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WO/2022/210559A1 |
According to the present invention, a first seal (9) and a second seal (10) sandwich a retainer (8), thereby sealing an annular space between an outer ring (5) and an inner ring (6). A stator (12) including a coil (16) is supported by th...
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WO/2022/208126A1 |
The present invention has improved the existing blades without changing its shape and using special mechanisms in such a way that in addition to the ability to adjust the blade length, it does not change the shape of the blade. Also, the...
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WO/2022/209261A1 |
Provided is an information processing method executed by one processor or a plurality of processors in cooperation, the information processing method comprising: an estimation step of estimating a relative position or a relative posture ...
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WO/2022/204572A1 |
A detachable, self-balancing, pod for an unmanned aerial vehicle. The pod is configured to hold a plurality of different payloads, and to dynamically shift the location of these payloads in order to maintain an optimal center of mass (ce...
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WO/2022/203948A1 |
Disclosed herein is a helicopter flight support for use in case of emergencies. The helicopter flight support comprises a motor which causes a threaded shaft to turn which is coupled to an underside of the helicopter. This causes outer s...
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WO/2022/200842A1 |
An apparatus for a rotorcraft is disclosed. The apparatus includes a body. The body includes an upper cabin which includes a cockpit. The body also includes a lower cabin operatively coupled beneath the upper cabin of the rotorcraft via ...
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WO/2022/204048A1 |
The present disclosure provides a rotating propeller design that maintains a high efficiency and reduces noise. The design provides an unloaded tip zone of positive lift starting prior to an end of the tip with negligible, if any, positi...
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WO/2022/200853A1 |
A description is provided of a planetary gear (21; 21'') comprising a sun (15) rotatable around a first axis (B), a crown (17) angularly fixed with respect to the first axis (B); two satellites (19) that are meshing, rotatable around res...
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WO/2022/193156A1 |
An unmanned aerial vehicle (100), comprising: a rack (110); a buoyance apparatus (120), mechanically coupled to the rack (110), wherein the buoyance apparatus (120) can be in an open state or a closed state, and when being in the open st...
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WO/2022/196515A1 |
[Problem] To provide a flight control system with which it is possible to perform safe manual steering of a flying body without requiring advanced steering technology. [Solution] The flight control system according to the present inventi...
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WO/2022/195747A1 |
[Problem] To provide a flight vehicle having a more fundamental structure and provided with safety measures. [Solution] This flight vehicle comprises a main body part, a thrust part provided with one or more thrust means, a connection pa...
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WO/2022/197686A1 |
The present disclosure discloses a bridle (100) for a vehicle (200). The bridle (100) being connected to the vehicle (200) and which creates a pivot point (P) located at a location selected from: above the vehicle's (200) center of gravi...
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WO/2022/193157A1 |
A multi-rotor aerial vehicle (10), comprising a fuselage (11), arms (12), and first rotor power devices (13) and second rotor power devices (14) mounted on the arms (12). The fuselage (11) comprises a head (11a) and a tail (11b); the fir...
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WO/2022/197211A1 |
Rotary systems are driven by jet engines disposed on the end of a rotor comprising a structure that rotates about a rotary shaft. A jet stream produced by a jet engine generates thrust orthogonal to the radius of the rotor, thereby stimu...
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WO/2022/193139A1 |
An unmanned aerial vehicle (100), comprising a vehicle body (10), two arm assemblies (30), and power assemblies (40). The vehicle body (10) comprises a top portion (12) and a bottom portion (14) opposite to the top portion (12). The two ...
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WO/2022/189651A1 |
An unmanned aerial vehicle comprising: a housing comprising an outer surface and an inner surface that forms a cavity, at least one propulsion device adapted to move the chassis in three dimensions, one or more first electrical component...
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WO/2022/189898A1 |
An aircraft (1) capable of hovering is described, comprising a motor member (10); a rotor (5) connected to the motor member (10); a transmission shaft (11) rotatable around a first axis (B) and adapted to drive the rotor (5); and a trans...
