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Matches 301 - 350 out of 1,582

Document Document Title
WO/2009/093916A2
The subject of the invention is a group of new derivatives of aminoalkaÏ€ols, more specifically [(phenoxy)alkyl]aminoalkanols and [(phenoxy)acyl)aminoalkanols, their method of obtaining and their use for production of a medicine which is...  
WO/2009/068265A4
The invention relates to an energy supply system for operating at least one air conditioning system (26) of an aircraft, with at least one air line network and at least one electric line network, wherein the air line network is connected...  
WO/2009/090026A1
An air-conditioning system for an aircraft for the individual temperature control of regions (28, 30, 32, 34) of a cabin (28) of an aircraft, comprises a central air-conditioning device (2), which provides a pressurised and temperature-c...  
WO/2009/083558A2
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...  
WO/2009/080168A1
The invention relates to an aircraft cooling system (10) comprising a cooling element (12) that comprises a housing (14), a cooling air inlet (18) that is embodied in the housing (14) and a plurality of heat exchangers (32, 34, 36, 38) t...  
WO/2009/007094A3
The present invention relates to an air conditioning system (10) for an aircraft cabin (12) with at least one air inlet (14) for supplying air to the cabin (12), at least one air outlet (16) for discharging air from the cabin (12) and at...  
WO/2009/073034A1
A comfort HVAC or refrigeration system includes a remote sensor for sensing an environmental condition within a climate-controlled space and having, an associated transmitter for sending, a wireless signal to a receiver of a controller s...  
WO/2009/053002A3
The invention relates to a system for air conditioning at least one partial region of an airplane, comprising an air supply device (18) for providing a region of the airplane that is to be ventilated with a desired temperature and with a...  
WO/2009/068265A1
The invention relates to an energy supply system for operating at least one air conditioning system (26) of an aircraft, with at least one air line network and at least one electric line network, wherein the air line network is connected...  
WO/2009/050006A3
The invention relates to a system for providing emergency oxygen and therapeutic oxygen in an aircraft, said system having an oxygen source (10), an oxygen conduction system (20) comprising a second oxygen outlet (21), a device for provi...  
WO/2009/064288A1
Aircraft environmental control systems having a single ram air inlet (201) providing air to both cabin compressors (204a, 204b) and associated heat exchangers are disclosed herein. In one embodiment, and environmental control system for ...  
WO/2009/053002A2
The invention relates to a system for air conditioning at least one partial region of an airplane, comprising an air supply device (18) for providing a region of the airplane that is to be ventilated with a desired temperature and with a...  
WO/2009/050006A2
The invention relates to a system for providing emergency oxygen and therapeutic oxygen in an aircraft, said system having an oxygen source (10), an oxygen conduction system (20) comprising a second oxygen outlet (21), a device for provi...  
WO/2009/019264A3
The invention relates to a valve for controlling a fluid flow from a first environment to a second environment, having a frame for disposing a separating element in the region of an opening, said element separating the first environment ...  
WO/2009/042322A1
One embodiment of a pressure management system for an aircraft may include a cavity (24), an opening (46) in a surface of the cavity, and a moveable door (42). An interior area within the cavity may have an interior pressure and an exter...  
WO/2009/040389A1
The invention relates to an outlet valve (10) for an airplane, having a frame (12) for arranging in an opening (14) of an outer skin (16) of the airplane, a first cover (18) pivotally disposed in the frame (12) for controlling a flow cro...  
WO/2008/115273A3
A tandem inlet apparatus (10) for use with a high speed mobile platform, for example a commercial or military aircraft. The tandem inlet apparatus includes a Pitot inlet (102) for feeding air to a cabin air compressor (CAC) of an air con...  
WO/2009/032497A1
Aircraft cabin airflow nozzles and associated systems and methods are disclosed. A system in accordance with a particular embodiment includes a cabin air nozzle (220) that in turn has a first passageway (223a) bounded at least in part by...  
WO/2008/143696A3
Ram air inlets for use with aircraft environmental control systems and other aircraft and non-aircraft systems are described herein. In one embodiment, a ram air inlet (201) configured in accordance with the present invention includes an...  
WO/2009/019264A2
The invention relates to a valve for controlling a fluid flow from a first environment to a second environment, having a frame for disposing a separating element in the region of an opening, said element separating the first environment ...  
WO/2008/148973A3
The subject of the invention is an air outlet device fitted with a grid (10) fitted to an aerodynamic surface of an aircraft, wherein said grid comprises a plurality of openings defined by intermediate zones extending away from the aerod...  
WO/2009/007094A2
The present invention relates to an air conditioning system (10) for an aircraft cabin (12) with at least one air inlet (14) for supplying air to the cabin (12), at least one air outlet (16) for discharging air from the cabin (12) and at...  
WO/2008/138930A3
According to an exemplary embodiment of the invention an oxygen supply system for an aircraft is provided, wherein the said system comprises a control valve (5), a reservoir bag (3), a respiration device (1) and a sensor device (22), whe...  
WO/2008/148973A2
The subject of the invention is an air outlet device fitted with a grid (10) fitted to an aerodynamic surface of an aircraft, wherein said grid comprises a plurality of openings defined by intermediate zones extending away from the aerod...  
WO/2008/143696A2
Ram air inlets for use with aircraft environmental control systems and other aircraft and non-aircraft systems are described herein. In one embodiment, a ram air inlet (201) configured in accordance with the present invention includes an...  
