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JP6879718B2 |
A galley (104) includes a cart compartment (102) configured to receive at least one galley cart (108). The cart compartment (102) is defined by a plurality of walls (154) including a rear wall (166) behind the cart compartment (102), sid...
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JP6880375B2 |
A method and an aircraft air contaminant analyzer for determining and classifying by type aircraft air contaminants, providing a sample flow path and bypass flow path bypassing the sample flow path, are disclosed.
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JP2021031055A |
To provide an aircraft contaminant removal system which includes one or more membrane separators configured to absorb a contaminant from a cabin air stream into a liquid sorbent, desorb the contaminant from the liquid sorbent, discharge ...
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JP2021028247A |
To provide a self-contained navigation unmanned moving object with reduced risk during luggage transportation.A luggage collection system that uses a small flying object includes: a step at which the small flying object receives a flight...
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JP6813345B2 |
A bearing assembly (42A) includes a shaft (90A) and a thrust runner (68A) attached to the shaft (90A). The shaft runner protrudes radially outward from the shaft. A thrust bearing (66A) is positioned axially adjacent to the thrust runner...
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JP6803214B2 |
A cooling air flow path (182) through an air cycle machine can include an inlet (184), at least one bearing (170) downstream from the inlet (184) and in fluidic connection with the inlet (184), an outlet downstream from the at least one ...
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JP2020134034A |
To provide a loop heat pipe capable of easily mounting an evaporator to an existing facility.A loop heat pipe 100 includes: a plurality of divided evaporators 11 that include a body 11a and a porous body 5 provided inside the body 11a an...
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JP2020132015A |
To provide an air conditioning piping structure for an aircraft, which can promote mixing of temperature adjusted air and recirculated air which flow into a mixing chamber forming an air conditioning system, and an air conditioning syste...
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JP2020524594A |
A device and method for low temperature purification of gas flow, a purification circuit comprising a first inlet (5) and a first set of filters (6, 7, 8, 9) arranged in series. The first set of filters with (4) is equipped with a termin...
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JP2020524634A |
A system (1) for inactivating at least one volume (3) in an aircraft, wherein the system is supplied with the compressed air generated from the cabin, at least one of the inert gases (2). It is a means (11) for distributing the inert gas...
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JP2020522422A |
Disclosure is an air quality area sensor in the cockpit, occupant rest area, or other area of the aircraft. Poisonous gases, fuel vapors, carbon monoxide, and other vapors can pose a significant risk to aircraft crew. Poisonous gas can c...
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JP6725489B2 |
The invention relates to a method for managing fluids necessary for the operation of a vehicle, wherein said method is characterized in that it includes an operation comprising anodic oxidation of a solution of hydrogen peroxide (P) for ...
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JP6707347B2 |
A water injector (45) for an aviation cooling system (2) includes a body (60) having a first end (62), a second end (63), and an intermediate portion extending therebetween. A conduit (68) extends through the body from the first end to t...
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JP2020071013A |
To provide a moving body cooling system that can restrain a decrease in cooling capacity caused by unevenness of a refrigerant by allowing it to be uniformly supplied to an evaporator.A moving body cooling system 100 comprises a compress...
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JP6680466B2 |
A panel (300) includes a structural substrate (310) and a damping element (320) including a viscoelastic material (VEM) layer (330) coupleable to the structural substrate of the aircraft, and a constraining layer (340) coupled to the VEM...
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JP6669845B1 |
To provide an infection control device capable of suppressing infection between passengers without causing discomfort to passengers. The device is mounted on a vehicle 100 in which a plurality of seats 10 are arranged in an arrangement i...
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JP6667998B2 |
Aircraft (10), air conditioning systems (12), and air diffusers (14) that may be used to create a quiet, comfortable environment within an aircraft cabin (16) are disclosed. For example, an aircraft cabin air diffuser, which may be used ...
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JP6661369B2 |
Temperature of a structural member is maintained at allowable temperature or less by suppressing heat transfer from a high-temperature duct to the structural member. An insertion sheet according to the present invention is inserted betwe...
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JP6649342B2 |
To provide an unmanned aerial vehicle that is provided with a separated section not to exert adverse influence on an atmospheric pressure sensor in an inertial measurement unit.An unmanned aerial vehicle (UAV) 100 may comprises a housing...
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JP6612218B2 |
Respiratory protection hood comprising a flexible envelope and a reservoir of pressurized oxygen comprising an outlet orifice that leads into the internal volume of the envelope, the outlet orifice being closed off by a removable stopper...
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JP2019528213A |
How to supply bleed air to the aircraft's environmental control system (48) using a gas turbine engine (12) and the aircraft determines the bleed air demand for the environmental control system (48) and low pressure and high pressure ble...
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JP2019528212A |
The method of supplying bleed air to the environmental control system (48) of the aircraft (10) using the gas turbine engine (12) and the aircraft determines the bleed air demand for the environmental control system (48) and low pressure...
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JP6582252B2 |
To provide a body temperature monitoring system for an in-flight passenger capable of accurately detecting a feverish patient with suspected infection of a new type virus, etc. who is determined to be in need of isolation, prior to entry...
