| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 21 | MULTI-ROTOR AERIAL VEHICLE | EP15854629 | 2015-10-28 | EP3212502A4 | 2018-04-04 | LJUNG ANDERS |
| 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 power unit 2, at least a first, second and third hydraulic pump 12, 22, 32 dedicated to the respective first, second and third hydraulic motor 11, 21, 31, wherein each hydraulic pump 12, 22, 32 is arranged to provide pressurized fluid to each hydraulic motor 11, 21, 31 for powering the hydraulic motor 11, 21, 31 and thereby rotating the respective rotor 10, 20, 30, a control unit 6 for controlling the operation of the multi-rotor aerial vehicle (1, 1′, 1″, 1′″, 1″″, 1″″′, 1″″″), wherein the control of the multi-rotor aerial vehicle (1, 1′, 1″, 1′″, 1″″, 1″″′, 1″″″) is arranged to be performed by altering the flow of pressurized fluid distributed to each respective hydraulic motor 11, 21, 31, wherein, wherein the flow of pressurized fluid provided to each hydraulic motor 11, 21, 31 is individually controllable by means of at least one control valve 13, 23, 33 configured to control the flow of pressurized fluid from each hydraulic pump 12, 22, 32 to its dedicated hydraulic motor 11, 21, 31. | ||||||
| 22 | UNMANNED AERIAL VEHICLE BATTERY AND UNMANNED AERIAL VEHICLE | EP16863190.1 | 2016-10-25 | EP3244468A1 | 2017-11-15 | QIU, Longxue; WU, Xingwen |
The present invention discloses an unmanned aerial vehicle and a battery thereof. The battery includes a battery body and a shell disposed on one end of the battery body. The shell has a clamp button disposed on the side opposite the unmanned aerial vehicle. One end of the clamp button is fixed on the shell and the other is used for detachably connecting with the unmanned aerial vehicle. The clamp button makes the battery detachably connect with the main body of the unmanned aerial vehicle be possible and it is very convenient for changing the battery. |
||||||
| 23 | Autonomous solar aircraft | EP13166020.1 | 2013-04-30 | EP2660151B1 | 2016-04-27 | Frolov, Sergey V.; Cyrus, Michael; Bruce, Allan J. |
| 24 | Short takeoff and landing aircraft | EP14187036.0 | 2014-09-30 | EP2889221A1 | 2015-07-01 | Ouellette, Rich P. |
A short takeoff and landing fixed wing aircraft (200) includes a primary powertrain (302) to provide power to a propulsion unit (208), a secondary powertrain (304) to provide power to the propulsion unit (208), and a detachable power coupling to transfer power to the secondary powertrain (304) from a source external to the fixed wing aircraft during takeoff.
|
||||||
| 25 | Autonomous solar aircraft | EP13166020.1 | 2013-04-30 | EP2660151A1 | 2013-11-06 | Frolov, Sergey V.; Cyrus, Michael; Bruce, Allan J. |
An unmanned solar-powered aircraft (300) comprises a lightweight solar wing (310) comprising an airfoil profile, a top surface, a bottom surface, a leading edge, a trailing edge, wing tips, and at least one photovoltaic cell, wherein the surfaces and edges follow an arched bow shape across a span of the wing. The unmanned solar-powered aircraft includes a fuselage (330) and a propeller (340), wherein the fuselage is placed below the solar wing and contains an electric motor, battery, and electronics.
|
||||||
| 26 | 멀티로터 타입의 회전익 무인비행체 시스템 | KR20160162885 | 2016-12-01 | KR20180001415A | 2018-01-04 | |
| 본발명은멀티로터타입의회전익무인비행체시스템에관한것으로, 제1 무인비행체, 적어도하나이상의제2 무인비행체및, 상기제1 무인비행체와상기적어도하나이상의제2 무인비행체를서로분리가능하게연결시키는브릿지를포함하며, 상기적어도하나이상의제2 무인비행체는구동되지않은상태에서상기브릿지에의해상기제1 무인비행체에결합된상태로상기제1 무인비행체에의해이동가능하고, 상기적어도하나이상의제2 무인비행체는비행중인상기제1 무인비행체로부터분리가능하다. | ||||||
| 27 | 소형 공중 무인로봇을 위한 지상전원 공급시스템 | KR1020110052791 | 2011-06-01 | KR1020120133885A | 2012-12-11 | 김진태 |
| PURPOSE: A ground power supply system for a small aerial unmanned robot is provided to supply power for the operation of a camera operation, a communication relay station operation, and a lighting device by hovering a small aerial unmanned robot for a long time. CONSTITUTION: A ground power supply system for a small aerial unmanned robot comprises a ground power supply device. The ground power supply device comprises a cable(9), a winder(11), a fixing device(10), a fixing support(12), a plug(13), and a power connection wire(14). The thickness of the cable depends on the size or use of a body of a small aerial unmanned robot. The cable is formed by a flexible material. The winder winds and unwinds the cable. The fixing device fixes the cable on the winder. The fixing support fixes and tows the small aerial unmanned robot. The plug receives AC or DC power from the outside. The power connection wire supplies the AC or DC power to a cable terminal of the winder to supply the power to the small aerial unmanned robot through the cable. | ||||||
| 28 | MANNED AND UNMANNED AIRCRAFT | US16192330 | 2018-11-15 | US20190193847A1 | 2019-06-27 | James KAISER; William Vatis |
| A manned or unmanned aircraft has a main body with a circular shape and a circular outer periphery. One or more rotor blades extend substantially horizontally outward from the main body at or about the circular outer periphery. In addition, one or more counter-rotation blades extend substantially horizontally outward from said main body at or about the circular outer periphery, but vertically offset from the main rotor blades. | ||||||