WO2008116628B1
A system (10) for cooling freight goods on board an aircraft comprises a refrigerating apparatus and a cooling station (14) to which cooling energy generated by said refrigerating apparatus is fed by means of a refrigerating medium and w...  
WO/2008/138846A2
A method and an apparatus for initiating a run-up procedure for a jet engine to avoid engine icing, the method comprising the following steps of providing at least one surface element that is made of a material suitable for ice in atmosp...  
WO/2008/138930A2
According to an exemplary embodiment of the invention an oxygen supply system for an aircraft is provided, wherein the said system comprises a control valve (5), a reservoir bag (3), a respiration device (1) and a sensor device (22), whe...  
WO/2008/140972A1
A cooling system for removing heat generated by electrical components (28) onboard aerospace vehicles flows coolant between an evaporator that removes heat from the component, and a condenser (52) within the skin (22,24) of the vehicle. ...  
WO/2008/118973A3
A method for manufacturing a wall of a thin- walled structure is described. The method includes receiving parameters for the wall and one or more stiffening features associated with the wall via a user interface, providing the parameters...  
WO/2008/135449A1
The invention relates to an aircraft including a cabin, in which the first parts of multiple multi-system connection devices are secured to at least one wall of the cabin. Each of said devices includes a male part or plug (80) and a fema...  
WO/2008/116628A1
A system (10) for cooling freight goods on board an aircraft comprises a refrigerating apparatus and a cooling station (14) to which cooling energy generated by said refrigerating apparatus is fed by means of a refrigerating medium and w...  
WO/2008/116862A1
A supply channel (1) with an air distribution system for vehicles, in particular for aircraft, is presented. The supply channel comprises an elongated housing (3), a hollow profile (5) extending in longitudinal direction of the housing, ...  
WO/2008/118973A2
A method for manufacturing a wall of a thin- walled structure is described. The method includes receiving parameters for the wall and one or more stiffening features associated with the wall via a user interface, providing the parameters...  
WO/2008/115273A2
A tandem inlet apparatus (10) for use with a high speed mobile platform, for example a commercial or military aircraft. The tandem inlet apparatus includes a Pitot inlet (102) for feeding air to a cabin air compressor (CAC) of an air con...  
WO/2008/112029A1
There is provided systems and methods for transporting heat away from galley refrigeration equipment (10) or other heat-generating systems such as avionics, power electronics, or in-flight entertainment units, via a potable water system ...  
WO/2008/101986A1
The present invention relates to a fuselage (1) of an aircraft or spacecraft, with at least one shell element (2) and a structural element (7). An interspace (5; 9) to which air can be admitted by an air stream (10) is provided between t...  
WO2008071319B1
An aircraft cooling system (1) according to the invention comprises a first coolant stream (4a) which cools at least one first heat load (2a), and a second coolant stream (4b) which cools at least one second heat load (2b), wherein the a...  
WO2008008324A9
There is provided systems and methods for transporting heat away from galley refrigeration equipment (12) or other heat-generating systems such as avionics, power electronics, or in-flight entertainment units, via a potable water system ...  
WO/2008/074433A1
The invention concerns a cooling system for an aircraft with an air inlet (4) through which air from the environment of the aircraft enters a ram air channel (2), and an air outlet (6) through which air emerges from the ram air channel (...  
WO/2008/071319A1
An aircraft cooling system (1) according to the invention comprises a first coolant stream (4a) which cools at least one first heat load (2a), and a second coolant stream (4b) which cools at least one second heat load (2b), wherein the a...  
WO/2008/065709A1
In supplying conditioned air in an airplane, conditioned air in which at least one of oxygen concentration and humidity has been regulated is produced in the airplane. The produced conditioned air is blown out through a plurality of air ...  
WO2007147259A9
Devices and systems are provided, that entrain ambient air within a primary stream of pressurised air, for use in a variety of applications including aircraft, buildings and other stationary structures. The ambient air is drawn through a...  
WO/2008/061712A1
The invention discloses the multistage cooling of an aircraft electronic system (2) with at least one electronic component which delivers heat. The multistage feature results from the use of a plurality of circuits for transferring the w...  
WO2008025462A8
A cooling system (10) for cooling heat loads (28, 34) on board an aircraft comprises a cold producing device (12), a first cold carrier fluid circuit (24), which is thermally coupled to the cold producing device (12) and is connected to ...  
WO/2008/061713A1
A cooling system (10) for cooling an aircraft device (12) comprises an evaporator (14, 16, 18) for receiving a fluid (F) which is to be evaporated, a first adsorber (24) which contains a medium (28) for the adsorption of the fluid (F) wh...  
WO/2008/055607A1
The present invention relates to a cooling device (20) for installation in an aircraft, in particular a passenger aircraft. The cooling device (20) comprises a heat exchanger (26) configured for flow-through of a liquid coolant for pre-c...  
WO/2008/043568A1
The present invention relates to an arrangement for deicing pipeline connections of an aircraft, which are connected to all fresh air outlets of an air conditioner, whose construction comprises the functions of multiple turbines and heat...  
WO2008017427B1
Aircraft air-conditioning system (1) for an aircraft having a plurality of zones (2, 4), comprising a first line (6) for feeding cold air at an actual temperature T1act., a second line (14) which branches off a portion of the air from th...  
WO/2008/034215A1
An air/oil separator (10 or 40) for use in a gas turbine engine comprises a labyrinth path (14 or 44) having an air/oil inlet (16 or 46), air outlet (18 or 48) and oil outlet (20 or 50), means (22, 24, 30 or 52, 54, 60) or creating an el...  

Matches 301 - 350 out of 1,582