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JP7180450B2 |
To provide a flight machine which can suppress that an airframe moves away from a wall surface while suppressing power consumption.A flight machine 10 comprises an airframe 11, a first wind direction anemometer 91, a second wind directio...
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JP7157967B2 |
To provide an unmanned helicopter capable of stably bringing a plurality of wheels into contact with an inspection object for accurately inspecting the inspection object.An unmanned helicopter 1 comprises: a mount part 20 of an inspectio...
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JP7155114B2 |
This unmanned aerial vehicle moves in midair and is capable of performing fluorescent X-ray analysis of a predetermined object of measurement, and is characterized by being provided with: an aerial vehicle main body; a fluorescent X-ray ...
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JP7153065B2 |
This anti-vibration device for an unmanned aircraft is configured by an anti-vibration rubber being interposed between the airframe body and legs of the unmanned aircraft which are connected to each other, the anti-vibration rubber being...
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JP2022151899A |
To provide an aircraft which changes a wing with a large wing width to a small wing width in view of convenience of road transportation or road travel in order to improve flight efficiency.An aircraft comprises a telescopic wing which ca...
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JP2022151416A |
To provide a frame for a multicopter that corresponds to not only a load, but also stress generated during flight, take-off and landing, and further, is high in degree-of-freedom of design of a component installation part, with a small n...
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JP2022145620A |
To provide a support structure to attach landing gear to a wing spar of an aircraft.The support structure includes a trunnion assembly having a first trunnion and a second trunnion that are connected together with the first trunnion posi...
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JP2022143988A |
To provide a landing device having a guide mechanism for landing a UAV at an accurate position, a survey system which enables measurement in a landed state, and a measuring method thereof.This landing device for a flying object 5 compris...
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JP2022136628A |
To provide a support leg device capable of simultaneously achieving magnetic attraction to an object and movement in the object without needing a separation mechanism.A support leg device 13 of an unmanned aircraft 10 comprises: a wheel ...
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JP2022127929A |
To provide an illumination system in which an unmanned flying object can be more easily and firmly fixed to a landing base and an illumination device used in the illumination system.An illumination system 1 comprises: an unmanned flying ...
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JP7123038B2 |
Provided are: a cable bead which can realize a weight reduction while maintaining the breaking pressure resistance; and an airplane tire including the same. A cable bead (10) includes: a core (1) composed of an annularly formed steel; an...
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JP7120808B2 |
A shrink mechanism (300) for use with a landing gear (200A) of an aircraft (100) is provided. The landing gear includes an outer sleeve (310) at least partially surrounding a shock strut (210), the shrink mechanism has a shaft (312) rota...
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JP7118976B2 |
An aerial vehicle safety apparatus (100) includes a safety mechanism (10), a drive mechanism, an ejection mechanism, and a control mechanism. The safety mechanism (10) is used for securing safety of at least one of an aerial vehicle (30)...
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JP7110086B2 |
To prolong a utilization time of a flight body by launching the flight body toward a working field.A traction device includes a traction truck which can be connected with a traveling vehicle, a power input part which is provided on the t...
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JP7110085B2 |
To easily spray spraying material even to a relatively large workplace.A flight vehicle includes an airframe, a wing part fixed to the airframe to generate lift force, and a float provided in at least one of the airframe and the wing par...
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JP7106082B1 |
To provide an aircraft landing gear elevating gear structure capable of lowering an landing gear by disconnecting a connection between a motor output and an electric linear actuator in an emergency with a simple configuration. A gear cou...
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JP2022107514A |
To provide a landing gear door system for a landing gear compartment which does not cause undesirable drag, turbulence and vibration which impose stress and wear upon egress doors.A landing gear door system for a landing gear compartment...
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JP7104061B2 |
An aerial vehicle safety apparatus (90) includes an expandable object (86) and an ejection apparatus (88). The ejection apparatus (88) includes a container (80) that accommodates the expandable object (86) and has an opening provided on ...
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JP7101054B2 |
To provide a vibration control structure of an unmanned aircraft which enables reduction of an impact input to an unmanned aircraft during landing of the unmanned aircraft to inhibit overturning and damage of the unmanned aircraft.A vibr...
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JP7098395B2 |
Systems and methods for indicating the health of brakes on an aircraft or a ground vehicle. One method for monitoring brake health calculates the ratio of input energy to output energy during braking. The input energy is a function of co...
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JP2022097298A |
To provide a flight vehicle taking-off and landing system, a taking-off and landing device for flight vehicle, and a flight vehicle, which can be used at even a place where a rail cannot be installed, and can smoothly perform taking-off ...
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JP2022095361A |
To provide an unmanned flying object movable in a stable posture and changeable in direction during moving with respect to an upper structure.An unmanned flying object 10 comprises; a main body part 12; lifting-power generating means 13 ...
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JP2022095291A |
To improve workability and safety, in work for inspecting a structure using the drone.A drone comprises; a plurality of horizontal rotors which are rotors having horizontal rotating wings; a mount part for holding an external instrument;...
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JP2022094950A |
To provide a tire monitoring device, a tire monitoring system, and a method.In one example, the tire monitoring device includes a wireless interface having range determining capability, and a processor. The processor is configured to: re...
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JP2022094905A |
To provide an aviation mobility landing gear control system and a control method.An aviation mobility landing gear control system in the present invention includes: a shaft of the landing gear control system, the shaft deployed when the ...
