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JP2020062919A |
To provide an air vehicle which achieves weight reduction compared to a conventional air vehicle while having performance higher or equivalent to the conventional air vehicle.An air vehicle 30 includes: an air vehicle body 31; one or mor...
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JP2020026180A |
To provide a flight body including a developing device of a parachute or a paraglider which has a simple structure, can easily and quickly develop a parachute umbrella part or canopy.A paraglider 10 includes a canopy 40, the canopy 40 in...
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JP2020026202A |
To provide a flight body including a development device of a paraglider which can adjust drawing condition of a break cord according to a range to be steered.A development device 80 of a paraglider mounted on a flight body includes an ac...
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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...
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JP2020011723A |
To provide a technique for optimizing an aerial vehicle for power generation flight.A method for transitioning an aerial vehicle may include the step of operating an aerial vehicle 130 in a hover-flight orientation. The aerial vehicle ma...
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JP2019534418A |
The present invention is an aerial floating device (10) comprising at least three wings (12) and one connecting device (18), the wings being linked and connected by a first cable (14, 16). Each wing is further connected to the coupling d...
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JP6609290B2 |
Methods and systems described herein relate to power generation control for an aerial vehicle. An example method may include operating an aerial vehicle in a crosswind-flight orientation substantially along a first flight path to generat...
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JP2019196159A |
To provide an airship or an ultra-lightweight power machine using helium or ammonia, and using hydrogen in such a form that explosive combustion hardly occurs.Main mixture gas is used, which is mixture gas comprising low-density flame-re...
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JP6604379B2 |
An electric energy transmission tether for an airborne wind power station comprises an elastic core, a first layer of one or more electric conductors helically wound around the elastic core, an electric insulation layer surrounding the f...
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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...
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JP6582072B2 |
A method may involve operating an aerial vehicle in a hover-flight orientation. The aerial vehicle may be connected to a tether that defines a tether sphere having a radius based on a length of the tether, and the tether may be connected...
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JP2019127155A |
To provide a mobile device capable of flying for a long time by effectively utilizing the power of a battery, a movement method and a program.A mobile device 1 for acquiring external information includes: a propeller or the like for acqu...
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JP6513870B1 |
[Task] Providing the main body structure of a foil type sport kite that can be assembled at low cost and with simple work and procedures It is a structure of the main body 100 of a foil type sports kite composed of a plurality of cells C...
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JP2019048630A |
To provide a method and a system for making transition of an aerial vehicle between certain flight modes that facilitate conversion of kinetic energy to electrical energy.A method can include making an aerial vehicle travel along a first...
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JP2019505425A |
The energy kite can be coupled to the tether and ground station via electromechanical thread. Energy kites can generate quite a lot of lift during power generation, and this load may need to be transferred to a tether anchored to the gro...
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JP2019026236A |
To provide a flight body comprising both of a rotary wing and a stationary wing, which can relax difficulty of posture control and steering when an operation state of a flight body is shifted between horizontal flight and vertical take-o...
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JP2018203188A |
To provide a crash detection device which can detect a state that a flight vehicle is about crash more promptly than a conventional crash detection device, and to provide a flight vehicle including the crash detection device.An unmanned ...
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JP2018204480A |
To provide a wind power generator capable of making power generation efficient, increasing a power generation amount and performing uncontrolled and stable attitude control to reduce a manufacturing cost or secure long-term reliability, ...
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JP6441776B2 |
To provide a drone kite which can fly for a longer time than a usual drone.Plural motors 2 are provided at an upper part of a kite main body, and a propeller 3 is attached to the motor. A photographic camera 4 is attached to a lower part...
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JP2018184166A |
To combine advantages of a kite and a drone.A kite body part is represented by 1. A plurality of motors 2 are provided on the top part of the kite body part 1, and propellers 3 are attached to the motors. A photographing camera 4 is atta...
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JP6423943B2 |
A method may involve operating an aerial vehicle (130) to travel along a first closed path (450A) while oriented in a crosswind-flight orientation. A tether (120) may be connected to the aerial vehicle (130) on a first end and may be con...
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JP6297259B2 |
The present disclosure relates to an unmanned aerial vehicle (UAV) able to harvest energy from updrafts and a method of operating an unmanned aerial vehicle. An unmanned aerial vehicle with a gliding capability comprising: a generator (1...
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JP6293904B2 |
A method involves operating an aerial vehicle in a hover-flight orientation. The aerial vehicle is connected to a tether that defines a tether sphere having a radius based on a length of the tether, and the tether is connected to a groun...
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JP6293939B2 |
A method may involve operating an aerial vehicle in a hover-flight orientation. The aerial vehicle may be connected to a tether that defines a tether sphere having a radius based on a length of the tether, and the tether may be connected...
