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Matches 101 - 150 out of 1,580

Document Document Title
WO/2015/095506A1
An air drying system for OBOGS is provided. The system comprises a bypass valve having an opened state and a closed state. The bypass valve is in fluid communication with an air inlet providing pressurized air. A dryer unit is configured...  
WO/2015/092251A1
The invention relates to an aircraft turbomachine (10) comprising a nacelle and an engine (12) comprising at least one outflowing jet of air, characterised in that a heat exchanger (20) of the precooler type for supplying air to the airc...  
WO/2015/004388A3
A mixing pump (2) according to the invention comprises : a so-called cool air duct; a so-called hot air intake (10) leading into the cool air duct; as well as means for injecting air from the hot air intake (10) into the cool air duct. T...  
WO/2015/067373A1
A cooling system (2) for an interior space of a vehicle comprises a main cooling system (4) coupled with an air inlet (6) for receiving air (10) and coupled with the interior space (12, 14, 16, 18, 20) for providing cooled air to the int...  
WO/2015/055672A1
The invention relates to a system (10) for treating air, comprising a first circuit (18) of air collected directly outside the aircraft, including: upstream, an inlet (20) for the intake of outside air; downstream, an outlet (22) for the...  
WO/2015/051687A1
A heating system and a method used for an airplane door area. The system comprises a heating source, a pipeline extending from the heating source, and a heat transfer medium. The heat transfer medium is air. The pipeline is used for supp...  
WO/2015/054009A1
A chilled air plenum system for aircraft galleys adapted to be connected to a food cart bay for a food cart includes an air return plenum having a return airflow duct with a plurality of midline primary apertures and a plurality of secon...  
WO/2014/012004A3
An air inlet grille for an appliance onboard an aircraft includes a screen having an inside-facing surface and an outside-facing surface, a plurality of airflow openings formed within the screen between the inside-facing surface and the ...  
WO/2015/031530A1
An apparatus for controlling airflow in a duct of an aircraft galley chiller includes first (102) and second (103) legs having ends connected together to form a vane, and free ends (104, 105) configured to be attached within the duct. A ...  
WO/2015/026432A1
An environmental control system (200) is provided. The environmental control system may receive pressurized air from a single supply line (220). A pressure regulating turbomachine (230) may be located within the supply line. A motor-gene...  
WO/2015/026433A1
A thermal energy harvester and power conversion system employs a bleed air duct (16) containing the flow of high temperature air from an engine. A lower temperature air source is included with an energy conversion device (38) having a ho...  
WO/2015/003073A1
A chiller for an aircraft galley that is sized to be disposed in a compartment for housing beverage carts, the chiller comprising a vapor cycle refrigeration system with a liquid cooled condenser located within the housing and a liquid c...  
WO/2014/202842A1
- An aircraft capable of passing from the aerial domain to the spatial domain and method for automatically adapting the configuration of same. - The invention involves providing, on said aircraft, an additional breathable gas supply (25)...  
WO/2014/124473A3
A system (100, 110) for cooling an (100, 110) includes a fuel tank (160), a fuel delivery system (165), a cooling system (120), and a heat exchanger (135). The fuel tank is configured to hold cooled fuel (155) for the aircraft. The fuel ...  
WO/2014/158280A3
A cooling system for an aircraft includes a first cooling circuit (702) having a first evaporator (706) and a second evaporator (708), and a second cooling circuit (704) having a third evaporator (712) and a fourth evaporator (714). One ...  
WO/2014/149101A3
An aircraft 1 is provided with a gas turbine engine 20 having a plurality of shafts. A first output shaft 32 provides power to an electrical machine 40 and a propeller 50, while a second output shaft 33 provides power to a refrigerant co...  
WO/2014/158280A2
A cooling system for an aircraft includes a first cooling circuit having a first evaporator and a second evaporator, and a second cooling circuit having a third evaporator and a fourth evaporator. One of the first and second cooling circ...  
WO/2014/149271A1
There is provided an air duct assembly. The air duct assembly has a deformable duct preform having securing portions formed along opposing longitudinal edges. Each securing portion has a flange portion and a radius portion. The air duct ...  
WO/2014/142727A1
A climate control system (1), intended to be temporarily connected to at least one aircraft (2), when the aircraft is on the ground, with which handled air with at least one flexible conduit (23) is supplied to the aircraft's cabin from ...  
WO/2014/143194A1
A cooling system includes a heat exchanger (210) through which a refrigerant flows, and which rejects heat to a fluid, an evaporator (208), a first circuit having an expansion device (214), a second circuit having an expansion machine (2...  
WO/2014/137515A1
A method and apparatus for an air circulation system. The apparatus comprises a suite and a circulation unit. The suite has walls extending upward from a floor of the passenger cabin without reaching a ceiling of the passenger cabin. The...  
WO/2014/135844A1
A heat exchanger assembly (201) comprises: a hot fluid flow channel (210); a cold fluid flow channel (220); and a heat exchanger (230) disposed between the channels. The heat exchanger comprises a heat sink (240) and a thermoelectric dev...  
WO/2014/127899A1
The invention relates to a hybrid component and a method for producing the same. The hybrid component according to the invention comprises a base (2) having at least one portion that is a laminate (3) produced from a plastic foam and a f...  
WO/2014/131061A1
An aircraft comprises composite skin (120) having an opening, and a ventilation conduit (120) having an end portion (132) that extends to the opening in the composite skin. The conduit is made of metal except for the end portion (132), w...  
WO/2014/055152A3
A bifurcated inlet scoop frame for a gas turbine engine and method of using such frame for a gas turbine engine are disclosed. The bifurcated inlet scoop frame may include a nose, a first side panel, and a second side panel. The first si...  
