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Patent Searching and Data


Matches 201 - 250 out of 1,580

Document Document Title
WO/2011/038888A8
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 ...  
WO/2011/101211A1
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...  
WO/2011/071602A3
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.  
WO/2011/026844A3
A system (2) for cooling at least one heat‑producing device (4) in an aircraft has at least one coolant circuit. A coolant absorbs heat from the heat‑producing device (4), and dissipates heat via a heat dissipation apparatus (8) to t...  
WO/2011/003723A3
The invention relates to a system for cooling a device (20) emitting heat in a vehicle having a body (2), a passenger cabin (6), and a region (8) outside of the passenger cabin (6) and pneumatically connected thereto, comprising at least...  
WO/2011/082983A2
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/2011/038889A3
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...  
WO/2011/038888A3
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 ...  
WO/2011/018381A3
An aircraft comprises an outer aerodynamic surface and an exhaust duct having an opening in the outer aerodynamic surface. The duct has a duct wall curved at the opening so as to blend with the aerodynamic surface downstream of the duct....  
WO/2010/149267A3
The invention relates to a method for operating an aircraft cooling system (10), comprising the steps: feeding a coolant medium through a cooling circuit (26) which is coupled to a chiller (12) and to at least one cold energy consumer (1...  
WO/2011/071602A2
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.  
WO/2011/056285A1
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...  
WO/2011/038889A2
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...  
WO/2011/038888A2
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 ...  
WO/2011/036255A2
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/2011/033525A2
A system and method for an adaptable oxygen regulator with an electronic control device is disclosed. In one embodiment, an oxygen regulator system includes an electronic control device which includes a non-volatile memory for storing a ...  
WO/2011/026844A2
A system (2) for cooling at least one heat‑producing device (4) in an aircraft has at least one coolant circuit. A coolant absorbs heat from the heat‑producing device (4), and dissipates heat via a heat dissipation apparatus (8) to t...  
WO/2010/026024A4
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/2011/018381A2
An aircraft comprises an outer aerodynamic surface and an exhaust duct having an opening in the outer aerodynamic surface. The duct has a duct wall curved at the opening so as to blend with the aerodynamic surface downstream of the duct....  
WO/2010/026024A3
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/2011/003344A1
The transport tool with epidemic prevention function comprises a vehicle body, a drive mechanism and an operating mechanism. An air/environment sterilizing device with epidemic prevention function is provided in the vehicle body. An air ...  
WO/2010/149494A1
A flow restrictor (2) has a line piece (4) with an air inlet (6) and with an air outlet (8), and has at least one resistance element (10, 32, 36). The resistance element (10, 32, 36) is positioned within the line piece (4) and imparts a ...  
WO/2010/108842A4
The invention relates to an aeroplane structure comprising hollow supporting structural elements (100, 101, 102) forming an aeroplane fuselage (11), the cavities in the structural elements being embodied as air guiding shafts (103) for t...  
WO/2010/141254A1
A modular air conditioning (AC) system including one or more AC modules is provided. The AC modules may be adapted to function individually or cooperatively as part of a modular system. The AC modules may be further adapted to connect in...  
WO/2010/121984A1
A system for cooling a space in a vehicle comprises a sorption wheel (4), at least one heat exchanger (8), at least a first humidifier unit (10) and at least one fuel cell (6), wherein the sorption wheel (4) is adapted for drying ambient...  
WO/2010/051920A4
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/2010/108842A1
The invention relates to an aeroplane structure comprising hollow supporting structural elements (100, 101, 102) forming an aeroplane fuselage (11), the cavities in the structural elements being embodied as air guiding shafts (103) for t...  
WO/2010/111284A1
A method and apparatus are provided for detecting a temperature of a cabin within an airplane. The method includes the steps of providing a temperature sensor, enclosing the temperature sensor within an enclosure, coupling an inlet of th...  
WO/2010/106520A2
A preconditioned air unit for supplying preconditioned air to an aircraft parked on the ground, the preconditioned air unit comprising a housing accommodating a flow duct with an air inlet for ambient air and an air outlet for connection...  
WO/2010/106510A2
A preconditioned air unit for supplying preconditioned air to an aircraft parked on the ground, the preconditioned air unit comprising a main unit with a housing accommodating a flow duct with an air inlet for ambient air and an air outl...  
WO/2010/057744A4
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/2010/080483A3
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/2010/097181A1
A system for cooling an aircraft zone comprises a mixing chamber (18), which is connected to an air-conditioning unit (12a, 12b) for providing cool air and a circulating air delivery device (20a, 20b) for feeding circulating air to the m...  
WO/2009/102524A8
A class divider for an aircraft passenger cabin is provided. The class divider includes a partition positioned immediately aft of a rear row of seats in a first predetermined class area of the aircraft cabin and an aft-facing panel havin...  
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...  

Matches 201 - 250 out of 1,580