| Document |
Document Title |
|
JP6714911B2 |
To provide a tilt wing configuration unmanned aircraft suitable for transporting a baggage when using a capacitor as a drive power source.The tilt wing configuration unmanned aircraft is configured so that a baggage compartment 36 is pos...
|
|
JP2020097345A |
To solve a problem with a conventional manned drone that a conventional manned drone is structured so that a person accommodating part is moved vertically with a wire rope connected to a drone body, or, in an emergency, the person accomm...
|
|
JP6714499B2 |
To provide an electric hydraulic system capable of downsizing an electric hydraulic supply source even with constitution necessary for large hydraulic force, such as a leg lifting/lowering system.An electric hydraulic system 10 is consti...
|
|
JP6707227B2 |
To provide an adsorption device or an adsorption head capable of adsorbing various objects.A body 20 has a base 21 and adsorption means 22 exhibiting adsorption power between an object 1 and the means, and has a recess 24 forming a close...
|
|
JP6706677B2 |
A steering control apparatus for an aircraft is provided that can improve the travelling stability of an aircraft. An actual steering angle determining section (13) inside a steering control apparatus (1) determines an actual steering an...
|
|
JP6705669B2 |
To provide an unmanned lifesaving aircraft hardly impacted by the wind and capable of flying at high speed.An unmanned lifesaving aircraft comprises a body part including an ellipse ring (4), a surface of which is covered with a covering...
|
|
JP6696825B2 |
To provide a flight device which accurately maintains a distance between itself and an object and enables easy resting at a specific position.A flight device 10 includes casings 13, each of which covers an outer periphery side of a thrus...
|
|
JP2020512953A |
The uplock device (101) for use with aircraft parts includes hooks (102) that engage with capture pins (126) attached to the aircraft parts. The hook (102) is attached so that it can move between the closed position and the open position...
|
|
JP6683444B2 |
A computer system 20 provided in an aircraft 1 includes, as a module of a computer program to be executed, an approach determination section 31 configured to determine whether the aircraft 1 is approaching a landing site. The approach de...
|
|
JP6682372B2 |
To provide a landing gear of an aircraft, which can reduce the size of a lock mechanism even in a structure in which both ends of the lock mechanism are connected to a brace.In a landing gear 100 of an aircraft, a lock mechanism mounting...
|
|
JP2020055525A |
To provide a drive system for rotating a plurality of wheels of an aircraft landing device for ground taxiing and or spin-up before landing.A drive system comprises a motor operable for rotating a drive pinion, and a driven gear adapted ...
|
|
JP6677492B2 |
A multi-position landing gear for an aircraft may include a first landing skid (102) disposed on a bottom side of the aircraft (200), and a second landing skid (104) disposed on one of a top side or the bottom side of the aircraft (200),...
|
|
JP6676846B1 |
[Task]It enables the painting work of the structure surface using an unmanned aerial vehicle to be performed with stable quality.An unmanned aircraft equipped with a rotor, a coating device, and wheels that can roll in all directions, th...
|
|
JP6671525B2 |
An automated and versatile autonomously climbing undercarriage with flight capability that automatically reaches a suitable area for cleaning purposes, repair purposes, and monitoring purposes without being constantly connected to a supp...
|
|
JP6667566B2 |
To provide a wall surface inspection device for accurately inspecting a wall surface and holding an interval between a drone and wall surface by a simple structure.A wall surface inspection device comprises: a drone 2 whose flight is rem...
|
|
JP6663638B2 |
The present disclosure provides a system, method, and apparatus for distributing energy amongst at least one forward brake and at least one aft brake for a vehicle. The method involves determining, with at least one processor, an energy ...
|
|
JP6664209B2 |
To provide a flight type inspection machine allowing safe and reliable inspection over a long period of time by avoiding secondary disasters.The flight type inspection machine, which is loaded with an inspection device for inspecting sur...
|
|
JP2020037403A |
To provide a gear for a drive system for rotating one or more wheels of an aircraft landing gear.A roller gear 600 arranged to form a circular array in an aircraft landing gear drive system further comprises primary roller mounting pin r...
|
|
JP2020026210A |
To provide a leg lifting system that can keep on controlling even if a problem occurs in an electric power source, without being increased in size and weight.The leg lifting system comprises an actuator 10 that lifts up and down a leg 5 ...
|
|
JP2020026209A |
To provide a leg lifting system that suppresses generation of regenerative electric power without being increased in size and weight.The leg lifting system comprises an actuator 10 that lifts up and down a leg 5 of an aircraft 1, a contr...
|
|
JP6649024B2 |
A hydraulic cylinder includes: a cylinder tube; a piston; a piston rod; a pair of end covers; and a snubbing mechanism configured to reduce the moving speed of the piston after the piston reaches the vicinity of the end of its stroke. Th...
|
|
JP6648971B2 |
To efficiently and safely perform structure inspection work.An inspection device 10 for a structure inspects a presence or absence of a failure on a surface 62 of the structure. A radio-controlled rotorcraft 20 is equipped with a camera ...
|
|
JP6644818B2 |
A levered landing gear (110) including a first shock strut (200) having a longitudinal axis (LAX), a second shock strut (300) disposed concentrically with the first shock strut (200) along the longitudinal axis (LAX) such that the first ...
|
|
JP6642961B2 |
An elastic device for coupling between an aircraft landing gear wheel and a coaxial motorization member for motorization of the wheel. The elastic device comprises a plurality of arms to be rotationally coupled to the motorization member...
