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WO/2023/286799A1 |
The present invention builds a rescue system that can reliably assist rescue work of a rescuer waiting near a water mobility device. A water surveillance system in which a water mobility device (100) that can be equipped with a camera,...
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WO/2023/286785A1 |
Provided are an electric fan and an electric vertical take-off and landing craft, wherein the following are included: a boss part, a periphery part disposed around the boss part, a moving wing disposed between the boss part and the perip...
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WO/2023/282789A1 |
The invention relates to the field of aviation, and more particularly to designs for vertical take-off and landing aircraft. The present aircraft comprises a body and a power module, which are coupled to one another. The power module is ...
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WO/2023/282124A1 |
A drone 10 comprises: a detection unit 12 that, after a flying vehicle is located over a structure specified as a destination, detects, on the basis of an image of a site including the structure captured by the flying vehicle, the struct...
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WO/2023/281836A1 |
This unmanned aircraft (100) for carrying baggage (BG1) while exposing the baggage (BG1) to the outside air comprises: an unmanned aircraft body (1) which floats and travels; and an air screen part which is disposed on a lateral surface ...
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WO/2023/280903A1 |
The present invention relates to a rotor (1, 1', 1'', 1''', 1'''', 1''''') for helicopter comprising a shaft (2) adapted to be put into rotation by at least one engine element, a hub (3) splined to the shaft (2), at least four blades (4)...
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WO/2023/272489A1 |
A propeller and an unmanned aerial vehicle. The propeller comprises: a hub (10); blades (20) connected to the hub (10), the blades (20) each comprising a connecting end connected to the hub (10), and a tail end distant from the hub (10);...
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WO/2023/277847A1 |
The present invention relates to a console (C) provided in air vehicles; at least one control stick (2) located on the console (C), providing mission input to the air vehicle by the user; at least one bracket (3) allowing the control sti...
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WO/2023/272367A1 |
The present invention consists of a device that adds thrust to the blades of rotary-wing aircraft such as helicopters, comprising an air inlet (8) located approximately in the middle of the span of each blade (4), a duct (9) extending fr...
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WO/2023/276454A1 |
The control device according to the present invention comprises a processor and a memory that is connected to or built into the processor. The processor carries out, when the processor causes a rotary drive device on which a distance mea...
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WO/2023/272353A1 |
An aerial vehicle configured to fly both vertically and horizontally, suited to fighting fires or assisting search and rescue operations. The aerial vehicle has an airframe, a drive shaft, a rotor having blades that allow the angle of pi...
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WO/2022/266806A1 |
A moving platform (1000), comprising a body (200) and an obstacle avoidance assembly (100), wherein the obstacle avoidance assembly (100) is mounted on the body (200); the obstacle avoidance assembly (100) comprises a plurality of vision...
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WO/2022/269762A1 |
[Problem] The present invention makes it possible to provide an aerial vehicle in which, during flight of the aerial vehicle, the influence of wind which hits the frame in a prescribed direction is reduced, and fuel efficiency and stabil...
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WO/2022/271429A1 |
A vehicle includes a fuselage, a wing, a pylon that is coupled to the wing, and a tractor tiltrotor. The tractor tiltrotor is coupled to the pylon and is located forward of the wing; the tractor tiltrotor tilts upwards during a hover mod...
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WO/2022/266836A1 |
A heat dissipation structure, a movable platform and a heat dissipation control method. The heat dissipation structure comprises a heat dissipation bracket (100), an airflow generation assembly (200) and a shunting assembly (300). At lea...
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WO/2022/269309A1 |
The present disclosure relates to an autonomous, electric, vertical takeoff and landing (VTOL) aircraft that is low-noise, safe, and efficient to operate for cargo transportation over relatively long ranges. A VTOL aircraft includes a fu...
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WO/2022/266807A1 |
An unmanned aerial vehicle (100), comprising a fuselage (10) and a plurality of arms (20). The plurality of arms (20) are rotatably connected to the fuselage (10) to allow the unmanned aerial vehicle (100) to be in a folded state or an u...
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WO/2022/264671A1 |
The present invention addresses the problem of providing a system that, when a plurality of aircraft approach one landing field, enables safe and efficient takeoff and landing. A control device (120) according to the present invention ma...
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WO/2022/263947A1 |
A convertible aircraft (1, 1') with an airframe (2) defining a first longitudinal axis (Y) is described; a pair of half-wings (3); a first, a second, a third, a fourth, a fifth and a sixth rotor (20a, 20b, 21a, 21b, 22a, 22b) rotatable a...
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WO/2022/263777A1 |
The invention relates to an aircraft flight compensator comprising a friction module (8) that has variable friction and is coupled on one side to a drive shaft (11) and on the other side to an output shaft (13) via a kinematic chain (12)...
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WO/2022/263911A1 |
A structure for an unmanned aerial vehicle is provided. The structure includes a wing-type fuselage (20). The structure also includes at least two fixed wings (40) which form a fixed-wing platform (70) of a cropped delta wing structure w...
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WO/2022/261720A1 |
A swashplate assembly for controlling rotor blades of a rotorcraft, comprising a rotating assembly, wherein the rotating assembly is arranged to rotate with the rotor blades about an axis and is coupled to the rotor blades; a base assemb...
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WO/2022/264696A1 |
Provided are a flight vehicle operation management system and a flight vehicle operation management method for airports, said system and method enabling improved airport utilization efficiency at an airport which is for the takeoff and l...
