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Matches 51 - 100 out of 1,281

Document Document Title
WO/2021/064374A9
A propulsion management system for an aircraft, an aircraft comprising such a propulsion management system and a method of decelerating an aircraft. The aircraft comprises an air propulsion system having one or more propellers. The propu...  
WO/2021/064390A9
A cooling system for an aircraft, an aircraft comprising such a cooling system, and a method of cooling a battery in an aircraft. The cooling system is for cooling a battery in an aircraft using a flow of gas. The cooling system comprise...  
WO/2021/099733A1
The invention relates to an air-conditioning system for a cabin (10) of an aircraft (80) comprising a bleed air source (12); a dynamic air circulation channel (13); a network of ducts and control valves; an air-cycle turbomachine compris...  
WO/2021/094323A1
There is provided an apparatus for preparing a ventilation gas mixture for pilots and crew of aircraft, the apparatus comprising a first gas mixer feed configured to receive exhaled air from a person, wherein the exhaled air comprises ca...  
WO/2021/092819A1
An air preparation system (100), comprising an air inlet (110), an air outlet (120), a compression device (130) and a main refrigeration device (140), wherein the compression device (130) is arranged between the air inlet (110) and the a...  
WO/2021/083670A1
The invention relates to a system (16, 35) for outputting air from an air source in a passenger cabin (46) of a vehicle (42), comprising at least one valve (2, 34) and at least one voltage source (11) that can be connected to the valve (...  
WO/2021/084237A2  
WO/2021/073186A1
A helicopter multi-cabin two-mode air conditioning system employing compressor intermediate air supplementation technology comprises a four-way reversing valve (1), a compressor (2), a first air-cooled heat exchanger (3), a first fan (4)...  
WO/2021/067573A1
An apparatus, system, and method for filtering and assaying a fluid sample are described. In an embodiment, the apparatus includes a filtration unit comprising: a filter bracket shaped to removably couple with a fluid sample cup and a va...  
WO/2021/061983A1
A control system for an onboard oxygen generating system (OBOGS) includes a gain control communicatively coupled to an oxygen sensor configured to measure an oxygen concentration outputted from the OBOGS. The gain control selectively swi...  
WO/2021/058080A1
The invention relates to a galley module (1) for an aircraft, comprising at least one heating and/or cooling unit having at least one first compartment (2) for drinks and/or food, wherein the temperature of said compartment can be condit...  
WO/2021/058916A1
Method for manufacturing a fire-resistant part of an air conditioning system (9) for an air or rail transport vehicle (8), characterised in that it comprises at least the following steps: a step (10) of obtaining a part comprising at lea...  
WO/2021/043839A1
Heat exchanger of an air-conditioning system of a cabin of a transport vehicle, comprising: a primary circuit supplied by a first air flow (169), a secondary circuit supplied by a second air flow (168), a casing (161) defining an air-cir...  
WO/2021/044142A1
There is provided a thermal management apparatus for use with a vehicle comprising: a chassis in thermal contact with one or more first components that require thermal management and one or more second components that require thermal man...  
WO/2021/046558A1
A cargo aircraft configured to carry a portion of its payload in a cargo bay volume enclosed by a moveable nose door and supported by a structural extension of the fuselage that extends forward into the moveable nose door is disclosed. E...  
WO/2021/042802A1
A high-temperature sterilization air conditioning system for an airplane, and a sterilization method. In said system, a high-temperature sterilization air recirculation apparatus is added to a traditional airplane air conditioning system...  
WO/2021/043733A1
Air conditioning system for a cabin of an air or rail transportation vehicle comprising a pneumatic turbomachine comprising at least one compressor and at least one turbine (126) connected by a mechanical shaft extending along an axis, r...  
WO/2021/046560A1
A fixed-wing cargo aircraft having a kinked fuselage to extend the useable length of a continuous interior cargo bay while still meeting a tailstrike requirement is disclosed, The fuselage defines a continuous interior cargo bay along a ...  
WO/2021/032476A1
The invention relates to a primary structural assembly (100) for an aircraft outside-skin heat exchanger (50), the assembly comprising: an outer-skin portion (5) which defines an outer shape of the aircraft (1) and forms a portion of a h...  
WO/2020/254393A1
The invention relates to a temperature-control device (100) for an aircraft (102), which device has a first layer (104) and a second layer (106) opposite the first layer (104), a heating layer (108), which is arranged between the first l...  
WO/2020/254755A1
The invention relates to an electrical air conditioning system for air-conditioning a cabin (10) of an aircraft comprising a source (11) of fresh air, a dynamic air circulation duct (12), a motorized compressor (13) comprising an air inl...  
WO/2020/254754A1
The invention relates to an assembly of heat exchangers comprising a dynamic air flow channel (14) extending in a longitudinal direction and characterised in that it comprises at least two heat exchangers (12a, 12b) which are separated a...  
WO/2020/249916A1
The invention relates to a regulator, configured to receive a stream of hot air carrying pneumatic power via an air inlet (12), to treat this hot air and to send the treated hot air to an air outlet (14) configured to supply a pneumatic ...  
WO/2020/234544A1
The invention relates to a regulator, configured to receive a hot air flow via an air inlet (12), to treat this hot air and to transmit the treated hot air to an air outlet (14) configured to supply a pneumatic actuator (16), comprising ...  
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/2020/101728A1
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...  

Matches 51 - 100 out of 1,281