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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...
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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...
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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...
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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 ...
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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...
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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...
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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...
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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...
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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.
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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...
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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)...
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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...
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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...
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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...
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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...
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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 ...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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 ...
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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 ...
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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 ...
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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 ...
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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...
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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 ...
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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...
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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...
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WO/2005/019747A1 |
A system, apparatus, and method are provided for selectively actively and passively refrigerating one or more enclosures. The apparatus includes a primary heat sink (26) that defines at least one surface configured to receive thermal ene...
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WO/2005/005026A1 |
The direct contact liquid air contaminant control system and method to revitalize air by removal of carbon dioxide and other trace gas contaminants use a direct contact air, liquid scrubber element and stripper element. The scrubber elem...
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WO/2005/002966A1 |
The on-board system comprises: an OBIGGS (2) that supplies, via outlet (6), nitrogen for inerting compartments (15, 16, 17) of an aircraft; a first OBOGS (3) that supplies oxygen to a supply circuit (19) for aircraft occupant masks (20, ...
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WO/2005/000467A1 |
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,...
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WO/2005/000675A1 |
An aircraft cabin pressure control system valve (100) integrates three cabin pressure control functions, main cabin flow control, positive pressure relief, and negative pressure relief, into a single valve package. The valve includes a c...
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WO/2005/000676A1 |
An aircraft cabin pressure outflow control valve that includes a rotationally mounted valve gate (110) and one or more flow influencing walls (130) adjacent to or part of to the valve body (102). Each wall has a distal edge (132) formed ...
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WO/2004/108174A1 |
An aircraft air conditioning system for conditioning of the cabin and/or cockpit air comprises an air re-circulation circuit (13, 14, 15, 16) and a UVC radiation unit (12) positioned so as to irradiate air in the re-circulation circuit (...
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WO/2004/106158A2 |
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...
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WO/2004/106157A1 |
A snow filter (10) for an airplane cabin air supply system is provided with a coned inlet screen (23) which allows some air to pass through and some snow to be retained. The coned configuration (22) diverts much of the air and snow towar...
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WO/2004/102636A2 |
An aircraft cabin pressure control system that controls cabin altitude during aircraft ascent to a cruise altitude, such that, under most operational circumstances, the cabin altitude rate of change during the ascent is set to fixed valu...
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WO/2004/087568A1 |
The invention concerns a system for supplying oxygen to occupants (6, 7) of an aircraft comprising a PSA device (1) having an air intake receiving compressed air from the engines (5), the oxygen distribution line (3) including a pressure...
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WO/2004/074750A2 |
A system and method are provided for refrigerating at least one enclosure (11), such as an aircraft galley cart. The system includes at least one air-to-liquid heat exchanger (18), an eutectic thermal battery (12), a liquid-to-direct hea...
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WO/2004/074095A1 |
The present invention provides a ventilated seating system. The ventilated seating system provides a back rest portion (110) including an upper end and a lower end and a perforated duct (130) positioned adjacent to the lower end of the b...
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WO/2004/074094A2 |
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...
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WO/2004/065215A1 |
A system and method for an engine bleed flow-sharing control system is disclosed. For a multi-engine bleed system, one (10) of the engines is selected as the master channel (15) such that the bleed air supply pressure of the control syst...
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WO/2004/056451A1 |
The invention concerns an alternating pressure adsorption system (1) containing a high-performance adsorbent having a grain size distribution not exceeding 0.8 mm, the cycle period not exceeding 10 seconds, and the input air is introduce...
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WO/2004/050479A1 |
A method of providing gas to a system (10) which separates from a pressurised supply gas (18), product gas, includes conditioning the supply gas (18) by both cooling and drying the supply gas.
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WO/2004/048827A1 |
A valve (10) for controlling a flow of a fluid between a first environment (E1) to a second environment (E2) is provided. The valve (10) includes a frame (14) that fits within an aperture (18) in a divider (22) separating the first envir...
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