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Patent Searching and Data


Matches 251 - 300 out of 1,623

Document Document Title
WO/2010/057548A8
The invention relates to a method for emergency ventilation of an aircraft cabin (12), wherein a leak in the area of an air mixer (24) of an aircraft air conditioner (16) is detected. An emergency air valve (38) preventing exchange of ai...  
WO/2010/094392A1
The invention relates to an air conditioner (10) comprising a fresh air line (12) connected to a fresh air inlet (14) for feeding fresh air to the air conditioner (10), and an adsorption device (16) disposed in the fresh air line (12) co...  
WO/2010/051920A3
The invention relates to a method for emergency ventilation of an aircraft cabin (36), comprising controlling a first valve (14) arranged in a first aircraft fuselage area (28), said valve serving as an air outlet valve of an aircraft ca...  
WO/2010/057744A3
According to one embodiment of the invention, a supply unit (100) to be mounted on a supply channel (200) of an aircraft is provided, comprising a fastening device (105, 106) and a connecting device (107). Both devices interact such that...  
WO/2009/141400A4
The invention relates to an inerting system for an aircraft, comprising at least one air separation module provided with at least one air inlet, a first air outlet and a second air outlet. Said air separation module is designed in such a...  
WO/2010/080483A2
Air treatment catalyst systems and methods for treating the air in the aircraft cabin environment are provided. The catalyst system and method remove ozone, volatile organic compounds, NOx and other pollutants. The catalyst system used t...  
WO/2010/012415A4
The invention relates to a system (10) for air-conditioning an aircraft cabin (12), said system comprising an air-conditioning unit (14) connected to a central mixer (16) in order to supply the central mixer (16) with air at a desired lo...  
WO/2010/051919A4
The invention relates to a system (10) for cooling a heat exchanger (12) on board an aircraft, comprising a process air line (28) whose first end is connected to an engine (16) of the aircraft in order to supply the process air line (28)...  
WO/2010/049060A4
A system (10) for air conditioning an aircraft cabin (12) comprises an air-conditioning unit (14), which is connected to a central mixer (16) to supply air at a desired low temperature to the central mixer (16). A first recirculation sys...  
WO/2010/066440A2
The invention relates to an emergency power system for an aircraft, comprising at least one fuel cell unit for generating electricity. Said fuel cell unit is cooled using at least one cooling cycle encompassing at least one heat exchange...  
WO/2010/012416A4
The invention relates to a system (10) for pumping recirculation air from an aircraft cabin, said system comprising a plurality of pumping devices (12a-12j) distributed along an aircraft cabin region (14). A control device (16) is design...  
WO/2010/012415A3
The invention relates to a system (10) for air-conditioning an aircraft cabin (12), said system comprising an air-conditioning unit (14) connected to a central mixer (16) in order to supply the central mixer (16) with air at a desired lo...  
WO/2010/057548A1
The invention relates to a method for emergency ventilation of an aircraft cabin (12), wherein a leak in the area of an air mixer (24) of an aircraft air conditioner (16) is detected. An emergency air valve (38) preventing exchange of ai...  
WO/2010/032250A3
The present invention discloses a direct current (DC)-based air conditioner. The air conditioner comprises: At least one DC source; At least one internal DC motor; At least one external DC motor; At least one battery coupled to the at le...  
WO/2010/051919A1
The invention relates to a system (10) for cooling a heat exchanger (12) on board an aircraft, comprising a process air line (28) whose first end is connected to an engine (16) of the aircraft in order to supply the process air line (28)...  
WO/2010/051920A2
The invention relates to a method for emergency ventilation of an aircraft cabin (36), comprising controlling a first valve (14) arranged in a first aircraft fuselage area (28), said valve serving as an air outlet valve of an aircraft ca...  
WO/2010/049147A1
An adsorption cooling system (1) for an aircraft, comprises an evaporator (18), a first adsorber (2), with a first adsorbent for adsorbing an adsorbent coolant evaporated in the evaporator (18) and an second adsorber (4), containing a se...  
WO/2009/153011A4
An intersecting element (10) for connecting a first section of an aircraft supply system, which section is provided on an aircraft interior equipment component (12), to a second section of the aircraft supply system comprises a support s...  
WO/2010/049060A1
A system (10) for air conditioning an aircraft cabin (12) comprises an air-conditioning unit (14), which is connected to a central mixer (16) to supply air at a desired low temperature to the central mixer (16). A first recirculation sys...  
WO/2010/003640A3
A system (10) for cooling an aircraft zone comprises an air-conditioning unit (12a, 12b) for supplying cool air, a device (20a, 20b) conducting circulating air, and a mixing chamber (18) which is connected to the air-conditioning unit (1...  
WO/2009/141400A3
The invention relates to an inerting system for an aircraft, comprising at least one air separation module provided with at least one air inlet, a first air outlet and a second air outlet. Said air separation module is designed in such a...  
WO/2010/040434A1
The invention relates to an air guiding element (10) for an aircraft air-conditioning system, comprising a distributor pipe (12) having an air inlet opening (14) in the region of a front face of the distributor pipe (12) and an air disch...  
WO/2010/012416A3
The invention relates to a system (10) for pumping recirculation air from an aircraft cabin, said system comprising a plurality of pumping devices (12a-12j) distributed along an aircraft cabin region (14). A control device (16) is design...  
WO/2010/034750A2
The invention relates to a power distribution system (2), for an aircraft with at least one engine (8, 10), comprising at least one torque transmission means (4, 6), with a movable bearing and connected to at least one shaft of the engin...  
WO/2009/146843A4
