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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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WO/2022/227054A1 |
A propeller, a power set, and an unmanned aerial vehicle, the propeller comprising a propeller clamp (10), at least two blades (11), and at least two rotating shafts (12); connecting ends (111) of the blades (11) are provided with throug...
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WO/2022/226932A1 |
An unmanned aerial vehicle, comprising a fuselage (1), at least two front arms (21) and at least two rear arms (22); the at least two front arms are symmetrically connected to the front end of the fuselage; the at least two rear arms are...
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WO/2022/229958A1 |
The present invention provides a method for on-site identification of damaged fruits and ripeness assessment, immediately after picking/harvesting, thereby enabling discarding damaged fruits on-site without delivering such damaged fruits...
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WO/2022/231554A1 |
The present invention relates to a body (2) provided at air vehicles; at least one rotor (3) extending longitudinally out of the body (2) and rotating around an axis along which it extends; at least one blade (4) connected to the rotor (...
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WO/2022/226933A1 |
A vertical takeoff and landing fixed-wing unmanned aerial vehicle, comprising a vehicle body (1), multiple arms (2) connected to the vehicle body, and a propeller (3) connected to the end of each arm away from the vehicle body, the prope...
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WO/2022/230561A1 |
The present invention provides a float that provides a higher degree of freedom in the installation location of an air hole for reducing deformation of the float body associated with the expansion or contraction of an internal gas due to...
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WO/2022/224331A1 |
Provided is a configuration of an aircraft, the configuration being lightweight and capable of absorbing vibration generated by driving of an engine-generator unit. An aircraft 1 comprises: a plurality of rotors 5 which generate a lift a...
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WO/2022/226012A1 |
An actuator transfer assembly comprising an actuator (18), a driven object (16, 116), a pushrod (19) or shaft (119), a disconnect housing (24, 124), a transfer member (50) movable relative to the housing from a first position in mechanic...
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WO/2022/221916A1 |
Some embodiments relate to a system for communicating with vertical take-off and landing (VTOL) aerial vehicles. An example system comprises: a central server system comprising: a central server system wireless communication system; at l...
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WO/2022/223680A1 |
The invention relates to a multicopter comprising a main part (10) and multiple rotors (22) which are arranged on the main part (10) and which are coupled to at least one drive (24) and generate lift and propulsion by rotating, wherein a...
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WO/2022/225421A1 |
The invention relates to the field of aviation, and more particularly to designs for compound aircraft capable of vertical take-off and landing and of horizontal flight in copter mode, with the axes of rotation of the propellers in a nea...
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WO/2022/224456A1 |
[Problem] To provide a technology capable of stabilizing a frame of an aircraft. [Solution] The primary invention of this invention for solving the above-mentioned problem is a frame assembly for an aircraft, the frame assembly being cha...
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