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JP6952910B2 |
To enhance the containment capability of a ducted fan device at the time of FBO without hindering the weight reduction thereof, in a ducted fan device including a fan shroud (52) having an annular shape in plan view and an electric fan d...
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JP6955280B2 |
Apparatus, systems, and methods are contemplated for electric powered vertical takeoff and landing (eVTOL) aircraft. Such are craft are engineered to carry safely carry at least 500 pounds (approx. 227 kg) using a few (e.g., 2-4) rotors,...
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JP6950971B2 |
A vehicle, includes a main body. A fluid generator is coupled to the main body and produces a fluid stream.. At least one fore conduit and at least one tail conduit are fluidly coupled to the generator. First and second fore ejectors are...
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JP6951603B1 |
To provide a helicopter or the like as a conventional vertical takeoff and landing aircraft by blowing a strong air flow toward the lower part of the airframe to raise the airframe as an aerodynamic reaction. There were drawbacks such as...
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JP6949869B2 |
A tailsitter aircraft includes one or more rotatable wings. The tailsitter aircraft optionally includes a fuselage from which wing supports extend. Each rotatable wing optionally includes a rotatable wing section having an inboard portio...
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JP2021154883A |
To provide an aircraft that can take off and land vertically and can efficiently extend the flight distance with a simple configuration.A flight device 1 with wings 3 extending horizontally from an airframe 2 comprises a plurality of tub...
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JP2021154802A |
To suppress decline in lift of a main wing.A flying body includes: a main wing extending in a horizontal direction of an airframe; an arm extending in a longitudinal direction of the airframe; and a tail extending in a vertical direction...
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JP2021154884A |
To provide a flight device that can take off and land vertically and can efficiently extend the flight distance with a simple configuration.A flight device comprises tubes 4 and ducted fans 5. The tube 4 is formed in a cylindrical shape ...
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JP6942710B2 |
A hybrid propulsion aircraft is described having a distributed electric propulsion system. The distributed electric propulsion system includes a turbo shaft engine that drives one or more generators through a gearbox. The generator provi...
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JP6929914B2 |
The purpose of the present invention is to accurately land a vertical take-off and landing aircraft on a target landing point. This automatic landing system is provided with: an imaging device mounted on a vertical take-off and landing a...
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JP6920889B2 |
To simplify delivery work, and reduce a burden on a user at a delivery destination or a package collection destination.A storage device comprises: a storage unit which is disposed in a building or on a ground surface, forms an internal s...
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JP2021518310A |
The structure (100) for the aircraft (200) comprises a first fuselage (101), a second fuselage (102), and at least one wing (103). In addition, the structure (100) comprises a support structure (104) for supporting the wings (103) and th...
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JP6905221B2 |
To provide a guidance control device which allows automatic guidance flights to be performed that follow an input of speed commands, ascending and descending rate commands, and heading commands, and which further covers automatic guidanc...
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JP2021103391A |
To provide a watching device capable of watching overall daily life while taking into consideration privacy of a watching object.A watching robot comprises: a main camera; a heart rate sensor; a robot body in which these main camera and ...
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JP6889797B2 |
A modular flying car includes a ground vehicle (10) and a flight vehicle (20). The ground vehicle (10) includes a chassis (11), a first cabin (12) and a landing platform (13) for landing the flight vehicle (20). The flight vehicle (20) i...
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JP6879866B2 |
There is provided a vertical takeoff and landing aircraft (VTOL), having a main propulsion unit (GT engine) with high-pressure and low-pressure turbine shafts installed along a longitudinal axis of a frame to be rotated by pressurized ga...
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JP2021079815A |
To provide a more flexible method for using a take-off/landing base, which corresponds to a usage pattern.A take-off/landing base for an unmanned aircraft capable of vertically taking off and landing comprises an attachment/detachment pa...
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JP2021075191A |
To provide a vertical takeoff and landing aircraft which effectively utilizes lift force of fixed wings, and is reduced in weight while having high strength, and therefore increases transportation efficiency, and which properly secures s...
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JP3231509U |
To provide a flying saucer type aircraft capable of taking off and landing vertically without requiring a dedicated runway. This is a flying disk type aircraft equipped with a flying disk body 1, a flying paddle, and a landing gear, and ...
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JP2021049960A |
To provide a flight body capable of securing a stably safe attitude and flight control by enabling vertical assent under moving flight and strong wind, diagonal assent under vertical descent and strong wind, diagonal descent, or the like...
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JP3231301U |
To provide an unmanned aerial vehicle capable of stabilizing flight control at the time of transition between a vertical flight mode and a horizontal flight mode. A multicopter 103 includes horizontal rotor units 130A to 130D and fixed w...
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JP6825011B2 |
Systems, devices, and methods for an aircraft having a fuselage; a wing extending from both sides of the fuselage; a first pair of motors disposed at a first end of the wing; and a second pair of motors disposed at a second end of the wi...
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JP6818988B1 |
To sufficiently study how the airflow generated by a plurality of rotary wings affects each other under the rotary wing aircraft in the case of a conventional rotary wing aircraft, and the wind pressure generated by the rotary wing is ef...
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JP6821518B2 |
A support system (10A) is mounted on an aircraft capable of hovering. The support system (10A) includes: a detecting portion (12) provided outside an airframe (31) and configured to detect a target object that may become an obstacle; an ...