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WO/2022/192398A1 |
A mobile emergency power generation and vehicle propulsion power system, method, and apparatus for full-scale, clean fuel, electric-powered vehicles having a fuel cell module including a plurality of fuel cells working together to proces...
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WO/2022/190370A1 |
A compound helicopter (10) comprises: a fuselage (20); a first main wing (31) extending from the fuselage to the right and a second main wing (32) extending from the fuselage to the left with respect to the direction of travel of the fus...
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WO/2022/183361A1 |
A multi-rotor unmanned aerial vehicle, the vehicle comprising: a vehicle arm (20), wherein a connecting portion (21) is arranged at an end surface of one end of the vehicle arm (20) in a lengthwise direction, and a rotor device (40) used...
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WO/2022/180755A1 |
An aircraft 1 takes off vertically. The aircraft 1 comprises: a fuselage 10; one or more pairs of fixed wings (20-1 to 20-4) which extend from the fuselage in the right/left direction; and a plurality of first rotor blades (402-1, 402-2)...
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WO/2022/180754A1 |
An aircraft 1 that takes off and lands vertically. The aircraft 1 comprises a fuselage 10, at least one pair of fixed wings 20–1–20–4 that extend from the fuselage 10 in the left/right direction, a plurality of first rotor blades 4...
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WO/2022/181130A1 |
The present invention realizes a configuration that enables a target landing position for a drone to be determined in accordance with a sentence generated by a user indicating a landing position. The present invention is configured to ex...
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WO/2022/181360A1 |
[Problem] To provide a flight body in which arrival position precision of cargo can be improved. [Solution] This flight body comprises a mounting unit that holds a mounted object, and has a movement means that holds the mounted object vi...
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WO/2022/180968A1 |
An aircraft 1 performs vertical takeoff and landing. The aircraft 1 comprises: a fuselage 10; two pairs of fixed wings 20-1 to 20-4 that extend in the left and right directions from the fuselage; a plurality of rotary wing modules 40-1 t...
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WO/2022/179278A1 |
A rotor blade downwash impact correcting method for a helicopter atmospheric data system, comprising the following steps: step S1: establishing a dynamic pressure correction coefficient table Kp; step S2: establishing a synthetic angle o...
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WO/2022/181150A1 |
[Problem] To highly precisely detect an airflow velocity and an airflow direction with respect to an airframe of an electrified aircraft and to quickly control an electric propulsion system and the attitude of the airframe in response to...
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WO/2022/174998A1 |
The invention relates to an assembly for controlling the blade position of rotor blades (17) on a rotor, containing a two-part swash plate (10; 100) with a rotating part (12; 112) and a non-rotating part (14; 114) which is connected to t...
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WO/2022/176967A1 |
The present invention provides a mechanism and device that can increase a degree of freedom in the arrangement of the center of rotation of a rotary body with respect to a rotation reference. The present invention also provides a system ...
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WO/2022/174712A1 |
A quadrotor unmanned aerial vehicle, comprising two sets of binocular sensors and two sets of fish-eye binocular sensors, wherein the two sets of binocular sensors are respectively diagonally arranged on the body of the unmanned aerial v...
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WO/2022/172793A1 |
Recently, jobs involving the transport of goods, tasks involving the survey of a wide area, etc., using a multicopter have increased, and it has become necessary for multicopters to fly for long periods of time. In the present invention,...
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WO/2022/171727A1 |
The invention relates to a propulsion system (1) for an aircraft, which propulsion system comprises a rotor (2; 2b; 2c) having a rotor main body (4-4c) and rotor blades (3; 3b; 3c) attached to the rotor main body (4-4c), wherein air can ...
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WO/2022/168536A1 |
[Problem] To provide an unmanned aircraft which can comprise a pruning structure that can prune trees, and that can increasing safety. [Solution] This unmanned aircraft 2 comprises: a pruning structure 23 that can prune trees; a storage ...
