/2012/065713 |
An aircraft outer skin heat exchanger (10) comprises a first cooling air inlet (14) and a first cooling air duct section (18), in which a first heat carrier fluid duct section (26) is arranged. A cooling air conveying device (24) is conf...
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WO/2012/045832 |
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/2012/025687 |
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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WO/2012/025687 |
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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WO/2012/025688 |
The aim of the invention is to remove the mechanical bleed constraints in the engines during the transient flight phases of an aircraft in order to optimize the operability of the engine assembly during said phases. To this end, a supply...
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WO/2012/022758 |
The invention pertains to an air-conditioning system for an aircraft. The air-conditioning system comprises a compressed air branch for conveying externally supplied and pressurized air, preferably bleed air. Furthermore, a cooling circu...
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WO/2012/019796 |
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...
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WO/2011/147977 |
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/2011/147977 |
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/2011/143662 |
A method for searching for airline travel based upon seat characteristics specified, by a traveler is disclosed. Travel information is received indicating an origin, a destination, one or more travel dates and one or more seat characteri...
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WO/2011/134614 |
The invention relates to a service supply system (10) for supplying passengers in a passenger compartment of a vehicle, in particular an aircraft, comprising a service supply line (12) and a number of service supply modules (14) which ca...
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WO/2011/134614 |
The invention relates to a service supply system (10) for supplying passengers in a passenger compartment of a vehicle, in particular an aircraft, comprising a service supply line (12) and a number of service supply modules (14) which ca...
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WO/2011/134615 |
The invention relates to a support structure (10) for use in an air supply arrangement for air conditioning passenger compartments in aircraft. Said air supply arrangement comprises at least one centrally controlled cabin ventilator and ...
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WO/2011/133603 |
An interior ceiling panel system (10) includes a ceiling panel (38) mounted in a ceiling area (14), a first airflow directing panel (44) in a first side of the ceiling area defining an airflow passage, and a second airflow directing pane...
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WO/2011/133603 |
An interior ceiling panel system includes a ceiling panel mounted in a ceiling area, a first airflow directing panel in a first side of the ceiling area defining an airflow passage, and a second airflow directing panel in a second side o...
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WO/2011/124390 |
A mixer assembly (10) for an aircraft air conditioning system comprises a plurality of fresh air lines (12, 18), which are adapted to be flowed through with cold fresh air during operation of the mixer assembly (10), and a plurality of r...
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WO/2011/124361 |
The invention relates to a compressor/turbine arrangement (10) for use in an air conditioning unit (200) of an aircraft air conditioning system comprising a process air supply line (12) which is designed to supply process air generated b...
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WO/2011/124390 |
A mixer assembly (10) for an aircraft air conditioning system comprises a plurality of fresh air lines (12, 18), which are adapted to be flowed through with cold fresh air during operation of the mixer assembly (10), and a plurality of r...
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WO/2011/125030 |
A glider 10 comprises a body 12, a closed cockpit 18 and an air extractor 22 for extracting air from the cockpit. The extractor is mounted on the body in a region of negative pressure relative to general ambient or atmospheric pressure, ...
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WO/2011/124391 |
A mixing device (10) for an aircraft air conditioning system comprises a plurality of cold-air supply lines (12, 14), which are devised to supply cold air to the mixing device (10). A plurality of warm-air supply lines (16, 18) is furthe...
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WO/2011/124391 |
A mixing device (10) for an aircraft air conditioning system comprises a plurality of cold-air supply lines (12, 14), which are devised to supply cold air to the mixing device (10). A plurality of warm-air supply lines (16, 18) is furthe...
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WO/2011/117142 |
The invention relates to an aircraft having at least one air supply channel (14) and at least one exhaust air channel (15) and at least one seat (2) comprising at least one seat frame (25) by means of which the seat is fastened to a part...
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WO/2011/117142 |
The invention relates to an aircraft having at least one air supply channel (14) and at least one exhaust air channel (15) and at least one seat (2) comprising at least one seat frame (25) by means of which the seat is fastened to a part...
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WO/2011/101211 |
The invention relates to an inlet air system for passengers in a passenger compartment, wherein the inlet air duct need not be modified in the event of a change in the seating configuration. This is ensured by means of an air distributin...
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WO/2011/082983 |
The present invention relates to sound damping of air conditioning systems in an aircraft. The invention in particular relates to an air conditioning air duct for an aircraft, and to an aircraft having air conditioning air ducts. In orde...
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WO/2011/082983 |
The present invention relates to sound damping of air conditioning systems in an aircraft. The invention in particular relates to an air conditioning air duct for an aircraft, and to an aircraft having air conditioning air ducts. In orde...
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WO/2011/071602 |
A device for producing electrical power. A thermoelectric device is coupled to an aircraft bleed system for generating electrical power using temperature differentials between ram air and bleed air.
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WO/2011/071602 |
A device for producing electrical power. A thermoelectric device is coupled to an aircraft bleed system for generating electrical power using temperature differentials between ram air and bleed air.
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WO/2011/056285 |
An aircraft system for improved cooling efficiency comprises at least one air conditioning pack (44), coupled to an aircraft, having at least one air compression device (50) powered by at least one power source (62) and having an air com...
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WO/2011/038889 |
A system (10) for cooling and/or heating aircraft devices to be cooled and/or heated comprises a first individual cooling and/or heating system (20, 22) associated with a first aircraft device (12, 14) to be cooled and/or heated, and a s...
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WO/2011/038889 |
A system (10) for cooling and/or heating aircraft devices to be cooled and/or heated comprises a first individual cooling and/or heating system (20, 22) associated with a first aircraft device (12, 14) to be cooled and/or heated, and a s...
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WO/2011/038889 |
A system (10) for cooling and/or heating aircraft devices to be cooled and/or heated comprises a first individual cooling and/or heating system (20, 22) associated with a first aircraft device (12, 14) to be cooled and/or heated, and a s...
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WO/2011/038888 |
A system (10) for controlling a cooling system (100) for use especially on board an aircraft comprises a operating state detection unit (30) that is designed to detect operating state signals characteristic of the operating state of the ...
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WO/2011/038888 |
A system (10) for controlling a cooling system (100) for use especially on board an aircraft comprises a operating state detection unit (30) that is designed to detect operating state signals characteristic of the operating state of the ...
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WO/2011/038888 |
A system (10) for controlling a cooling system (100) for use especially on board an aircraft comprises a operating state detection unit (30) that is designed to detect operating state signals characteristic of the operating state of the ...
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WO/2011/036255 |
The invention relates to a regulating system (2) for regulating the cabin pressure P C of an airplane (4), comprising at least one cabin pressure regulating unit (6), which is equipped, by controlling at least one air removal or air supp...
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