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Patent Searching and Data


Matches 401 - 450 out of 1,582

Document Document Title
WO/2006/105049A2
The present invention comprises systems and methods for providing conditioned air to a selected portion of an aircraft cabin. In one embodiment, a system includes a cargo compartment air recirculation system fluidly coupled to the cargo ...  
WO/2006/104535A1
A bleed air balancing system includes a plurality of bleed air flow paths (12) each carrying bleed air from one of a plurality of gas turbine engines (10), each bleed air flow path (12) including a flow rate sensor (19), and a circuit (5...  
WO/2006/092525A1
The invention concerns a filtering system comprising, in a main line (1) between a compressed air source (3) and an onboard user equipment (2) an exchanger/cooler (8) and at least one vapour-phase pollutant filtering downstream stage (9,...  
WO/2006/092526A1
The invention concerns a self-propelled vehicle, in particular an aircraft, comprising an onboard equipment such as an inerting system, means for vapour pollutant filtering (1) arranged between an air intake (8) connected to a compressed...  
WO2006028548A3
Apparatus and methods for forming thermoplastic clamshell components are disclosed. In one embodiment, a method includes providing first and second spaced-apart mold members (102,104). Next, first and second half-body portions (118) are ...  
WO/2006/079507A1
An air system for pressurizing and air conditioning a cockpit and cabin space of a plane comprises a compressor (3) for compressing an air mass flow, wherein the air mass flow to be compressed is extracted through a ram air duct (13, 14)...  
WO2004074094A3
Method and arrangement for adjusting nitrogen and oxygen concentrations within regions of an aircraft. The method includes separating nitrogen from ambient air onboard an aircraft thereby establishing a high-concentration nitrogen supply...  
WO/2006/058774A2
A supply system (100) for the energy supply in an aircraft comprising an engine (101) for propelling an aircraft, a fuel cell (102) for supplying an aircraft with electric energy, a first fuel reservoir (103) for supplying the engine (10...  
WO/2006/036724A1
An ECS system provides an ACM which locates the compressor (20) upon a common shaft (84) between a first turbine (22) and a second turbine (24). Each RAF is located remote from the ACM such that the turbines (22, 24) are located outboard...  
WO/2006/018225A1
Nowadays in aircraft so-called on-board inert gas generation systems (OBIGGS) are used to generate inert gases, to which OBIGGS cooled bleed air of engines or auxiliary power units is fed. According to an embodiment of the present invent...  
WO/2006/015858A1
A system for the provision of process air comprises a first cooling system (2) with a first heat exchanger, which is arranged in a channel (3) that serves as a cooling sink, and a cooling system (8), integrated in the first cooling syste...  
WO2005000467A8
The present invention provides a method and system for combined conversion of ozone and organic compounds in airplane bleed air. Catalytic converters have previously been used to reduce the levels of ozone in airplane bleed air. However,...  
WO/2005/113334A1
An aircraft with a fluid-duct system for extraction of the laminar layer and/or blowing out of fluid at vulnerable places of the outer skin, wherein the fluid-duct system (26, 19, 18) by means of switchable valves (6, 4) is connectable t...  
WO/2005/110844A1
A humidification apparatus which makes possible individual humidification of the air in a cabin of a passenger or cargo aircraft makes available a conditioning fluid to be ejected into the cabin from an outlet nozzle (10). The conditioni...  
WO/2005/102499A1
An air filter system (10) for use by airline passengers on commercial airlines and the like. The housing is configured to clamp to the gasper air supply nozzle (30) of the airliner. The housing is configured to direct air from the air su...  
WO/2005/094346A2
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...  
WO2005063576B1
The invention relates to a device (10) for heating an aircraft cabin and comprises a first hot air supply line (12) that leads to an air conditioning unit (14), a flow control valve (16) that is disposed in the first hot air supply line ...  
WO2005063566A3
With a cooling system for expelling heat from a heat source (30) located in the interior of an aircraft to a heat reducer (32), with a piping system (10) sealed against the surrounding atmosphere which is thermally coupled to a heat inta...  
WO/2005/085066A1
Systems, apparatus, and methods for the catalytic removal of at least one pollutant from an air stream via a catalytic precooler arranged in series with at least one augmentative catalytic device. The augmentative catalytic device may be...  
WO/2005/082489A1
A tool (110) for adsorbing carbon dioxide for use in adsorbing carbon dioxide in air, which has a carrying member (111) in the form of a foil or a plate, a porous aluminum oxide film (112) covering the carrying member (111), and an amine...  
WO/2005/082711A1
An inert tactical weapons system including a non-lethal application system to deal with terrorists. The system includes an inert gas supply (11) that is pumped through a wall (15) and into a structure in which terrorists are present. The...  
WO/2005/070764A1
A pressure control system (100) including an inflow unit (104) for admitting pressurized air into a cabin (102), an outflow unit (112) including a motor (308, 320) for operating a valve to discharge air from the cabin (102) at a predeter...  
WO/2005/068293A1
A method and a device for air-conditioning aircraft cabins proposes that the direction and/or impulse of an air jet (26) injected into the cabin is altered, dependent upon a temperature measured.  
WO/2005/063573A1
A method and a line system for the air-conditioning of a freight compartment or a cabin of an aircraft envisage that at sites (A, B, C, D) remote from passengers air that is at a temperature different from that at sites (E, F, G, H) clos...  
WO/2005/063572A1
With a method for controlling the temperature of feed air supplied to a cabin area of a passenger aircraft (10), a measurement value for the ambient temperature in the cabin area is determined by means of a temperature sensor system (24)...  
WO/2005/063578A1