| 29 | Battery used for unmanned aerial vehicle and an unmanned aerial vehicle | US15812860 | 2017-11-14 | US10115944B2 | 2018-10-30 | Longxue Qiu; Xingwen Wu |
| The present invention discloses an unmanned aerial vehicle and a battery thereof. The battery includes a battery body and a shell disposed on one end of the battery body. The shell has a clamp button disposed on the side opposite the unmanned aerial vehicle. One end of the clamp button is fixed on the shell and the other is used for detachably connecting with the unmanned aerial vehicle. The clamp button makes the battery detachably connect with the main body of the unmanned aerial vehicle be possible and it is very convenient for changing the battery. | ||||||
| 30 | OVERHEAD TETHERED DRONE SYSTEM | US15956340 | 2018-04-18 | US20180297699A1 | 2018-10-18 | Luis M. Ortiz; Kermit D. Lopez |
| An overhead tethered drone system can include a least one camera-bearing drone tethered by a retractable electrical power carrying tether line to a retraction assembly attached to venue infrastructure located above a live activity occurring within the venue. Controlling x-y-z orientation of the camera bearing drone can be accomplished via power to drone propellers and/or a tether line retraction motor located in the retraction assembly attached above the drone to venue infrastructure (e.g., ceiling rafters). Control over drone movement can be conducted remotely from a remote controller (e.g., control booth) while capturing high definition images of perspective within the venue by one or more drone cameras. Video images captured by the camera bearing drone can be provided to at least one of a production server or mobile devices via a wired and/or wireless data network where the images can be processed and rendered on display screens viewable by media directors, editors and spectators located either at the venue or remote from the venue (e.g., at home). | ||||||
| 31 | APPARATUS FOR CONTROLLING STILL POSITION IN AIR | US15756048 | 2016-08-30 | US20180251217A1 | 2018-09-06 | Kazuo ICHIHARA; Kiyokazu SUGAKI |
| An apparatus for controlling a still position in the air, allowing a miniature unmanned aerial vehicle equipped with a plurality of rotors to move swiftly to a given position in the air and make its airframe hover stably in that position, the apparatus including a miniature unmanned aerial vehicle equipped with a plurality of rotors, a stationary plane from which and on which the miniature unmanned aerial vehicle takes off and lands, and a plurality of string-like members which link the miniature unmanned aerial vehicle with the stationary plane, wherein the plurality of string-like members are stretched to a length for all the members to become tense when the miniature unmanned aerial vehicle has come to a specified position which is a given position in the air. Also, it is preferable that the plurality of string-like members include at least three string-like members. | ||||||
| 32 | Electricity generation in automated aerial vehicles | US15369527 | 2016-12-05 | US10065745B1 | 2018-09-04 | Brian C. Beckman; Amir Navot; Daniel Buchmueller; Gur Kimchi; Fabian Hensel; Scott A. Green; Brandon William Porter; Severan Sylvain Jean-Michel Rault |
| This disclosure describes a system and method for operating an automated aerial vehicle wherein the battery life may be extended by performing one or more electricity generation procedures on the way to a destination (e.g., a delivery location for an item). In various implementations, the electricity generation procedure may include utilizing an airflow to rotate one or more of the propellers of the automated aerial vehicle so that the associated propeller motors will generate electricity (e.g., which can be utilized to recharge the battery, power one or more sensors of the automated aerial vehicle, etc.). In various implementations, the airflow may consist of a wind, or may be created by the kinetic energy of the automated aerial vehicle as it moves through the air (e.g., as part of a normal flight path and/or as part of an aerial maneuver). | ||||||
| 33 | UNMANNED AIRCRAFT AND METHOD OF CONTROLLING THE SAME | US15753655 | 2015-11-17 | US20180244385A1 | 2018-08-30 | Jungsik KIM; Jaehark PARK; Woosok CHANG; Taegil CHO |
| Disclosed is an unmanned aircraft including: a housing; a drive unit that is formed in such a manner that the housing is moved; multiple UWB communication modules that are arranged a distance away from one another and that receives a wireless signal from an external device; a sensor unit that detects movement of the housing; and a control unit that calculates a distance between the external device and the housing, using pieces of movement information which are output by the multiple UWB communication modules and the sensor unit, and that controls the drive unit in such a manner that a specific distance between the external device and the housing is maintained. | ||||||
| 34 | MANNED AND UNMANNED AIRCRAFT | US15883781 | 2018-01-30 | US20180244378A1 | 2018-08-30 | James Kaiser |