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JP2019526734A |
A method for supplying bleed air to an aircraft's environmental control system using a gas turbine engine and the aircraft selectively supplies low-pressure and high-pressure bleed air to the environmental control system with the steps t...
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JP6557487B2 |
The present invention provides a water inflow prevention device for aircraft, working when landing in water, the device including: a blocking body for blocking a flow channel from an outside of the aircraft when landing in water, the flo...
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JP6554511B2 |
Apparatus and methods for providing a desired volumetric conditioned airflow rate and for reducing noise level, airflow recirculation and airflow separation are disclosed. An example apparatus includes a nozzle housing having a pair of o...
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JP2019516611A |
An unmanned aviation vehicle is configured to drive and rotate at least one propeller, with at least one rotor motor, a passenger compartment sized to accommodate human or animal passengers, and power to at least one rotor motor. Include...
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JP6516547B2 |
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JP6518423B2 |
An air cycle machine (ACM) pack system (10) for an aircraft (12) with an improved low inlet pressure cooling performance is provided. The ACM pack system (10) has an air cycle machine (ACM 42) with at least one compressor (72) mechanical...
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JP2019069770A |
To provide an onboard inert gas generation system for generation of inert gas on board an aircraft to facilitate inerting of fuel tanks and other areas on board the aircraft.An onboard inert gas generation system for an aircraft receives...
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JP6510390B2 |
The present invention relates to testing equipment of onboard air conditioning system, comprising: a sound receiver and a sound processor, wherein the sound processor processes the running noise of onboard air conditioning system sampled...
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JP6507022B2 |
An aircraft environmental conditioning system (100) is disclosed that includes an air cycle machine for conditioning an airflow comprising hot compressed air by reducing its temperature and pressure. The air cycle machine is disposed in ...
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JP6482897B2 |
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JP6470561B2 |
The turbo-compressor (TC) system has a TC assembly with a turbine (138) mechanically coupled to at least one compressor (144). The TC system has a TC inlet (132) in fluid communication with a bleed air system (34) in the aircraft engine ...
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JP2018534212A |
An aircraft environmental control system (4) for controlling the temperature of a fluid, a temperature sensor (30) configured to measure the temperature of the fluid and to generate a first signal. The first signal is a temperature senso...
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JP6422888B2 |
The invention concerns a structure (3) for feeding air to an auxiliary power unit (2) of an aircraft (1) comprising a pressurized cabin (10) and an auxiliary power unit (2), the structure comprising: a pipe (30) for feeding air to the au...
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JP6413509B2 |
Heat exchangers (17, 31) are adjacent to electric driving units (19, 33). Electric blowers of electric blower units (21, 35) rotate at rotational speed corresponding to amounts of heat generation of the electric driving units (19, 33) an...
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JP6412010B2 |
Air conditioning system for the pressurized cabin of an aircraft, said system (1) being characterized in that it comprises an air withdrawal module (3) configured for withdrawing ambient air from outside the aircraft, an air compression ...
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JP6407792B2 |
An aircraft environmental conditioning system (100) is disclosed having an air cycle machine for conditioning an airflow comprising hot compressed air by reducing its temperature and pressure. The air cycle machine is disposed in a housi...
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JP6377731B2 |
A hood comprising a flexible envelope and a reservoir of oxygen comprising a calibrated outlet orifice that leads into the internal volume of the envelope, the outlet orifice being closed off by a removable stopper, characterized in that...
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JP6340305B2 |
A method, system, and device for liquid drainage are provided. The system includes a drain tube (224) coupled to the air distribution system, a sump (220) coupled to the drain tube (224) and configured to receive liquid from the drain tu...
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JP6326381B2 |
A pressure equalization vent (314) for use in an aircraft assembly (102) is provided. The pressure equalization vent includes an opening (500) having a first end (502) and a second end (504) opposite the first end, and a first side (506)...
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JP6316801B2 |
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...
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JP6305904B2 |
A dehumidification system for use in a vehicle is provided. The system includes a thermally conductive member (230) coupled to an outer skin (218) of the vehicle, and a duct (238) at least partially circumscribing the thermally conductiv...
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JP6302897B2 |
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...
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JP6292840B2 |
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JP6281981B2 |
A cooling system for use with a galley monument having at least one galley compartment includes a heat exchanger supplying cooled air to at least one galley compartment. An airflow supply and return system has a supply duct that couples ...
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JP2018007804A |
To provide an in-cabin air cleaner capable of cleaning the air in a cabin of a vehicle, an aircraft or a ship efficiently and safely without using an agent.A bearing member is arranged on a periphery of a ceiling of a cabin, at a prescri...
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JP6261192B2 |
An aircraft (12) is provided including a fuselage comprising a passenger area (18), an occupancy zone (28), a recirculation zone (30), and a floor distribution section (22) that is coupled in flow communication to the occupancy zone (28)...
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JP6257882B2 |
The disclosure relates to a method and a system for detecting the performance of a crew oxygen system (100). The method comprising: obtaining an oxygen pressure of an oxygen cylinder (101) of the crew oxygen system, an ambient air temper...
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