With a method for controlling the temperature of feed air which is injected into the cabin zone of a passenger aircraft, the cabin of which is sub-divided into several cabin zones supplied respectively with specially temperature-controll...  
WO/2005/063566A2
With a cooling system for expelling heat from a heat source (30) located in the interior of an aircraft to a heat reducer (32), with a piping system (10) sealed against the surrounding atmosphere which is thermally coupled to a heat inta...  
WO/2005/063568A1
A cooling system (10) for the cooling of heat producing devices (44, 46, 48) in an aircraft is designed with a central cold producing device (12), at least one cold consumer (44, 46, 48) and a cold conveyance system (14) which connects t...  
WO/2005/063571A1
The invention proposes that a camera (18) takes a technical picture of an air outlet valve (10) of an aircraft, and the picture taken of the outlet valve (10) is displayed on a picture display unit (20), for example in the cockpit of the...  
WO/2005/063576A1
The invention relates to a device (10) for heating an aircraft cabin and comprises a first hot air supply line (12) that leads to an air conditioning unit (14), a flow control valve (16) that is disposed in the first hot air supply line ...  
WO/2005/063570A1
The invention relates to floor heating for an aircraft which has a floor (20) made up of heatable panels (18). In order to be able to heat up the panels (18) in an energy-saving way, the same are provided with hollow chambers (26) which ...  
WO/2005/063577A1
Device and method for temperature control in an aircraft cabin (104) wherein is controlled with a first supply control arrangement the supply of heated air from a first source into a first temperature area (106) of the aircraft cabin (10...  
WO/2005/063575A1
A process and device for temperature regulation of sections (zone 1….zone n) of the interior of an aircraft wherein the respective actual temperatures (Tactual) and the respective nominal temperatures (Tnominal) in the individual secti...  
WO/2005/063574A1
A system for controlling the temperature of feed air supplied to a cabin area of a passenger aircraft (10) includes a temperature sensor system (24), by means of which a representative reading can be taken for an ambient temperature in t...  
WO2005052459A3
The invention relates to an air conditioning assembly for a room, in particular for compartments of vehicles such railway cars, busses and airplanes. The invention further relates to a vehicle compartment comprising the air conditioning ...  
WO/2005/063569A1
A cooling air supply system (10) for an aircraft in order to supply cooling air from the aircraft surrounds to at least two devices requiring cooling air (38, 44, 56) within the aircraft, is designed with an air inlet (12), an air channe...  
WO/2005/063579A1
A ram air channel (10) for the supply of ambient air in an aircraft includes a first air inlet (12) and a main flow channel (16) which extends downstream of the first air inlet (12). In order to guarantee that the systems on board the ai...  
WO/2005/063567A1
In a cooling system (10) for cooling heat-generating installations (44, 46, 48) in an aircraft, with a refrigerating installation (12), at least one refrigeration consumer (44, 46, 48) and a refrigeration transport system (14) connecting...  
WO2005043265A3
A cabin pressure control system (100) and method extends the cabin pressure control logic (20) beyond the original maximum certified altitude of the aircraft, without having to update the control logic. Thus, the control system provides ...  
WO/2005/057087A1
[PROBLEMS] To provide a cooling system capable of preventing the efficiency of a refrigerating machine from being lowered when providing a specified temperature and a specified humidity in a cooling chamber even if there is a change in o...  
WO/2005/054645A1
The invention relates to a gas turbine, in particular an aircraft engine and to a method for generating electrical energy in a gas turbine. The gas turbine comprises at least one engine core (18), in which a shaft (19) produces a shaft o...  
WO/2005/052459A2
The invention relates to an air conditioning assembly for a room, in particular for compartments of vehicles such railway cars, busses and airplanes. The invention further relates to a vehicle compartment comprising the air conditioning ...  
WO/2005/047784A1
An aircraft galley air cooling system utilizes a controller having software for regulating the temperature within food carts within a galley air cooling unit. The cooling unit includes supply air and return air temperature sensors which ...  
WO/2005/043265A2
A cabin pressure control system (100) and method extends the cabin pressure control logic (20) beyond the original maximum certified altitude of the aircraft, without having to update the control logic. Thus, the control system provides ...  
WO/2005/030583A1
An air conditioning pack (10) for an aircraft provides primary (24) and secondary (26)heat exchangers arranged in a ram air duct (15). A third heat exchanger (28) is arranged in the ram air duct (15) and is selectively fluidly connected ...  
WO/2005/030581A1
A mixer (16) includes a fresh air tube (40) defining a passage (42) having an inlet (44) receiving conditioned air (14) from an air conditioning pack (12). The fresh air tube (40) includes an outlet (46) providing mixed air (18) to a cab...  
WO/2005/030582A1
A mixer includes a fresh air tube (40) defining a passage (42) having an inlet (44) receiving conditioned air (14) from an air conditioning pack (12). The fresh air tube includes an outlet (46) providing mixed air (18) to a cabin of the ...  
WO/2005/030579A1
A galley chiller system for an aircraft includes at least one condenser (42a, 42b) having a refrigerant fluid. The fluid within the condenser rejects heat to a first surrounding environment. To more efficiently use the condenser of the g...  
WO2004106158A3
An air conditioning system (10) provides a pack conditioned air passage (22) which intersects with a recirculation passage (28) prior to communication of the combined air flow with a mixer (30). The combined air flow traverses a distance...  
WO/2005/023649A1
A valve is provided for controlling a flow of a fluid between a first environment and a second environment. The valve includes a frame adapted to fit within a perimeter of an aperture in a divider separating the first environment from th...  

Matches 401 - 450 out of 1,582