|
|
JP6644247B1 |
To provide an air vehicle in which a flight unit and a main body can be attached and detached and can be operated by each. A flying object according to the present invention has a flying portion and a main body portion. The main body is ...
|
|
JP2020019463A |
To provide a deployment device for parachute or paraglider which is less likely to twist a connection member, and a flying object comprising this deployment device.Another end of a connection member 86b is provided with a riser line 34 w...
|
|
JP2020016337A |
To provide a flexible interface between a wheel of an aircraft landing gear and a drive system for rotating the wheel for grand taxing.A drive system for an aircraft landing gear, comprises: drive shaft 120; a driven gear configured to m...
|
|
JP6630072B2 |
Many types of tailless airplanes which are triangular in planar view have been disclosed, but all of these are exclusively suited to high-speed flight; in contrast, the purpose of the present invention is to provide a tailless airplane w...
|
|
JP6631977B2 |
[Object] To provide a noise reduction apparatus, an aircraft, and a noise reduction method capable of increasing the amount of noise reduction.[Solving Means] The noise reduction apparatus 1 includes a porous plate 2 disposed to face a f...
|
|
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...
|
|
JP6628296B1 |
To avoid a collision with a floor surface or an operator when an unmanned aerial vehicle falls. An unmanned aerial vehicle 1 is provided with a fall prevention portion for preventing a fall, and the fall prevention portion is provided on...
|
|
JP6628297B1 |
To avoid a collision with a floor surface or an operator when an unmanned aerial vehicle falls. An unmanned aerial vehicle 1 is provided with a fall prevention portion for preventing a fall, and the fall prevention portion is provided at...
|
|
JP6625844B2 |
The invention provides a drive system for rotating a wheel of an aircraft landing gear. The drive system includes a motor operable to rotate a drive pinion, and a driven gear adapted to be mounted to the wheel. The drive system has a fir...
|
|
JP6626328B2 |
An electric taxiing system of an aircraft (1) includes: a wheel (5a, 7a) of an aircraft (1); a taxiing motor (5b, 7b) which is rotated together with the wheel (5a, 7a) in landing of the aircraft (1) to apply breaking force to the wheel (...
|
|
JP6624529B2 |
To provide a flying object and an automatic charging device for solving a problem in which conventional flying objects with a propulsion system are susceptible to damage at the time of landing or crash, fracture in a collision with an ob...
|
|
JP2019199254A |
To provide drive systems for rotating one or more wheels of an aircraft landing gear for the purposes of ground taxiing and/or spin-up prior to landing.The drive system includes a motor operable to rotate a first drive pinion via a first...
|
|
JP6608385B2 |
A roller gear for use in a roller gear and sprocket configuration of a drive system is disclosed, particularly for use in a landing gear drive system of an aircraft. Alternative embodiments and, in particular, means for permitting remova...
|
|
JP6606639B2 |
|
|
JP6597040B2 |
A flying machine frame structural body (30) including: a frame (32) that surrounds a flying machine body (20) including a rotating blade (22), and to which the flying machine body (20) is fixed; and plural wheels (34) that are rotatably ...
|
|
JP6592680B1 |
To provide an unmanned aerial vehicle capable of performing painting work on a structure surface with stable quality. A rotor which is a horizontal rotary blade, wheels arranged so as to protrude horizontally or upward from the machine b...
|
|
JP6590353B2 |
[Problem] To provide a technology for reliably landing a flying body on a ground surface that is covered with a granular medium. [Solution] The present invention is a leg part structural body which can support a body part of a flying bod...
|
|
JP6590173B2 |
A vertical take-off and landing aircraft 1 according to an embodiment of the present disclosure includes: a pair of ducted fans 2; a fuselage 3 that is disposed at a lower position than the ducted fans 2; a frame body 4 that connects the...
|
|
JP2019172259A |
To provide a small-sized multi-copter that is based on the assumption of usage in a survey field.A multi-copter can perform a "one-hand landing mode" of lowering an arm immediately beneath, as a landing mode. If a road surface is a prefe...
|
|
JP6589068B1 |
In water skiing, we provide flying water skiing equipment that enables floating and flying in the air in addition to gliding on water. A wing frame that is a flying water skiing device used to float and fly from the water to the air in w...
|
|
JP2019167096A |
To provide methods and systems for controlling the speed of an aircraft during an autonomous pushback maneuver, i.e., a maneuver under the aircraft's own power.A system includes a control system 200 that applies a torque to at least one ...
|
|
JP2019167087A |
To provide a braking system that contains brake heat and dust when an aircraft brakes, that reduces the frequent need for replacement parts of the braking system and a landing gear, that has the ability to direct taxi power to the landin...
|
|
JP6585051B2 |
A drive system for an aircraft landing gear, the drive system comprising: a pinion gear (110); a drive shaft (120) arranged to rotate the pinion gear about a drive axis; a driven gear arranged to mesh with the pinion gear to be rotatable...
|
|
JP6583311B2 |
To avoid a disaster caused by an unmanned missile generating an abnormality.An unmanned missile 100 includes a detection part for detecting that an abnormality is generated in the unmanned missile, an estimation part 118 for estimating a...
|
|
JP2019162931A |
To provide a new device capable of quickly replacing a fan even in an unmanned state.A fan device is an autonomous flight type fan device. An automatic replacement device 10 comprises an attachment/detachment control unit 12, a start con...
|
|
JP2019162980A |
To provide an unmanned flying body, an unmanned flying method and an unmanned flying program capable of maintaining a position and a posture, resisting an external force.An unmanned flying body 1 acquiring a thrust by the rotation of a p...
|