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JP6243532B2 |
A method may involve operating an aerial vehicle (130) to travel along a first closed path (450A) while oriented in a crosswind-flight orientation. A tether (120) may be connected to the aerial vehicle (130) on a first end and may be con...
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JP6215491B2 |
Systems and methods are provided for a wiring harness for an aerial vehicle. A wing of the aerial vehicle comprises a pocket for insertion of the wiring harness. The wiring harness provides wiring and associated connections capable to at...
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JP6215849B2 |
The inventions provides for a system for electric power production from wind (50) comprising a glider (10), said glider (10) having an airfoil (14), on-board steering means (20, 22, 24) for pitching, rolling and yawing the glider (10) wh...
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JP6198017B2 |
A power generation apparatus and method comprises at least one gyroglider rotary wing flying at an altitude above the nap of the earth. A strong and flexible tether, connected to the gyroglider frame is pulled with a force generated by t...
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JP6200020B2 |
A kite system with a ground station adapted for airborne power generation. The kite system may include a kite which includes one or more airfoils which have mounted thereon a plurality of turbine driven generators. The turbine driven gen...
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JP6185180B2 |
Methods and systems described herein relate to power generation control for an aerial vehicle. An example method may include operating an aerial vehicle in a crosswind-flight orientation substantially along a first flight path to generat...
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JP6177674B2 |
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JP6152123B2 |
A flight control system for at least one tethered gyroglider along a flight path consistent with at least one flight mission is configured to fly the gyroglider within a portfolio of winds, managing an interaction between portfolios of a...
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JP6108300B2 |
Composite comprises identical or different polyurethane films that are linked with one another, a reinforcing grid disposed between the films, and a reinforcing textile thread oriented according to a predetermined line. An independent cl...
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JP6105080B2 |
A wind system (1) for converting energy is described, comprising: at least one kite (2) adapted to be driven from ground immersed in a wind current (W); at least one module (5) adapted to translate on a rail (6; 7) placed next to ground,...
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JP6100397B2 |
The invention relates to a method for control of a flying wing. The flying wing is arranged to be controlled to move along a predetermined trajectory by means of a fluid stream passing a wing of the flying wing. The flying wing comprises...
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JP6093099B2 |
A method may involve operating an aerial vehicle in a hover-flight orientation. The aerial vehicle may be connected to a tether that defines a tether sphere having a radius based on a length of the tether, and the tether may be connected...
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JP3207743U |
[Subject] A paraglider provided with a thrust unit which can control that a lift occurs even if it sets to begin to fly and there is no run-up, and an unnecessary moment occurs to a canopy by impelling force is provided. [Means for Solut...
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JP2016148608A |
To provide an electronic apparatus capable of notifying a user of the direction of a ground movement with respect to a front direction of the user.The electronic apparatus includes: a front azimuth detection section that detects a front ...
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JP3205609U |
To provide an aerial levitation device capable of stably levitation in the air without power. An aerial levitation device 1 is a paraglider type having a device main body 2 having a hang glider wing structure and a paraglider wing struct...
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JP2016521824A |
Wings that act in two modes are described. It changes from an arc to a flat shape without distortion, and vice versa. Consists of 3 or more power wing wings (1-1,1-2,1-3), connected in series and at least a pair of adjacent power wing wi...
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JP5950347B2 |
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JP5908989B2 |
A kite system with a ground station adapted for airborne power generation. The kite system may include a kite which includes one or more airfoils which have mounted thereon a plurality of turbine driven generators. The turbine driven gen...
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JP5841124B2 |
An actuating system for controlling the flight of a power wing profile or kite controlled via at least two cables for conversion of wind energy into electrical or mechanical energy, includes a first unit for exerting an action of unwindi...
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JP5816744B2 |
Flying electric generator aircraft that include groupings of four rotors mounted to booms extending fore and aft of a fuselage structure wherein the rotors are placed so that when the aircraft is facing the wind, each rotor has a direct ...
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JP5811384B1 |
To provide an aerial levitation device capable of long-time fixed point observation at low cost while reducing energy consumption. An aerial levitation device 1 includes an airframe body 2, an aircraft wing-shaped structure 3, an angle c...
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JP2015530954A |
The present invention provides a glider (10) for producing electricity from the wind (50). The glider is the first with respect to the wings (14), the on-board maneuvering means (20,22,24) for pitching, rolling, and yawing the glider (10...
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JP2015037898A |
To provide a laminar airfoil paraglider where a canopy on a ground is easily spread overhead and gliding speed is fast.An airfoil is made of cloth impervious to wind by sewing the cloth. A part within 15% of a front end of the airfoil is...
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JP5660706B2 |
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JP2014196046A |
To provide a technology for performing stable airborne flight near ground or a sea surface.A flight vehicle comprising a wing and the like 5 is restrained in such a manner as to mainly allow the degree of freedom of rotation of vertical ...
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JP5503521B2 |
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