Login| Sign Up| Help| Contact|

Patent Searching and Data


Matches 101 - 150 out of 57,454

Document Document Title
WO/2022/087207A1
An aircraft electrical power supply system includes a fuel cell auxiliary power unit (APU) that supplies auxiliary electrical power to an aircraft, a fuel cell power plant that supplies primary electrical power to the aircraft, and a hyd...  
WO/2022/084629A1
The invention relates to a method for manufacturing an air inlet lip, which comprises: - placing a blank opposite a three-dimensional forming surface of a die of a hydroforming tool, the three-dimensional surface comprising an outer annu...  
WO/2022/084630A1
The invention relates to a method for manufacturing an air inlet lip, comprising: - supplying a sheet of sheet metal, - cutting the sheet of sheet metal to form a ring, - mechanically machining one or more regions of reduced thickness in...  
WO/2022/082415A1
A method for controlling the ejection overload of a rocket ejection seat, the method comprising: step 1, by means of calculating ballistic performance, obtaining a stroke of a dynamic response index (DRI) at 21ºC and the minimum ejectio...  
WO/2022/086796A1
A system and method for evaluating runway conditions that combines known brake control systems with a new runway condition monitoring unit working in conjunction with an anti-skid/brake control unit to improve runway condition evaluation...  
WO/2022/085745A1
[Problem] To enable improvements in the safety of a flying body with regards to wind. [Solution] A safety management system according to the present invention comprises an acquisition unit that acquires a predicted value of wind speed. T...  
WO/2022/084628A1
A method for manufacturing annular sectors of an air intake lip (70, 71), comprising: the placement of a blank with a shape exhibiting symmetry of revolution with regard to a three-dimensional forming surface of a die of a hydroforming t...  
WO/2022/084241A1
The invention relates to a self-cleaning external layer (22) comprising a self-cleaning aerodynamic surface (S) configured to extract at least some of the oxygen present in the atmosphere (A) in contact with the aerodynamic surface (S) s...  
WO/2022/085325A1
An obstacle detection unit (202) detects obstacles in the surroundings of a mobile body (20) that can fly. A position acquisition unit (203) acquires the position of the mobile body (20). An obstacle information reception unit (204) rece...  
WO/2022/082383A1
A self-locking structure (100), an arm assembly (300) and a movable platform (1000), the self-locking structure (100) comprising a mounting member (10), a movable member (20) and a self-locking assembly (30). The movable member (20) is r...  
WO/2022/085259A1
A terminal control device 300 of a client 30 of an image provision system 1: stores location information of construction stakes 41-45; when an operator selects construction stake 42 among the construction stakes 41-45, transmits a flight...  
WO/2022/083881A1
The present invention relates to a coupling device for fastening a shipping container to an unmanned air vehicle or to a manipulator; to a shipping container for indirect fastening to an unmanned air vehicle or to a manipulator by means ...  
WO/2022/082441A1
A gimbal and a gimbal control method. The gimbal control method comprises: acquiring attitude information of a gimbal; determining, according to the attitude information, whether the gimbal is in a falling state; and when the gimbal is i...  
WO/2022/085225A1
Provided is an aircraft restroom unit that enables passengers to disinfect hands and fingers every time a passenger uses the aircraft restroom unit, and is advantageous in preventing COVID-19 on board. The skeleton frame 22A of an airc...  
WO/2022/082962A1
An aircraft propulsion system. The system comprises: a control apparatus, rotary power sets and fixed power sets, wherein the control apparatus is used for sending a target working mode to the rotary power sets and the fixed power sets a...  
WO/2022/083073A1
An unmanned aerial vehicle landing pad self-cleaning system based on multisensor fusion. A landing pad refers particularly to a contact face on which an unmanned aerial vehicle lands. The landing pad is generally located inside a bigger ...  
WO/2022/086321A1
A ground effect flight vehicle comprising, a fuselage (1), a wing assembly (4, 5), an engine assembly comprising one or more engines or engine sets (6, 7, 8), and a hull (2) for enabling floatation of the vehicle; wherein the wing assemb...  
WO/2022/087607A1
An aircraft with a variety of control surfaces including but not limited to multiple winglet rudders. Each winglet can have multiple independently controlled rudders to improve the flight stability and maneuverability of the aircraft. Ad...  
WO/2022/086523A1
Described are tray tables for passenger seats having a first surface, a second surface opposite from the first surface, and at least one of a pocket, a control panel, or a table support. The pocket may be defined in one of the surfaces o...  
WO/2022/082301A1
A system for generating a labelled dataset is provided. The system comprises processing means configured to: receive first data wherein the first data comprises one or more frames and wherein the first data comprises data defining an obj...  
WO/2022/083129A1
A smart elastic bearing and a control method. The smart elastic bearing comprises smart polymer material layers (3), metal spacer layers (4) and two joints (1, 2). One of the joints is used for connecting a rotor blade, and the other joi...  
WO/2022/085832A1
The present invention relates to an individual personal air vehicle operable on water, the personal air vehicle comprising: a lower body which supports an occupant and has a float on the floor surface, a front arm holder and a rear arm h...  
WO/2022/085224A1
Provided is an arrangement structure for a pump-type bottle inside an aircraft cabin, said structure: being advantageous in preventing the spread of the novel Coronavirus inside the aircraft cabin; and making it possible to arrange a pum...  
WO/2022/080916A1
A device for supporting takeoff and landing of an aerial vehicle is provided. The device comprises: a plate which is disposed on a target takeoff and landing surface and configured to be able to maintain an aerial vehicle; a moving body ...  
WO/2022/077238A1
An imaging display method, a remote control terminal (30), a device, a system, and a storage medium. The present invention is applied to the remote control terminal (30). The remote control terminal (30) is communicationally connected to...  