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WO/2022/168535A1 |
[Problem] To provide a device for controlling an unmanned air vehicle and an unmanned air vehicle system, with which pruning positions where the branches of a tree will be pruned can be appropriately designated, the tree can be pruned, a...
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WO/2022/168793A1 |
The present invention provides a safety device that can control a landing point when a flight vehicle falls. The safety device is provided in a flight vehicle and comprises: a first parachute that slows the rate of fall and controls the ...
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WO/2022/163271A1 |
A flying body (100) provided with a propeller (20) on a main body (10) comprises: a travel device (30) having a ground contact surface (31) that contacts an object to be inspected; and a control device that controls at least the propelle...
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WO/2022/164468A1 |
A system and method for capturing an unmanned aerial vehicle includes a net configured to receive the unmanned aerial vehicle, an infrared emitter arrangement including a plurality of infrared emitters arranged around the net, an infrare...
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WO/2022/163116A1 |
One purpose of the present invention is to provide a movement prediction device that can predict the movement of a flying vehicle with a high degree of accuracy. This movement prediction device (100) comprises: a first light output dev...
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WO/2022/159951A1 |
A system and method for controlling a multi-rotor aircraft that implements the unconventional use of different sized rotors. The different sized rotors than the main rotors tend to generate an unbalanced torque and pitch on the aircraft ...
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WO/2022/156854A1 |
The invention relates to a flight module for a vertical take-off and landing aircraft with a plurality of drive units arranged on a support structure, wherein the support structure comprises elongate support beams joined to one another a...
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WO/2022/157709A1 |
A damping rod (1) configured to connect a first and a second element of a vehicle, comprising an intermediate body (2) and a first and a second anchoring element (3, 4) carried by the intermediate body (2), the intermediate body (2) bein...
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WO/2022/157371A1 |
An object detection system and/or collision avoidance and/or surveillance and/or safety system sensor system for a rotorcraft, comprising a detector () which is mountable on, or forms part of, a rotary wing.
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WO/2022/157152A2 |
The present invention relates to an aircraft and to a method using this aircraft to inspect equipment in coking plants for detecting sources of error. The aircraft has at least one inspection device for inspecting surfaces of the equipme...
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WO/2022/158011A1 |
[Problem] To provide a flying object and communication system with which, by using an antenna capable of receiving information transmitted from a transmission antenna having a range wider than an antenna for linearly directed use, it is ...
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WO/2022/151219A1 |
A propeller assembly (10), a power system (100), and an unmanned aerial vehicle (1000), the propeller assembly (10) comprising a propeller (11) and first fittings (12); the first fittings (12) are mounted on the propeller (11), and the f...
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WO/2022/154059A1 |
The present invention is provided with: a fan (10) for producing an airflow; a rotor core (20) provided radially outward of the fan (10); a stator core (40) that faces the rotor core (20); a housing (30) which forms an inner peripheral s...
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WO/2022/153784A1 |
A drone control system (100) comprises a destination determination unit (114) and a movement instruction unit (115). The destination determination unit (114) determines the destination of a drone (101) from a plurality of standby locatio...
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WO/2022/154683A1 |
The invention relates to the field of aviation, and more particularly to rotary wing aircraft structures. The present rotary wing aircraft has a fuselage, a skid-type landing gear, a main rotor, an engine, a tail boom, and a tail rotor f...
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WO/2022/154684A1 |
The invention relates to the field of aviation, and more particularly to helicopter main rotor structures. A helicopter main rotor has a main rotor hub and main rotor blades. The main rotor hub has a housing and pitch hinges, one for eac...
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WO/2022/150194A2 |
A method and system of calculating and executing an optimized avoidance maneuver to be performed by a rotorcraft in the presence of oncoming air traffic. The method features the steps of: (a) acquiring information about a threat aircraft...
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