WO/2014/076391A1
The invention relates to an air conditioning system for the pressurized cabin of an aircraft. The system (1) comprises an air intake module (3) that is designed to draw in ambient air external to the aircraft, an air compression module (...  
WO/2014/072619A1
The invention relates to a method and to a device for determining, in real time, the flow rate of air collected from an aircraft engine (39) by a system (1) for collecting air from the engine, comprising: acquisition means (33) for acqui...  
WO/2014/070545A1
An air vehicle power and thermal management system (10) includes an aircraft controller (20) structured to distribute power provided by a gas turbine engine (36) between a cooling system (22) and an electrically powered load (14). The co...  
WO/2013/160390A3
The present invention relates to a device (10) for cabin pressure difference warning for an aircraft or spacecraft (1), comprising a cabin pressure difference sensor means (12) for detecting the current cabin pressure difference ΔΡ, a ...  
WO/2014/048731A1
The invention relates to a device for cooling a component (2) in a vehicle by means of a cooling air flow (4), wherein the device has at least one air inlet (11) and at least one air outlet (12), which are arranged such that the cooling ...  
WO/2014/044981A1
The invention relates to a body panel (1) for a transport vehicle — in particular for an aircraft — including a supporting plate (2) and a heat-exchange device (6), said supporting plate forming (2) on the outer surface (4) thereof f...  
WO/2013/121139A3
The device for supplying air to an auxiliary power unit (GAP) of an aircraft, said auxiliary power unit comprising a diesel engine (M) coupled to a turbocharger (TC), the said turbocharger comprising at least one first air inlet (AIR_CAB...  
WO/2014/041291A1
The invention relates to a method for supplying non-propulsive power of an aircraft, comprising driving a shaft (13) of a system (1) for controlling the environment of the aircraft by a combination of energy sources selected from: an aux...  
WO/2014/033052A1
Disclosed is a humidification device comprising a stacking unit with membranes which are permeable to water vapour, and with support frames which are stacked on top of one another and between which the membranes are clamped. An air inflo...  
WO/2014/033051A1
A moistening device has at least one stacking unit which contains a plurality of water-permeable membranes which are each enclosed at the edges by a frame. The frame is formed by a film composite with a lower film and an upper film, betw...  
WO/2014/030024A1
The present disclosure relates to a pre-cooler system comprising a pre-cooler (112) for cooling hot bleed air from an engine, and a bypass valve (204) for diverting at least a portion of the hot bleed air to bypass the pre-cooler (112). ...  
WO/2013/176946A3
The present invention provides a system and method for supplying, generating, conserving, and managing oxygen that is ideally suited for use on-board an aircraft for supply of breathable oxygen to passengers and flight crew. The system i...  
WO/2014/012746A1
The invention relates to an aircraft galley (1) comprising at least one cooling compartment (2) for receiving a container for foods and/or drinks to be cooled, characterized in that at the back of the galley (1) at least one first panel ...  
WO/2014/012742A1
The invention relates to an aircraft galley (1) comprising at least one cooling compartment (2) for receiving a container for foods and/or drinks to be cooled, characterized in that at the back of the galley (1) at least one panel (3) wi...  
WO/2014/001304A1
The present invention pertains to a heated floor panel (10) for an airborne vehicle (20) and an airborne vehicle having at least one heated floor panel. The floor panel comprises a controller housing (9), a first heated panel (6) configu...  
WO/2013/192047A1
An aircraft emergency oxygen dispensing device (19) includes an oxygen storage vessel (12) having a frangible pressure seal (14), and a manifold (16), a pressure regulator (18), one or more flow control valves (20) connected to the oxyge...  
WO/2013/180994A1
Provided herein is a hybrid system (100) for generating oxygen on¬ board an aircraft for passengers and/or flight crew to breath. The system includes a first chemical oxygen generator component (112) configured to promptly supply oxygen...  
WO/2013/176996A1
The present invention provides a system and method for supplying and managing oxygen suited for use on-board an aircraft for providing breathable oxygen to pilots and cockpit crew. Components of the system work together to optimize oxyge...  
WO/2013/079466A3
An on board inert gas generation system for an aircraft receives air from a relatively low pressure source such as low pressure engine bleed air or ram air and passes it to a positive displacement compressor (40) to increase the pressure...  
WO/2012/173580A3
The present invention has some functions like heating, cooling and air-conditioning consisting of a main unit and auxiliary units. It can be adopted to the available floor standing boilers or central coilers in the dwellings or working p...  
WO/2013/149936A1
A Heat exchanger (100, 200, 300) comprises a plurality of heat transfer modules (10, 20, 30, 40) which are disposed side by side so as to define a multilayer body (102, 202, 302) of the heat exchanger (100, 200, 300), wherein each heat t...  
WO/2013/041841A3
There is disclosed herein a layer assembly for a heat exchanger, the layer assembly comprising: at least one heat pump module, the module comprising a thermo-electric cooler (TEC) attached to an island formed from a flow-permissive mater...  
WO/2013/135534A1
The invention relates to a valve (10) for controlling the internal pressure in a cabin of an aircraft, comprising a first flap (12) and a second flap (14), which are supported in a frame (16), wherein the flaps (12, 14) control a fluid f...  
WO/2013/124344A1
The invention relates to an aircraft oxygen emergency device comprising a chemical oxygen generator (10), an oxygen supply line including a first line section (21) connecting said chemical oxygen generator with a flow regulator unit (20)...  
WO/2013/120764A1
A ventilation system (1) for an interior room (510) is provided, having a first air suction device (10), a second air suction device (20), a suction volume control device (30), a first air conduction pipe (11), a second air conduction pi...  

Matches 101 - 150 out of 1,580