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WO/2022/248202A1 |
Disclosed is a method of determining an operating condition of a valve of an aircraft system. The method includes obtaining a first time period associated with actuating the valve, and a second time period associated with actuating the v...
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WO/2022/248631A1 |
A remote control system for an aircraft, comprising: - an aircraft, of the Magnus-effect type, comprising a cylinder (1) extending along a longitudinal axis (Y), the cylinder (1) being able to rotate about the longitudinal axis (Y); - a ...
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WO/2022/247027A1 |
Provided are a deicing fluid tank (1) internally provided with an electric heating device (2); a deicing fluid filling station provided with the deicing fluid tank (1); a deicing fluid replenishing vehicle, comprising a vehicle chassis (...
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WO/2022/248742A1 |
System for inspecting the hose used in refueling operations, consisting of a set of image sensors and electromagnetic radiation emitters in a ring that follows the vertical movement and inclination of the hose and allows the hose to pass...
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WO/2022/247050A1 |
A positive design method for an osculating curved surface waverider suitable for a complex leading edge shape, which realizes, by solving a shock wave curved surface corresponding to a leading edge profile, the function of designing a wa...
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WO/2022/243606A1 |
A device for securing objects, such as reflectors, to an aerial line comprises a frame (10), a suspension member (12) for suspending from a flight device, connecting members for connecting to the aerial line and an installation mechanism...
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WO/2022/243764A1 |
A computer- implemented method is described (19) for detecting anomalies in a transmission system (1) of an aircraft (HC1) equipped with a monitoring system (10, MS), which includes a number of sensors (A1-A13) coupled to the transmissio...
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WO/2022/237300A1 |
A lever structure which has an anti-jamming function, comprising a lever body, and a first anti-wear hemispheroid (18) movably mounted at the top part of the lever body by means of an anti-wear assembly. The anti-wear assembly comprises ...
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WO/2022/239141A1 |
[Problem] To provide a device for restricting the position of a suspension member, by which it is possible to improve the positional accuracy of a flight vehicle by use of a simple mechanism. [Solution] This device for restricting the po...
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WO/2022/231478A1 |
The invention relates to takeoff and acceleration systems for unmanned aerial vehicles. A method comprises the launching and acceleration of aircraft up to take-off speed using the mortar method, characterized by opening the aircraft noz...
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WO/2022/229197A1 |
The invention relates to a main body (1) of an aerial vehicle, made of fibre-reinforced composite material, and to a method for producing a main body (1) of an aerial vehicle. The main body (1) of the aerial vehicle has a load-bearing st...
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WO/2022/230406A1 |
The present invention can provide a more simplified system for operation management and assistance for an aircraft.　Said system has: an aircraft operation management device provided with a guidance information generation unit that gene...
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WO/2022/229944A1 |
Disclosed herein is a system for transporting items having two or more robots configured to transport items throughout a facility, each robot transfers the items along a designated robot route, one or more automated carts configured to t...
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WO/2022/224874A1 |
The present invention provides a wireless relay system of the wired feeder type that can stop transmitting radio waves and stop operations safely when a mooring line (feeder line) is disconnected for some reason. In the wireless relay sy...
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WO/2022/219781A1 |
This ocean monitoring system comprises a control device 1 and at least one flying body 2, wherein the control device 1 comprises: a sensor unit 13 that measures an undersea environment and/or sea-surface environment to acquire ocean data...
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WO/2022/218461A1 |
The invention relates to an anemometer (10) for measuring wind speeds, containing a housing (16) and/or frame. A shaft (20) is mounted such that it can rotate in a bearing of the housing (16) and/or frame. Wind capturing means (14) are a...
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WO/2022/215429A1 |
An aircraft monitoring system (10) monitors a fuselage (120) of an aircraft (100) and comprises an imaging device (12) that is attached to the fuselage and acquires captured images obtained by capturing an operation unit (40) related to ...
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WO/2022/217253A1 |
System (100) for determining a health state of component (104) includes processor (108) and non-transitory computer-readable storage medium (110) that stores a plurality of computer-executable instructions thereon. Processor (108), in re...
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WO/2022/217262A1 |
A pump health monitoring system is provided. Such a system includes one or a plurality of data capture devices that together collect a multiple variable data set relating to a device being monitored such as a water pump device for a pool...
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WO/2022/206562A1 |
The present disclosure provides a method for controlling an unmanned aerial vehicle to return to a hangar, comprising: S101: at a first preset height, searching for and identifying a first identifier by means of a gimbal camera; S102: wh...
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WO/2022/206136A1 |
An automatic ramp, comprising a cockpit (1) and a trailer (2). The trailer (2) is provided with support columns (4), a ramp frame (6) is fixedly connected to one side of the top end of each support column (4), a chain wheel (7) and a bel...
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WO/2022/208655A1 |
Provided is a passenger boarding bridge with which it is possible to prevent interference between a door of a large aircraft and a cab before the door is completely opened. One example of a passenger boarding bridge according to the pres...
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WO/2022/208601A1 |
Provided is a passenger boarding bridge that can accurately move a cab to a target position. An example of this passenger boarding bridge comprises first and second cameras that capture images of the boarding portion of an aircraft, and ...
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WO/2022/204056A1 |
A device receives a data query from a source, the data query associated with a hardware component. The device determines a likelihood that an aircraft of an aircraft entity associated with the data query will require the hardware compone...
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WO/2022/202165A1 |
Provided is an inspection device (100) for inspecting an aircraft, the inspection device (100) comprising: one or more rotary wings (30); wheels (9) for taxiing; and an information acquisition unit (6) which acquires airframe-related inf...
