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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...
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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 ...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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 ...
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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...
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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...
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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...
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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...
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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 ...
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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...
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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...
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WO/2018/132245A1 |
Described herein are methods which involve minimizing or eliminating the occurrence of delayed negative effects that may arise from exposure to reduced oxygen partial pressure. An amount of supplemental oxygen, which substantially mimics...
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WO/2018/106359A1 |
An aircraft has a gas turbine engine including a compressor section that includes at least one compressor bleed. An environmental control system has an air input configured to receive pressurized cabin air. An intercooler has an input an...
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WO/2018/086511A1 |
A ventilating and lighting apparatus (100) for an individual cabin can improve a contact area between air and a photocatalyst and ensure sufficient light irradiation on the surface of the photocatalyst, and implements rational utilizatio...
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WO/2018/088915A1 |
The purpose of the present invention is to cool the brakes of the landing gear of an aircraft. For this purpose, the air of the air-conditioning system of the aeroplane is used. Pre-conditioned air from the outside can be supplied to the...
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WO/2018/089934A1 |
Commercial supersonic aircraft and associated systems and methods. A representative commercial supersonic aircraft includes a fuselage configured to carry a crew and between 20 and 60 passengers, a delta wing mounted to the fuselage, and...
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WO/2018/067370A1 |
An air duct includes a first chamber and a second chamber, the first chamber being defined between an air handling device and the second chamber, and the second chamber being defined between the first chamber and an environment exterior ...
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WO/2018/060392A1 |
Aircraft comprising a fuselage (1) divided by a floor (2) into an o upper volume (3) and a lower volume (4) through which joists (5) extend that support the floor and delimit, along with the fuselage and the floor, two side chambers (6),...
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WO/2018/060186A1 |
The invention relates to a cabin wall element for thermal and acoustic insulation of an aircraft fuselage section located between two frames of an aircraft fuselage, wherein the cabin wall element has an outer wall which comprises a ther...
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WO/2018/060531A1 |
A secondary power unit for an aircraft comprises: a gas turbine engine (14) having at least one drive shaft, a twin load compressors (3) including first and second load compressors both coupled with the drive shaft, a first Ram-air intak...
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WO/2018/060579A1 |
The invention relates to an aircraft electrical network comprising an electrical device (28, 29) for protecting an outer surface of the aircraft from frost, which is suitable for being able to be supplied with power by a shared electrica...
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WO/2018/055287A1 |
Pressurised-air supply unit (1A; 1B; 1C; 1D) for an aircraft, comprising: a load compressor (30) configured to supply pressurised air (3) to the aircraft; a driving part (10) that can drive the load compressor (30); an electric motor (60...
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WO/2018/039289A1 |
A method and aircraft for providing bleed air to environmental control systems of an aircraft using a gas turbine engine, including determining a bleed air demand for the environmental control systems, selectively supplying low pressure ...
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WO/2018/038875A1 |
A method and aircraft for providing bleed air to environmental control systems of an aircraft using a gas turbine engine, including determining a bleed air demand for the environmental control systems, selectively supplying low pressure ...
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WO/2018/024983A1 |
The invention relates to an aircraft electrical power supply network architecture, comprising at least one compressor motor (116a, 116b) for the aircraft's air conditioning plant and at least two electrical generators (112a, 112b) of the...
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WO/2018/013661A1 |
A water separator (108) includes a tube (112) defining a longitudinal axis, wherein the tube (112) includes a tube wall separating an interior (114) of the tube from an exterior (116) thereof. A tube insert (118) is mounted within the tu...
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WO/2018/002171A1 |
The invention relates to a heat exchange device (1), comprising: - an enclosure for circulation of heat transfer fluid, delimited by at least two external plates (18), - an inlet frame (4) and an outlet frame (8) for a first heat transfe...
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WO/2018/002855A1 |
Apparatus and method for conditioning engine-heated air onboard an aircraft including a heat exchanger (140) at least partially disposed in a pylon structure (118) for supporting an engine (134) of the aircraft. The pylon heat exchanger ...
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WO/2017/216689A1 |
Ducts and methods for directing a flow of air from air-cooled devices onboard aircraft are disclosed. An exemplary method disclosed comprises: receiving air carrying heat extracted from the device, directing the air away from the device,...
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WO/2017/186895A1 |
The invention relates to a heating device (100) for the interior of an aircraft. Said heating device (100) comprises a mechanically loadable support structure (102), a mechanically loadable, heat-conducting top structure (106), and a hea...
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WO/2017/182318A1 |
An air vent (10) with a device for controlling an air flow is described. The air vent (10) has a housing (12) which surrounds an air duct (16) at least in sections, and has a displacement body (32) mounted pivotably in the housing (12). ...
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WO/2017/176754A1 |
In an illustrative embodiment, an apparatus for treating air discharged to a passenger suite of an aircraft includes an enclosure that houses components for treating air passing through the enclosure and a detachable cover connected to t...
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WO/2017/176650A1 |
In a preferred embodiment, an aircraft monument is adapted for being mounted against an aft-facing bulkhead of the aircraft. The monument may have an aisle-accessible compartment that includes comestible item dispensers and lower footwel...
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WO/2017/149228A1 |
The present invention proposes a system comprising an air conditioning unit using an electric motor coupled to the rotary shaft of an air cycle machine (ACM) so that the rotation of the shaft of the ACM is accelerated during phases of fl...
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WO/2017/137429A1 |
The invention relates to an aircraft (1) having at least two aero engines (2, 3, 4, 5, 6), having – a device for diverting bleed air from the various aero engines (2, 3, 4, 5, 6) in order to supply air to an air-conditioning system of ...
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WO/2017/139729A1 |
A method and aircraft for providing bleed air to environmental control systems of an aircraft using a gas turbine engine, including determining a bleed air demand for the environmental control systems, supplying low pressure and high pre...
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WO/2017/107718A1 |
A multi-shaft manned aircraft, comprising a heat exchange system, a cabin and a cockpit which is located within the cabin, the heat exchange system at least comprising an air inlet (10) in communication with exterior of the cabin, an air...
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WO/2017/107719A1 |
Provided is a multi-axis manned aircraft, comprising an electrical system, a heat exchange system, a cabin, and an equipment bay located within the cabin, the electrical system being received in the equipment bay, the heat exchange syste...
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WO/2017/077305A1 |
An aircraft environmental control system (4) for controlling a temperature of a fluid, the control system (4) comprising: a first temperature sensor (30) configured to measure a first temperature and to generate a first signal, the first...
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WO/2017/077301A1 |
An aircraft environmental control system (4) for controlling a temperature of a fluid, the control system (4) comprising: a temperature sensor (30) configured to measure a temperature of the fluid and to generate a first signal, the firs...
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