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JP6796736B2 |
A modular flying car includes a ground vehicle (10) and a flight vehicle (20). The ground vehicle (10) includes a chassis (11), a first cabin (12) and a landing platform (13) for landing the flight vehicle (20). The flight vehicle (20) i...
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JP2020175713A |
To provide a multi-rotor aircraft with a plurality of rotary wings in which flight with high energy efficiency can be performed with a simple mechanism during horizontal flight.A multi-rotor aircraft includes: a fuselage; wings which are...
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JP2020530913A |
A shroud for aircraft that is configured to at least partially surround a noise source, including a propeller. The shroud contains two or more sound absorbing materials located on the outer layer and inside the shroud. The outer layer is...
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JP6770068B2 |
A flying object according to the present invention has been developed to have a plurality of rotor blades or jet engines, and to reduce the risk of a crash even if any one of the rotor blades or jet engines is damaged. The flying object ...
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JP2020158104A |
To provide a flying vehicle capable of improving drive feelings and ride comfort for a passenger.A flying vehicle which a passenger can get on board and which moves by floating above the ground comprises: a fuselage which the passenger g...
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JP2020158098A |
To provide a flying vehicle capable of improving drive feelings and ride comfort for a person on board.A flying vehicle 1 which a passenger can get on board and which moves by floating above the ground comprises: a fuselage 2 which the p...
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JP6758697B2 |
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JP6751537B2 |
To provide a manned aircraft as new means of moving.A hybrid manned aircraft of the present invention comprises: an engine; a motor; a first rotary wing unit for generating an aerodynamic lift using the engine; a second rotary wing unit ...
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JP6749019B2 |
To provide a manned flight vehicle as new transportation means.A flight vehicle 1 having main frames 2, 2', and lift generation parts 3, 3' which are attached to the front and rear of the main frames respectively. The main frame comprise...
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JP6739779B1 |
To provide a personal flight device which is small and lightweight, easy to operate, allows a passenger to fly in the air in any direction, is economically excellent, and is easy to move, store and store. A main body portion 2, a spindle...
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JP2020108997A |
To provide a flight vehicle which is allowed to efficiently and safely transfer from hovering to horizontal flight.A flight vehicle 1 is equipped with lift generation parts 100 such as main wings, thrust generation parts 104 that enable ...
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JP6719107B2 |
An aircraft includes: a plurality of rotor units each including propeller and motor that drives propeller; a shock absorber covering an entire vertical length of a lateral side of the plurality of rotor units; and a plurality of rudders ...
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JP6720201B2 |
Multi-rotor aerial vehicle (1, 1′, 1″, 1′″, 1″″, 1″″′, 1″″″) comprising, at least a first, second and third rotor 10, 20, 30, each rotatable by a dedicated first second and third hydraulic motor 11, 21, 31, a powe...
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JP6711805B2 |
A VTOL aircraft comprising a magnetic orientation detent includes a motor (124a) coupled to a motor shaft (310), the motor (124a) mechanically coupled to a motor mount (320). The magnetic orientation detent may also include a flywheel (3...
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JP6711565B2 |
To provide a communication apparatus capable of starting operation in a desired operation mode without having a user perform complicated operation.A communication device 100 accepts prescribed operation from a user 202, accepts a control...
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JP6693650B2 |
To provide a flight vehicle body having one propulsion part or propulsion parts, an axle which is disposed so as to be perpendicular to a main travel direction, and a protection frame which encloses the flight vehicle body in a three-dim...
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JP2020509972A |
This subject relates to the aircraft (100). The aircraft (100) includes a main body (102), which is at least one to draw in ambient air, amplify the sucked air, and release the amplified air. It has a suction motor (104). The aircraft (1...
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JP6672279B2 |
A transportable ground station for a UAV includes a container in which the UAV may be transported and housed. The container includes a wireless or contact-based recharging station that recharges the UAV's batteries or other power sources...
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JP6671375B2 |
A flight aiding method for an unmanned aerial vehicle includes receiving a receiving, from a mobile terminal that controls the unmanned aerial vehicle, a flight aiding instruction to execute a flight aiding function. The flight aiding me...
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JP6657500B2 |
A system for operating a mobile platform using distance and speed information and methods for making and using same. The system includes a time-of-flight sensor and an ultrasound sensor for measuring a distance between the mobile platfor...
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JP6654306B1 |
To provide an amplified fluid flow generation mechanism capable of obtaining a large fluid flow without using a high output motor having a large power consumption or a large motor. A rotary wing mechanism for generating a fluid flow and ...
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JP2020015457A |
To provide a vertical take-off and landing system being extremely safe without depending on a conventionalflying method (that is, normal flying technique of blowing down the descending wind from an airframe itself).A conventional vertica...
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JP6636778B2 |
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JP6631367B2 |
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JP2020001671A |
To provide a flight body which flies by hydrogen energy without fossil fuel, which is a disk-shaped flight body flying on a flight locus and having a novel shape.A disk-shaped flight body comprises on a lower part of its body a plurality...
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JP6618564B2 |
To provide a flight body which can be flown by a simple operation even indoors.A flight body 10 includes: a cylindrical shape body part 100 having an outer peripheral part and an inner peripheral part; a lift force generation part which ...
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