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Patent Searching and Data


Matches 351 - 400 out of 1,618

Document Document Title
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...  
WO/2008/031510A1
The invention relates to an air supply system of an aircraft, in particular of a passenger aircraft, which comprises a fresh air system, through which fresh air can be supplied to an aircraft cabin, a circulating air system, which is cou...  
WO/2008/030097A1
The invention pertains to use of a low-temperature ozone conversion means containing an ozone catalyst composition supported on a honeycomb structure in cabin conditioning and/or inerting fuel tanks. The ozone conversion means preferably...  
WO/2008/025462A1
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/2008/008324A3
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 ...  
WO2007147259B1
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/2008/022752A1
A frame element (10; 10') for use in an aircraft air-conditioning system is attachable to an aircraft structure (36) and includes at least one strut (12, 14, 16, 18; 12', 14', 16') which is formed at least in sections as a hollow cylinde...  
WO/2008/017427A1
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/2008/014912A1
An aircraft air-conditioning unit (10) includes a compressor (18) and a motor (20) driving the compressor (18). A fuel cell system (24) is connected directly to a control unit (22) for controlling the motor (20) driving the compressor (1...  
WO/2008/008324A2
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/2007/147259A1
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/2007/134858A1
The invention relates to a device for the improvement of individual comfort and the reduction of health problems in an airplane, which is arranged between the roof paneling of the cabin and a passenger and which has a surface facing the ...  
WO/2007/134749A1
The present invention relates to a wiring arrangement (50) for protecting a bleed air supply system (10) of an aircraft against overheating, the bleed air supply system (10) comprising a bleed air source (12), a bleed air feed (14), a sh...  
WO/2007/130051A1
A climate control system (10) includes an outdoor unit (14) and an indoor unit (12) having at least two fans (26,28). The fans (26,28) include control wiring (38,40) that is interchangeably connected to a control system (20), and feedbac...  
WO/2005/094346A3
In the improved cooling system for a commercial aircraft galley, heat is transferred from a galley food cart by a point-of-use heat exchange system to a liquid cooled condenser. Liquid coolant for the liquid cooled condenser is circulate...  
WO/2007/118494A1
The invention relates to a respiratory gas supply circuit for an aircraft carrying passengers, comprising a pressurized source of respiratory gas (R1, R2) and a supply line (2, 3), said circuit further comprising on said supply line a re...  
WO/2007/115830A1
A system (10, 10') for cooling items of freight on board an aircraft includes a refrigerating device and also a cooling station (14, 14') to which cooling energy generated by the refrigerating device is supplied by means of a refrigerant...  
WO/2007/115810A1
The invention relates to a device (30) for mixing fresh air (2) and heating air (4) which comprises a fresh air inlet (32, 42), a heating air supply body (33, 43) for supplying the heating air (4) into the device (30, 40), and a mixed ai...  
WO/2007/115811A1
Air-conditioning system (10) for aircraft, in particular for commercial aircraft, with a bleed air source (12), a bleed air line (22-30) comprising a main valve (16), and an air-conditioning unit (32), wherein a mass air flow conveyed fr...  
WO2007088012B1
A cooling system (10), which is in particular suitable for cooling food on board an aircraft, comprises a chiller device (12) and a first cooling circuit (16) which is adapted to feed cooling energy generated by the chiller device (12) t...  
WO/2007/113070A1
The present invention relates to a device and a method for generating electricity on board an aircraft, comprising several generators (GEN1-GEN4) and several environmental control systems (ECS1, ECS2, ECS3, ECS4) with an external air inl...  
WO/2007/110248A1
The invention relates to a device and a method for distributing air in a cargo aircraft. The cargo aircraft has an air distribution system (10) which is connected to at least one cargo deck. The air distribution system comprises a source...  
WO/2007/080096A3
In a process and a system (10) for controlling the pressure in an aircraft cabin the status of at least one aircraft door is detected by at least one detection device (12a-c, 14a-c, 16a-c, 18a-c). A signal indicative of the status of the...  
WO/2007/093389A1
A system for improving the air quality in a pressure cabin of an aircraft comprises a recirculation air circuit by means of which a portion of the cabin air, referred to as recirculation air, is withdrawn from the pressure cabin, filtere...  
WO/2007/090608A1
The invention relates to an aircraft air conditioning system with at least one fresh air supply line (14) for conveying fresh air into an aircraft cabin, wherein the fresh air is blown out into the aircraft cabin via at least one dischar...  
WO/2007/087974A1
An air conditioning arrangement (22) for an aircraft (10) or other premises with a plurality of climate zones (12 to 20) that may be individually temperature-controlled, comprises a main branching system (26) comprising an air supply fee...  
WO/2007/087709A1
A method of sanitizing a passenger cabin includes excluding people from the passenger cabin and substantially sealing the passenger cabin such that air inside the passenger cabin is prevented from exiting the passenger cabin. An ozone en...  
WO/2007/088012A1
A cooling system (10), which is in particular suitable for cooling food on board an aircraft, comprises a chiller device (12) and a first cooling circuit (16) which is adapted to feed cooling energy generated by the chiller device (12) t...  
WO/2007/083027A1
The invention concerns a precooler (30) having an annular cross-sectional shape about the axis (L-L) of the pod and arranged inside the rear part (10R) of the inner shroud (10) in external contact with the cold flow (9) exiting the fan d...  
WO/2007/084123A2
A method and system for alerting an aircrew of terrorist activity in a cabin of an aircraft. When a terrorist or emergency situation is detected by a flight attendant, the flight attendant speaks an activation word, which turns the perso...  
WO/2007/083026A1
The invention concerns a precooler (30) having an annular cross-sectional shape about the axis (L-L) of the pod and arranged inside the rear part (10R) of the inner shroud (10) in contact with a cold fluid (9) exiting the fan duct (13).  
WO/2007/080096A2
In a process and a system (10) for controlling the pressure in an aircraft cabin the status of at least one aircraft door is detected by at least one detection device (12a-c, 14a-c, 16a-c, 18a-c). A signal indicative of the status of the...  
WO/2006/115657A3
Combined aircraft hybrid fuel cell auxiliary power unit and environmental control system and methods are disclosed, hi one embodiment, an auxiliary power unit includes a fuel cell component which chemically converts combustible fuel into...  
WO2007039212B1
The present invention relates to a fluid throttle screen (2) for low-noise control of a fluid volume flow rate (Q) in a pipe and the use of such a throttle screen (2) in an aircraft climate control system. In addition, the present invent...  
WO/2007/045646A3
The invention relates to a bleed air supply system and a safety device (12) for closing a valve (5, 6, 7) in at least one of the several bleed air supply lines (3, 4, 8, 11) depending on an alarm signal that indicates an opening in at le...  

Matches 351 - 400 out of 1,618