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Matches 1 - 50 out of 1,629

Document Document Title
WO/2020/208420A1
A gasper assembly for use in an aircraft that includes a housing that includes an outer wall having an inner surface that defines a central opening, a nose member positioned in the central opening, a plurality of directional blades exten...  
WO/2020/207678A1
The invention relates to an air-conditioning arrangement (1) for a vehicle, comprising at least one fluid channel (20), which has at least two identically designed connection devices (22A, 22B), and comprising at least one movable vehicl...  
WO/2020/201654A1
The invention concerns an aircraft cabin air conditioning system, comprising two motorised turbomachines (16a, 16b) each comprising a compressor (14a, 14b) supplying an outlet (24) common to the compressors and a turbine, one of the turb...  
WO/2020/193518A1
In a method for producing an air guiding component (4) for an air-conditioning system of an aircraft: - at least two part-shells (2a, b) of the component (4) are provided, wherein at least one of the part-shells (2a, b) has a joining are...  
WO/2020/178504A2
Air conditioning system for a cabin (10) of an aircraft, comprising: an air intake device; an air cycle turbomachine (12); at least one main cooling exchanger (16); a water extraction loop (30); a duct (26) for distributing water extract...  
WO/2020/178505A1
Exchanger (16) for cooling warm primary air with cool secondary air, comprising: a plurality of circulation channels for the secondary air (80); a plurality of circulation channels for the primary air, characterised in that it further co...  
WO/2020/174213A1
The present invention provides a vehicle (100) comprising: a body (4) having a skin; a heat source (12); and a thermal management system. The thermal management system comprises: a heat pipe (14) comprising: an evaporator end (close to 1...  
WO/2020/141053A1
The invention provides a circuit arrangement (1) and comprises: a first cooling body (10) having at least one first cooling channel (101) which is at least partially open at the top; at least one electrical power module (12) arranged in ...  
WO/2020/138076A1
An outer plate cooling system is provided with: an outer shell having an outer plate, an inner plate placed inside the outer plate, and a heat insulating layer placed between the outer plate and the inner plate; a cooling chamber which i...  
WO/2020/138075A1
This outer panel cooling system comprises: an outer shell having an outer panel and an inner panel; a heat source chamber provided on the inner side of the inner panel; a cooling path provided between the outer panel and the inner panel,...  
WO/2020/137465A1
A device to be mounted on a vehicle 100 having a plurality of seats 10 arranged in the front-rear direction and the left-right direction, for preventing infection among a plurality of passengers. The device includes air barrier forming u...  
WO/2020/124216A1
An air deflector that includes a vane with a vane top, a vane bottom, a vane first side, and a vane second side, where the vane first side and the vane second side define a vane longitudinal axis extending therebetween and a closure with...  
WO/2020/109889A1
An aerial, marine or land vehicle (1) comprising: a compartment (6) to be cooled; a first circuit (20) through which can pass and, in turn, comprising, a heat exchanger (22) that can be fed with the coolant and is designed to enable the ...  
WO/2020/109740A1
The invention relates to an air management system (10) for an ECS pack (20), comprising: - a leading edge (110, 210) of a turbomachine nacelle (100) or aircraft wing, - an air inlet (22), for example of an ECS pack (20), characterised in...  
WO/2020/104734A1
The invention relates to a silent air treatment device comprising a photocatalytic material (3), a porous support (5) made of photocatalytic material, wherein the porous support, which is flexible, and the photocatalytic material are per...  
WO/2020/033010A3
An aircraft propulsion system with a drag reduction portion adapted to reduce skin friction on at least a portion of the external surface of an aircraft. The drag reduction portion may include an inlet to ingest airflow. The aircraft may...  
WO/2020/101728A1
A door assembly configured to be positioned between a first compartment and a second compartment that includes a main door portion having a first decompression opening defined therein, at least a first panel portion positioned in a first...  
WO/2020/095477A1
This aircraft air conditioning device provided to an aircraft comprises: a plurality of base units (U1-U6) each comprising two electrically driven compressors (1, 3, 4, 6) connected serially to an air flow passage; a temperature regulato...  
WO/2020/084251A1
The invention concerns a loop (40) for extracting water from an air conditioning system of a cabin (5) of an air or rail transport vehicle comprising an air cycle turbine engine (20), the loop comprising: a condenser (41); a three-dimens...  
WO/2020/064665A1
The invention relates to a component (2) for airflow guidance in an air-conditioning system for an aircraft, having at least one inlet aperture (18) and at least one outlet aperture (20) for air (4), having at least two part shells (6a, ...  
WO/2019/227237A1
Disclosed is a method including sampling the air of a pressurized zone of an aircraft by identifying a pre-existing pressurized air flow in a pressurized zone of an aircraft without substantially blocking the pre-existing pressurized air...  
WO/2019/211566A1
The invention relates to an air sampling system comprising an air sampling port created on an engine of the aircraft, an air supply duct, a pressure sensor, an overpressure valve mounted in said air supply duct, characterized in that sai...  
WO/2019/161069A1
An oxygen mask container assembly that includes a container that defines a container interior and includes a container opening, an oxygen mask assembly disposed in the container interior, a mask ejector in operative communication with th...  
WO/2019/119115A1
An overhead flow distribution assembly for an aircraft cabin, including a conduit defining a plenum having an inlet, upper outlets and lower outlets, the upper outlets spaced apart from each other along a longitudinal direction of the ai...  
WO/2019/126134A1
The invention is directed to preparation of hollow fiber membrane devices that exhibit improved durability and mechanical strength in air separation operations such as generation of nitrogen enriched air on board aircraft. In particular ...  
