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Matches 151 - 200 out of 1,579

Document Document Title
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...  
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...  
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 ...  
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...  
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...  
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...  
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...  
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...  
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 ...  
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...  
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...  
WO/2012/152934A3
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 ...  
WO/2008/144295A3
Systems and methods for providing airflow in an aerospace vehicle are disclosed. A system in accordance with one embodiment includes an aerospace vehicle having an interior volume with a first portion and a second portion. The system can...  
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.  
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...  
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...  
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...  
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...  
WO/2012/084209A3
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...  
WO/2012/079756A3
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...  
WO/2012/065713A3
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...  
WO/2012/100542A1
Disclosed is a dehumidification system for use in an airplane, comprisingļ¼š 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, ...  
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...  
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...  
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...  
WO/2012/025687A3
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...  
WO/2011/117142A3
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...  
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...  
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...  
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...  
WO/2012/025688A1
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...  
WO/2012/022758A1
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...  
WO/2011/124391A8
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...  
WO/2012/019796A1
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...  
WO/2011/147977A3
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...  
WO/2011/134615A3
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 ...  
WO/2011/134614A3
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...  
WO/2011/124390A8
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...  
WO/2011/133603A3
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...  
WO/2011/124391A3
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...  
WO/2011/143662A1
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...  
WO/2011/134614A2
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...  
WO/2011/133603A2
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...  
WO/2011/082983A3
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...  
WO/2011/124390A1
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...  
WO/2011/125030A1
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, ...  
WO/2011/124361A1
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...  
WO/2011/117142A2
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...  
WO/2011/036255A3
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...  
WO/2011/038889A8
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...  

Matches 151 - 200 out of 1,579