The invention relates to a cooling system (10) for cooling a device (14) subjected to heat in a vehicle, particularly an aircraft, comprising a cooling circuit (12) permeated by a heat-carrying fluid and thermally coupled to the device (...  
WO/2010/026024A2
The invention relates to an air conditioning system for a transportation means, having multiple zones (20) to be air-conditioned, which may be variably air-conditioned by means of processed supply air in combination with individual trim ...  
WO/2009/153011A3
An intersecting element (10) for connecting a first section of an aircraft supply system, which section is provided on an aircraft interior equipment component (12), to a second section of the aircraft supply system comprises a support s...  
WO/2010/021791A1
Apparatus and methods described herein provide for the management of noise associated with a duct. A sound-dampening apparatus (100) is provided consisting of a duct (102) through which a fluid flows, such as an air duct. A flexuous cord...  
WO/2010/019732A2
The present invention provides a combination vepntilation 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 comp...  
WO/2010/015361A2
In order to increase the humidity in a cabin region (10) of an airplane equipped with a plurality of seats (16; 28), a device (12; 14) is provided, comprising a plurality of humidifying units (26) arranged in spatial association with a p...  
WO/2010/012416A2
The invention relates to a system (10) for pumping recirculation air from an aircraft cabin, said system comprising a plurality of pumping devices (12a-12j) distributed along an aircraft cabin region (14). A control device (16) is design...  
WO/2010/012684A1
The invention relates to a heat exchanger (70) for an outer skin (4) of an aircraft, comprising at least one feed line (80) for a coolant, at least one discharge line (82) for the coolant and at least one bundle of coolant channels (76) ...  
WO/2010/012415A2
The invention relates to a system (10) for air-conditioning an aircraft cabin (12), said system comprising an air-conditioning unit (14) connected to a central mixer (16) in order to supply the central mixer (16) with air at a desired lo...  
WO/2010/011153A1
The invention relates to airplanes lighter than air and can be used for producing highly efficient airships. The inventive airship comprises a permanent volume section which is filled with a helium and oxygen mixture in a breathable prop...  
WO/2009/144234A4
The invention relates to a fresh air inlet for an aircraft, comprising at least one ram air inlet (20) with at least one ram air inlet opening (36), at least one additional air inlet opening (26), situated at a distance from the ram air ...  
WO/2010/003640A2
A system (10) for cooling an aircraft zone comprises an air-conditioning unit (12a, 12b) for supplying cool air, a device (20a, 20b) conducting circulating air, and a mixing chamber (18) which is connected to the air-conditioning unit (1...  
WO/2009/120308A3
In an example embodiment, a vehicle seating arrangement includes a fore-facing lower seat convertible between a sitting position and a lie flat sleeping position in a lower horizontal plane, an aft-facing lower seat convertible between a...  
WO/2009/156120A2
The invention relates to an air duct (10) for supplying ambient air in an aircraft, comprising an air inlet (12), a duct channel section (16) extending downstream of the air inlet (12) and an air conveying device (22) which is adapted to...  
WO/2009/127652A3
The invention relates to a de-icing system for an aircraft, comprising at least one heat source (28) and at least one air discharging means (23) for discharging air in areas of the aircraft to be de-iced. The invention is characterized i...  
WO/2009/153033A2
The invention relates to an aircraft conduit monitoring system comprising a conduit that conducts gas from a source to a point of application. A flow sensing device and a pressure sensing device are provided within the conduit. At least ...  
WO/2009/149904A2
An aircraft system carrier element (10) comprises a base body (12) made of a sound- and heat-insulating material, in which a climate channel (14), which is provided for supplying an aircraft compartment (22) and can be connected to an ai...  
WO/2009/150223A1
The present invention relates to a system for oxygen supply to persons in an aircraft. In order to provide as simple a system as possible that is suitable in particular for a reconfiguration of the seat devices (12), the system comprises...  
WO/2009/100897A8
The invention relates to a system (10) for ventilating an explosive region (12) of an aircraft, comprising a ram air channel (16), which has an air inlet for supplying ambient air into the ram air channel (16), and an air outlet (18). Th...  
WO/2009/147161A1
The present invention provides an air inlet valve (2) for an airplane and a manufacturing method for an air inlet valve. The air inlet valve has an opening area (6) for ambient air (3) to pass therethrough to a internal fuselage area (7)...  
WO/2009/111677A3
Air treatment systems including an environmental control system, a mixer, an air distribution duct system, and one or more catalysts for treating the air in the aircraft cabin environment are provided. Methods for treating aircraft cabin...  
WO/2009/146843A1
The invention relates to a cooling system (10) for cooling a device (14) subjected to heat in a vehicle, particularly an aircraft, comprising a cooling circuit (12) permeated by a heat-carrying fluid and thermally coupled to the device (...  
WO/2009/144234A1
The invention relates to a fresh air inlet for an aircraft, comprising at least one ram air inlet (20) with at least one ram air inlet opening (36), at least one additional air inlet opening (26), situated at a distance from the ram air ...  
WO/2009/144162A1
A device for cooling exhaust air of aircraft air-conditioning systems (10), with a bypass duct (20) which bypasses an aircraft air-conditioning system, which is arranged downstream of a ram air duct (30) with a ram air inlet duct section...  
WO/2009/143954A1
A system (10) for ventilating 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) through which the flow can pass parallel to the first ra...  
WO/2009/083558A4
The invention relates to a system for the prevention of icing in a conduit, as can occur in, for example, a conduit of an aircraft air conditioner. The system according to the invention has at least one sensor (10) for detecting mechanic...  

Matches 251 - 300 out of 1,623