WO/2019/119828A1
Provided are a temperature control method and apparatus, and an unmanned aircraft, said temperature control method being used for said unmanned aircraft; the unmanned aircraft comprises a heat dissipation device; the temperature control ...  
WO/2019/109172A1
A system and method for determining a remaining useful life of an ozone converter of an aircraft are disclosed. The method comprises using flight data of the aircraft and location-based ozone exposure data to determining a cumulative ozo...  
WO/2019/070438A1
An emergency vision apparatus includes a housing for attachment underneath an instrument panel in a cockpit, the housing including a front opening, a front cover for the front opening, a bottom portion of the front cover being pivotably ...  
WO/2019/025653A3
The invention relates to temperature control equipment for inside aircraft or similar, comprising a closed-cycle cooling circuit, said circuit including compression means, a condensation/evaporation exchanger, an expansion valve and an e...  
WO/2019/059394A1
A compact unmanned mobile body capable of carrying a package with reduced risk during package transportation, and a package collection and delivery method involving the use of the compact unmanned mobile body, wherein the compact unmanne...  
WO/2019/051604A1
Systems and methods for a heat exchange system used to heat or cool a space. The system includes an airflow source for providing an airflow and at least one conduit that defines an airflow path for receiving the airflow. The system furth...  
WO/2019/048761A1
This device comprises a hollow body delimiting a generating space, means for generating droplets from a liquid jet (J) flowing inside said chamber, means for discharging a majority of the liquid jet, as well as means for diffusing drople...  
WO/2019/048763A1
This device comprises a hollow body delimiting a generating space, means for generating droplets from a liquid jet (J) flowing inside said space, along a generation path, ventilation means capable of generating a gas flow intended to ent...  
WO/2019/036803A1
Apparatus and methods for providing air to pneumatic loads such as an environmental control system for a passenger cabin of an aircraft or an ice protection device of the aircraft are disclosed. In one embodiment, the apparatus comprises...  
WO/2009/122238A3
A valve assembly is provided including an injection molded flow body having at least one inlet port, at least one outlet port, and a flow passage there between. The injection molded flow body is formed of a high performance engineering t...  
WO/2019/025653A2
The invention relates to temperature control equipment for inside aircraft or similar, comprising a closed-cycle cooling circuit, said circuit including compression means, a condensation/evaporation exchanger, an expansion valve and an e...  
WO/2019/010581A1
In an aspect, a test platform for testing an embedded control system having a plurality of interconnected components is operable to: receive, at run time, configuration data for configuring a system under test ("SUT") representing the em...  
WO/2019/008085A1
The aircraft (100) comprises at least one power electronics component (210) and a coolant circuit (230) for cooling the at least one power electronics component (210) by means of a coolant. The aircraft (100) comprises temperature contro...  
WO/2018/233977A1
System (1) for inerting at least one volume (3) in an aircraft, said system comprising at least one generator of inerting gas (2) fed with compressed air originating from a passenger cabin, and means for distributing (11) the inerting ga...  
WO/2018/222789A1
Disclosed is an area sensor for air quality in the cockpit, crew rest or other area of an aircraft. Noxious fumes, fuel vapors, carbon monoxide and other vapors can cause significant risks to the flight crew of an aircraft. Fumes may cau...  
WO/2018/144080A8
Systems and methods for integrated power and thermal management in a turbine-powered aircraft are provided. The systems may include rotationally-independent first and second auxiliary power unit shafts, a power turbine, a first compresso...  
WO/2018/210744A1
The invention relates to a device for equalising a pressure difference for an aircraft. The device according to the invention comprises a planar separating wall (1), which is fixed to the aircraft and which separates a first space (2) fl...  
WO/2018/202455A1
A manifold assembly (300) configured for integration with a joint cover apparatus in a ducting system to detect leaking gas comprises an elastomeric manifold block (303) having a substantially circular inlet aperture and one or more gas ...  
WO/2018/191216A1
An onboard rebreathing loop system resident on an aircraft for providing oxygen to aircraft personnel includes a ceramic oxygen generating system (COGS) module configured to receive an inlet air and output a high purity oxygen (O2) gas i...  
WO/2018/183731A1
A solid state liquid-chilled bar unit for an aircraft galley includes a multilevel frame dimensioned to fit the galley and including stacked slots, each slot configured to fit a compartment. Warmer compartments include a liquid thermoele...  
WO/2018/172252A1
The invention relates to a cabin air inlet module (16). The cabin air inlet module (16) has a flow channel body (8). The flow channel body (8) has at least one wall which delimits a flow channel in which feed air (5) is supplied to a zon...  
WO/2018/165498A1
An unmanned aerial vehicle includes at least one rotor motor configured to drive at least one propeller to rotate; and a micro hybrid generator system configured to provide power to the at least one rotor motor. The micro hybrid generato...  
WO/2018/163692A1
This heat radiator for an aircraft cools a heat source mounted on the aircraft and is provided with a heat radiation section (3) having recesses or protrusions formed on the surface thereof which comes in contact with a main stream, the ...  
WO/2018/144080A1
Systems and methods for integrated power and thermal management in a turbine-powered aircraft are provided. The systems may include rotationally-independent first and second auxiliary power unit shafts, a power turbine, a first compresso...  
WO/2018/134025A1
The invention relates to devices (3) and associated methods for the secure and low-cost monitoring of environmental conditions during a transportation, wherein, during the transportation, at least one measurement variable can be, prefera...  

Matches 1 - 50 out of 1,629