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WO/2022/264665A1 |
Provided is a flight vehicle control system that performs proper control on flight vehicles capable of vertical takeoffs and landings and that enables the flight vehicles to perform takeoffs and landings safely in a dense state in accord...
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WO/2022/264813A1 |
Provided is a route planning device for an operation control system that enables safe and space-efficient takeoff and landing of a plurality of aircrafts simultaneously even when remarkable reduction of maneuverability occurs in an aircr...
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WO/2022/263879A1 |
The disclosure relates to hybrid unmanned aerial vehicle (UAV) having vertical take-off and landing (VTOL) capabilities. Specifically, the disclosure relates to a stable hybrid fixed angle rotor arrays UAV having VTOL capabilities with h...
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WO/2022/263881A1 |
Present disclosure discloses an Unmanned Aerial Vehicle (UAV). The UAV (100) comprises a frame (1) and an engine (3) mounted to the frame (1). A first propeller (2) is coupled to the engine (3), where first propeller (2) provides a subst...
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WO/2022/257050A1 |
A structural component (100) and a propeller protection support (103) for a multi-rotor unmanned aerial vehicle, and the multi-rotor unmanned aerial vehicle. The structural component (100) comprises a plastic member (10) and a carbon fib...
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WO/2022/260555A1 |
The invention relates to the field of aviation, and more particularly to rotary wing aircraft structures. The present aircraft comprises a fuselage, airfoils, a tail assembly, a pusher propeller disposed on the tail end of the fuselage, ...
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WO/2022/261620A1 |
A passenger vertical take-off and landing aircraft includes a flying wing comprising a passenger compartment, a first set of rotors positioned at least partially forward of a leading edge of the flying wing, and a second set of rotors po...
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WO/2022/259631A1 |
A moving body according to one aspect of the present technology comprises a body part, a notification part, and a notification control part. The notification part is provided to the body part. By controlling the operation of the notifica...
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WO/2022/259799A1 |
A control device that comprises a processor and a memory that is connected to or housed in the processor. The processor: obtains the vertical position of a marker detected by an optical sensor mounted on a flight vehicle, for a marker th...
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WO/2022/260634A1 |
This invention is about nested output shafts on the same side of the differential gearbox. The rotation of output shafts is in reverse directions and consists of differential features.
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WO/2022/260021A1 |
[Problem] To provide: a vertical takeoff/landing aircraft placement apparatus that is capable of shielding noise and high wind during takeoff/landing and taxing of a vertical takeoff/landing aircraft and that also enables prompt preparat...
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WO/2022/254808A1 |
The vibration isolation structure according to one embodiment of the present technology comprises a retaining member and first through third elastic members. The retaining member retains an imaging device and has first through third atta...
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WO/2022/254162A1 |
The invention relates to an aircraft flight compensator control system including a motor (3) and a variable-friction actuator (6) coupled to the motor and to an output shaft (8). The variable-friction actuator includes a variable-frictio...
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WO/2022/255208A1 |
Provided are a flying vehicle and a flying vehicle guard that can prevent a fall in the event of collision, while ensuring the visibility of surroundings. More specifically, a flying vehicle 1 is a vehicle capable of flying. The flying v...
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WO/2022/253285A1 |
A building convenient for fire extinguishing and related devices and technology used during a fire-extinguishing process. An aircraft carries fire-extinguishing devices such as a glass breaking apparatus and a spraying apparatus, and sai...
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WO/2022/254894A1 |
A control device (19) for controlling a drive motor (12) for driving a rotary wing (30) that an electric aircraft (100) is equipped with, the control device (19) controlling the drive motor so as to make the same selectively operate in o...
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WO/2022/249319A1 |
In this invention, a management server 2 calculates, on the basis of the weight of articles included in each of a plurality of orders, a total weight of the plurality of articles to be loaded on a UAV1 and compares the calculated total w...
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WO/2022/242458A1 |
A multi-layer swing rotor wing vertical reaction force strong wind-resistant aircraft. When the aircraft is in an energy saving mode, a lower swing wing (6) rotates to generate a sidewise and upward lift force to form a resultant force t...
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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/2022/244933A1 |
The present invention relates to a folding-type transport drone which facilitates storage and transportation of a drone, when a large-sized transport drone is stored and transported, by folding and transforming a body of the drone into a...
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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/2022/241974A1 |
A tilting structure and an aircraft comprising the tilting structure. The tilting structure comprises a machine arm (100), a tilting electric motor (200) arranged on the machine arm (100), and a power electric motor assembly (300) in tra...
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WO/2022/239580A1 |
This mooring system is for mooring a floating structure to a mooring facility, one of the floating structure and the mooring facility serving as a first object and the other as a second object. The mooring system comprises: a mooring lin...
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WO/2022/236820A1 |
Provided are a propeller, a power apparatus, a power system, and a multi-rotor unmanned aerial vehicle. The power apparatus comprises a driving motor (70) used for being connected to a propeller (2) to drive the propeller (2) to rotate; ...
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WO/2022/238653A1 |
A power management system for an aircraft with a hybrid power source comprises at least one rechargeable electricity source and an electricity generating source, a detector (200) arranged to determine, on the one hand, status data indica...
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WO/2022/239342A1 |
The present invention provides a ducted fan apparatus and an aircraft that can achieve suppression of lip separation, increase in thrust, improvement of silencing property, and the like. This ducted fan apparatus comprises: a plurality o...
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WO/2022/234858A1 |
Provided is an engine device for an unmanned flying object, the engine device giving the aircraft body a favorable weight balance and being capable of cancelling out gyro effects and capable of autorotation of propellers. The engine de...
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