WO/2022/077290A1
A multi-rotor unmanned aerial vehicle, comprising a frame (10), rotors (20), and an elastic member (30). Each rotor (20) comprises a motor (21), a propeller (22), and a fixed member (23); the motor (21) is mounted on the frame (10); the ...  
WO/2022/079415A1
A method of manufacturing an aircraft aerofoil such as a winglet. The aircraft aerofoil comprises: a first cover, a second cover, an aerofoil leading edge, and an aerofoil trailing edge where the first and second cover are joined at a tr...  
WO/2022/077152A1
A clamping and fixing device (300) for clamping components of a multi-rotor unmanned aerial vehicle (100). The clamping and fixing device comprises a main body part (310); a first side of the main body part (310) is provided with a clamp...  
WO/2022/080289A1
The present invention realizes a pickup system in which, even when a package is carried by using one unmanned aerial vehicle, the unmanned aerial vehicle or the package is unlikely to be inclined. A pickup system (1) includes a holder (1...  
WO/2022/079522A1
A gas flow generator (200, 500) for generating a gas flow in a quiescent volume includes an inlet module (202) configured to receive a gas (216); a measuring module (204) configured to measure a parameter associated with the gas (216); a...  
WO/2022/079411A1
According to the present disclosure there is provided a transmitter unit for providing power and data to an unmanned aerial vehicle (UAV), the transmitter unit comprising: a free-space optical transmitter configured to generate and trans...  
WO/2022/079722A1
An insect distribution device to be carried by drone to distribute insects from the air, comprises a source of passive cooling; an insect chamber; one or more insect containers in said insect chamber; and a release point. The source of p...  
WO/2022/079360A1
The invention relates to an assembly for a turbine engine blade, the assembly comprising a fastener (9) defining a well (10) for receiving a blade root (7), and a clamping device (32) for clamping the blade root (7) against the fastener ...  
WO/2022/077285A1
A multirotor unmanned aerial vehicle, comprising a frame (10), forward-rotation rotors (20), and reverse-rotation rotors (30). Each forward-rotation rotor (20) comprises a first motor (21), a first propeller (22), and a first elastic mem...  
WO/2022/078258A1
The present disclosure relates to a flapping wing aircraft, the flapping wing aircraft comprising an empennage mechanism, the empennage mechanism comprising a tail rudder stabilizer; and the tail rudder stabilizer comprises a first tail ...  
WO/2022/080512A1
The present application relates to a control stick for a military aircraft, a system for managing health information regarding a pilot, a military aircraft, and a simulator for a military aircraft. According to the control stick for a mi...  
WO/2022/080546A1
The present invention relates to an exhaust duct assembly and an aerial vehicle including same. The exhaust duct assembly according to an embodiment of the present invention is disposed in a low-pressure turbine unit of a gas turbine eng...  
WO/2022/080232A1
This flying body is provided with: a front rotor 10 provided on a front portion of a fuselage; a rear rotor 12 provided on a rear portion of the fuselage; a front deflecting mechanism which changes the angle of the front rotor 10 relativ...  
WO/2022/080208A1
Provided is a space navigating body that, while having a relatively simple configuration enabling reduction in size, makes it possible to capture an object without the need of highly accurate positioning. A space navigating body 1 is pro...  
WO/2022/081243A1
CERMET fuel element includes a fuel meat of consolidated ceramic fuel particles (preferably refractory-metal coated HALEU fuel kernels) and an array of axially-oriented coolant flow channels. Formation and lateral positions of coolant fl...  
WO/2022/082099A1
An air purification system for a passenger cabin of a transport vessel. The air purification system comprises an elongated air compartment having a panel, with a plurality of openings along the panel. Air filters reside within the variou...  
WO/2022/078257A1
An ornithopter, comprising: a crank transmission assembly (100) mounted on the fuselage of the ornithopter, and comprising a first transmission mechanism (101) and a second transmission mechanism (102), which are arranged about the cente...  
WO/2022/079474A1
A light garment that can be made by filling up the Hydrogen (H2) into the garment so that it has the function of resisting gravity particularly when there is a fire in high rise buildings and residents need to jump off the building or th...  
WO/2022/081129A1
A ground power system for supplying electrical power to an aircraft and method of using the same is disclosed in which an electric motor is connected to an aircraft wheel to drive the aircraft wheel, an autonomous vehicle battery carrier...  
WO/2022/077177A1
An unmanned aerial vehicle (100) comprises a fuselage (110), a spraying device (120) and a controller (130). The spraying device comprises a support (121), at least two spray nozzles (122) and a driving mechanism (123). The support is co...  
WO/2022/078092A1
An unmanned aerial vehicle (100), comprising: a fuselage (10) having a first accommodating cavity and a second accommodating cavity; a first wing (20) and a second wing (30) arranged on the two sides of the fuselage; a first rotor assemb...  
WO/2022/079187A1
Aircraft landing gear comprising: a strut mounted on an aircraft structure such that it can move between an extended position and a retracted position; a bracing member for holding the strut in the extended position, comprising a first c...  
WO/2022/079435A1
An aircraft (101) comprising: one or more main engines (104a, 104b); a first fuel in a first fuel tank (111a) configured to be fed towards at least one of the one or more main engines through a first fuel line; and a second fuel differen...  
WO/2022/079309A1
A system (49) for loading containers into and unloading containers from a cargo vehicle (51) and having a storage module (1) for storing multiple containers and comprising a storage array (3) having columns of storage locations (7), wher...  
WO/2022/080626A1
A device for supporting takeoff and landing of an aerial vehicle is provided. The device comprises: a plate which is disposed on a target takeoff and landing surface and configured to be able to maintain an aerial vehicle; a moving body ...  

Matches 101 - 150 out of 57,454