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WO/2022/203498A1 |
An ultraviolet disinfection system (10) for disinfecting multiple surfaces of a moving object comprising at least one disinfection modules; at least one ultraviolet light disinfection sources (12); at least one removable side panels (14)...
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WO/2022/193079A1 |
Provided are an unmanned aerial vehicle system, and a control method and control apparatus for an unmanned aerial vehicle. The unmanned aerial vehicle system comprises an unmanned aerial vehicle (1), an accommodation box (2) for accommod...
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WO/2022/189129A1 |
An ultraviolet radiation cleaning system for baggage trays (3) in an airport security environment, comprising a radiation tunnel (7) with an input (1) for dirty trays (3) and an output (8) for clean trays (10), wherein at the input (1) a...
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WO/2022/154887A9 |
A docking system for unmanned aerial vehicles (UAVs) includes a docking housing that defines a docking compartment, and a docking assembly coupled to the docking housing and configured to suspend the UAV within the docking compartment. T...
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WO/2022/190012A1 |
The present discloses a system for washing and de-icing of aircrafts. The preset invention provides a washing and deicing area comprising one or more gantries to ensure different steps of the washing or the de-icing process. The structur...
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WO/2022/190667A1 |
Provided is a passenger boarding bridge with which it is possible to reduce excessive raising/lowering operations by an operator and shorten the docking time when docking a cab to an aircraft. One example of a passenger boarding bridge a...
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WO/2022/192607A1 |
A fixed-wing, powered, non-buoyant, enclosed cargo aircraft design for carrying low-density wind turbine components is disclosed. The cargo aircraft can include a fuselage defining a forward end, an aft end, and a continuous interior car...
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WO/2022/189235A1 |
The invention relates to a method and a computer program product for monitoring a bleed air supply system (10) of an aircraft. The method according to the invention for monitoring a bleed air supply system (10) of an aircraft, having at ...
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WO/2022/191838A1 |
A fixed-wing cargo aircraft having a kinked fuselage is disclosed. The fuselage contains a continuous interior cargo bay, and includes a forward portion, an aft portion, and a kinked portion forming a junction in the fuselage between the...
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WO/2022/192608A1 |
Systems to reduce the loads on highly flexible aircraft cargo, such as wind turbine blades, are disclosed. Such systems can be active and/or passive. Active systems can be in the form of open or closed loop active control systems compris...
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WO/2022/191279A1 |
A seat determination system according to one embodiment determines a seat arrangement for each of a plurality of passengers in a flying body comprising a plurality of seats for passengers, the seat determination system comprising: a weig...
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WO/2022/189723A1 |
A system for controlling the aeraulic conditions present above an aerial arrival zone (Z) comprises anemometric means and aeraulic means. The anemometric means deliver speed and bearing values that characterise a relative wind speed with...
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WO/2022/186777A1 |
A method of localizing a mobile robot 100 with respect to a target object 601 using an initial map of a reference object which is a representation of the target object is disclosed herein. The method comprises obtaining LiDAR data 503 of...
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WO/2022/186026A1 |
[Problem] To provide a compact port with which the reliability of loading can be increased with a simple mechanism while also keeping costs low. [Solution] The port according to the present disclosure has a loading part that turns about ...
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WO/2022/183570A1 |
A method and apparatus for collecting and utilizing relative motion kinetic energy of a vehicle. A reversible power device is adopted in advance and is driven by stored energy to reach a fast speed, and then a relative motion kinetic ene...
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WO/2022/186556A1 |
An unmanned aerial vehicle storage device according to an embodiment of the present invention comprises: a transmission connection unit which is recessed at one side to have a transmission recessed unit into which an electricity receivin...
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WO/2022/182803A1 |
An autonomous vehicle (AV) delivery system is configured to deliver a payload or package in a rural and/or urban environment. The AV delivery system includes a first autonomous vehicle (AV). The first AV is configured to travel between a...
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WO/2022/179679A1 |
The present invention concerns a pre-conditioned air (PCA-) device for conditioning air in an interior of a cabin of a parked aircraft (12) and for sanitizing an air and surfaces in the interior of the cabin, the PCA-device comprising: a...
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WO/2022/181864A1 |
The present invention relates to a jig system for aircraft assembly, wherein the jig system is for solving the problems of the related art. The jig system for aircraft assembly comprises: a lower support (100) for arranging a plurality o...
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WO/2022/177544A1 |
An off-aerodrome servicing of unmanned aerial vehicles comprising a device for catching and launching a guided UAV (19), the device comprises a supporting post (1), a horizontal shaft (7) mounted on the post, and a lever (2) is mounted o...
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WO/2022/178500A1 |
A method for assigning swappable battery packs to electric aircraft includes receiving, at a computing system, status information for a plurality of battery packs (200, 302, 304, 402, 502, 900) located at at least one battery swapping lo...
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WO/2022/170888A1 |
Provided are a spacecraft launch system and launch method, and a spacecraft. The spacecraft launch system comprises: a pulley block (1), a flexible cable (3), a spacecraft (5), a separation device (6), a decoupling and slow-down device (...
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WO/2022/170401A1 |
The present invention is directed to systems and methods for monitoring activities in an aviation environment. The system includes at least two monitoring units, each including at least two types of sensors, wherein: the sensors are moun...
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WO/2022/173839A1 |
A tiltrotor aircraft is designed to accommodate rotors of different diameters, as well as corresponding wings and fuselages with different span and length, while maintaining very high parts commonality, especially with respect to drive t...
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WO/2022/172987A1 |
[Problem] To provide a work system that can better stabilize the attitude of an airframe during work using the airframe. [Solution] The work system according to the present disclosure comprises rotors 3, an airframe 2 that supports the r...
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