| A manned or unmanned aircraft has a main body with a circular shape and a circular outer periphery. One or more rotor blades extend substantially horizontally outward from the main body at or about the circular outer periphery. In addition, one or more counter-rotation blades extend substantially horizontally outward from said main body at or about the circular outer periphery, but vertically offset from the main rotor blades. The rotor blades and counter-rotation blades can be folded upward into a storage position. In addition, the unmanned aircraft can have solar panels positioned about the top housing and fuselage of the aircraft. | ||||||
| 35 | System and method for enhancing distribution logistics and increasing surveillance ranges with unmanned aerial vehicles and a dock network | US14818329 | 2015-08-05 | US09984347B2 | 2018-05-29 | Frank Dreano, Jr. |
| A system and method for enhancing distribution logistics and surveillance ranges with unmanned aerial vehicles (UAV) and at least one dock in a dock network. The UAV remains in communication with the dock for enhancing distribution logistics of at least one package and increasing the range of surveillance for the unmanned aerial vehicle. From the dock, the UAV delivers the package to a destination point, obtains the package from a pick up point, recharges the unmanned aerial vehicle throughout the network of docks, and increases the range of distribution and surveillance. A logistics software controls the delivery and surveillance. A wireless communication device enables communication between the UAV and the dock. Light indicators indicate status of the package and the operational status of the UAV. A camera captures an image of the package in the dock. A motion detector detects the UAV for regulating access for loading/unloading and docking. | ||||||
| 36 | Aerial system and vehicle for continuous operation | US15291878 | 2016-10-12 | US09926084B2 | 2018-03-27 | James Peverill; Adam Woodworth; Benjamin Freudberg; Dan Cottrell; Terrence McKenna |
| An aerial vehicle landing station comprising a first post and a second post, wherein the second post is spaced apart from the first post and a cable to capture an aerial vehicle, wherein the cable is stretched between the first post and the second post and configured to support the weight of the aerial vehicle once captured and the cable may provide a charging current to the aerial vehicle once captured. One or more markers may be further positioned on the cable to designate a landing point, wherein the one or more markers are configured to be visually tracked by the aerial vehicle. A cable management device coupled to the cable via one or more pulleys may regulate tension of the cable. A communications transceiver at the aerial vehicle landing station may wirelessly communicate data with the aerial vehicle. | ||||||
| 37 | Methods of laser powering unmanned aerial vehicles with heat engines | US15009080 | 2016-01-28 | US09920706B1 | 2018-03-20 | Dmitriy Yavid; Stephen Jon Blank |
| Methods of laser powering unmanned aerial vehicles (UAV) with heat engines are disclosed. The laser powered heat engines are used in conjunction with devices for absorbing laser optical radiation, turning the laser optical radiation into heat, supplying the heat to a working fluid of the heat engine and harvesting mechanical work from expanding working fluid in the heat engine. | ||||||
| 38 | BATTERY USED FOR UNMANNED AERIAL VEHICLE AND AN UNMANNED AERIAL VEHICLE | US15812860 | 2017-11-14 | US20180069218A1 | 2018-03-08 | Longxue QIU; Xingwen WU |
| The present invention discloses an unmanned aerial vehicle and a battery thereof. The battery includes a battery body and a shell disposed on one end of the battery body. The shell has a clamp button disposed on the side opposite the unmanned aerial vehicle. One end of the clamp button is fixed on the shell and the other is used for detachably connecting with the unmanned aerial vehicle. The clamp button makes the battery detachably connect with the main body of the unmanned aerial vehicle be possible and it is very convenient for changing the battery. | ||||||
| 39 | BATTERY USED FOR UNMANNED AERIAL VEHICLE AND AN UNMANNED AERIAL VEHICLE | US15812773 | 2017-11-14 | US20180069216A1 | 2018-03-08 | Longxue QIU; Xingwen WU |
| The present invention discloses an unmanned aerial vehicle and a battery thereof. The battery includes a battery body and a shell disposed on one end of the battery body. The shell has a clamp button disposed on the side opposite the unmanned aerial vehicle. One end of the clamp button is fixed on the shell and the other is used for detachably connecting with the unmanned aerial vehicle. The clamp button makes the battery detachably connect with the main body of the unmanned aerial vehicle be possible and it is very convenient for changing the battery. | ||||||
| 40 | Manned and unmanned aircraft | US15600296 | 2017-05-19 | US09896196B1 | 2018-02-20 | James Kaiser |
| A manned or unmanned aircraft has a main body with a circular shape and a circular outer periphery. One or more rotor blades extend substantially horizontally outward from the main body at or about the circular outer periphery. In addition, one or more counter-rotation blades extend substantially horizontally outward from said main body at or about the circular outer periphery, but vertically offset from the main rotor blades. The rotor blades and counter-rotation blades can be folded upward into a storage position. In addition, the unmanned aircraft can have solar panels positioned about the top housing and fuselage of the aircraft. | ||||||
QQ群二维码
意见反馈
意见反馈