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JP7090431B2 |
An aircraft landing gear structure (18, 152) according to the present disclosure includes a retract actuator (32) and a shrink mechanism (22). The retract actuator (32) is configured to transition a strut assembly (100, 154) of the aircr...
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JP7090432B2 |
An aircraft landing gear structure (18, 70, 152) according to the present disclosure includes a strut assembly (71, 100, 154) and a wheel assembly (20) operatively coupled to the strut assembly. The strut assembly includes an upper tubul...
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JP7086144B2 |
To provide a movable body movable in air and on the water and to easily perform investigation and survey about a water area and a land around the water area.A movable body (an investigation and survey apparatus 10) enables aerial flight ...
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JP7085218B2 |
To provide a flight body that can bring a working portion closer to a work object at a proper distance.A feeding method for a flight body according to the present invention includes a work rotorcraft, a relay rotorcraft, and a feeding ma...
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JP2022085900A |
To provide a flying body or the like, which lowers a loaded object from the flying body after landing while maintaining an attitude of the loaded object and releases the loaded object in such a manner that an impact occurring to the same...
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JP7078475B2 |
To provide a flight work body capable of solving problems for example, when moving directly, on a curve ceiling plane such as inside of a duct, when the flight work body is deviated from a direct movement direction, since force directed ...
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JP7076639B2 |
A landing gear (100) comprises a leg (110A, 110B, 110C), a rotating body (130A, 130B, 130C), and a housing (150). The leg (110A, 110B, 110C) makes contact with the landing surface at one end and moves linearly in the axial direction with...
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JP7073479B2 |
Provided is an unmanned aerial vehicle including a waterproof container (50) including: a container main body (52) having an opening (56) in a bottom surface defined in a landed state of the unmanned surface aerial vehicle; a waterproof ...
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JP7072370B2 |
A semi-levered landing gear (200) including a shock strut (210) configured for coupling to an airframe (101) of an aircraft (100), a truck lever (220) being rotatably coupled to the shock strut, a tension link assembly (230) having a ten...
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JP2022525774A |
INDUSTRIAL APPLICABILITY The present invention controls the braking of the wheels of an aircraft by operating the wheel brake 10 by the wheel braking control device 14 of the aircraft based on both the deceleration adjustment request 16 ...
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JP2022075192A |
To solve such a problem that since a conventional unmanned machine has adopted a landing gear comprising a support mechanism with a stretchable structure and a buffer mechanism, it had a heavy weight, and there was not enough space at a ...
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JP7069368B1 |
To provide a flying object and an inspection method capable of easily accessing a high place. A flying object 100 having a propeller 20 in a main body 10 includes a traveling device 30 having a contact patch 31 to an inspection object B,...
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JP2022070702A |
To provide an unmanned aircraft of which airframe can be controlled to various positions, postures and movement states.An unmanned aircraft 1 includes: a body 10; multiple propeller units 20 for floating and moving vertically the body 10...
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JP2022066645A |
To provide a multiple rotor manned aircraft including a manned cabin, a lifting rotor, an equipment cabin, and a steering wheel.In the multiple rotor manned aircraft, a window 7 is arranged on an upper part of a manned cabin 1, a landing...
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JP7053305B2 |
A tail skid shock absorber (110) including an outer shock absorber canister (200), a crushable indicator cartridge (300) disposed within the outer shock absorber canister (200), and an indicator rod (310) coupled to the crushable indicat...
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JP7053300B2 |
A strut assembly (71, 100, 154) for an aircraft landing gear structure (18) according to the present disclosure is transitioned between an extended configuration, corresponding to the aircraft being off the ground, and a retracted config...
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JP7053774B2 |
To provide an underwater survey system and an underwater survey method capable of speedily and easily carrying out a survey underwater in a plurality of positions in various locations.An underwater survey system 1 includes: an unmanned f...
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JP7048131B1 |
To provide an unmanned aerial vehicle capable of suppressing an increase in power consumption due to a landing gear. An unmanned aircraft 100 includes an aircraft body 101, a plurality of rotors 104A and 104B facing upward, and left and ...
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JP2022520924A |
The present invention provides an unmanned aircraft recovery device, including recovery pulleys, pulley rails and dampers, of which the recovery pulleys are used for abutting and recovery of unmanned aircraft, and the pulley rails are us...
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JP7045034B2 |
To provide a method for coating a coating material by use of an unmanned aircraft which coats a coating material onto a structure with high accuracy.In a method for coating a coating material by use of an unmanned aircraft which coats a ...
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JP7044413B1 |
To provide a flight device having a wing portion capable of effectively obtaining lift during flight. A flight device 10 is provided with an airframe base 14, a first leg portion 26 and a second leg portion 27, and a first leg portion 26...
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JP7033937B2 |
To provide a measurement device, a robot, and a method for measurement that can stably and smoothly measure a plurality of parts continuously.The measurement device includes: a rotational body (21), which can rotate on an arbitrary objec...
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JP7032934B2 |
A landing gear assembly for use with an aircraft includes a housing including a trunnion brace, a drag brace, and an aft brace that together define an opening through the housing. The landing gear assembly also includes a shrink link ass...
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JP2022034865A |
To provide a helicopter that can reduce impact at landing by increasing probability of capable of descending while deploying a parachute in the event of emergency landing.A multicopter 1 with a parachute 61 includes a control unit 33 for...
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JP7029838B1 |
To provide an unmanned aerial vehicle in which a wing body can be deployed and the increase in the weight of the unmanned aerial vehicle is suppressed. The aircraft main body 101, a plurality of rotors 104A and 104B facing upward, and le...
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