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公开(公告)号：US5118052A
公开(公告)日：1992-06-02
申请号：US115333
申请日：1987-11-02
Applicant: Albert Alvarez Calderon F
Inventor： Albert Alvarez Calderon F
CPC classification number: B64C3/56 , B64C1/30 , B64C39/024 , B64C2201/102 , B64C2201/146 , B64C2201/165 , B64C2201/201 , Y02T50/145
Abstract: A Variable Geometry Remotely Piloted Vehicle (VG-RPV) has a main fuselage portion supporting at one end main wing panels and a forward fuselage portion. In the stowed position, the main wings and forward fuselage portion are laterally adjacent the main fuselage. This provides compact volume of small dimensions for stowage inside a canister. When deployed for flight, the wings are inclined at a large angle to the main fuselage, and a fuselage forebody is positioned upstream of the main fuselage, to establish a vehicle center of gravity adjacent to the deployed wings. Folding panels are mounted on chordwise hinges at the tip of the main wing panels. These panels overlap the main wing panels in the stowed configuration, inside the canister or on deck, and extend the span and area of the deployed main panels in the flight configuration. In-flight deployment is provided to launch the VG-RPV with a reduced span and area with the folding panels placed under the main panels. After launch, but prior to slow speed flight, aerodynamic in-flight deployment of the folding panels is aided with trailing tabs on the folding panels.
Abstract translation: 可变几何遥控牵引车（VG-RPV）具有主机架主体部分，主机翼部分和前机身部分支撑。 在收起位置上，主翼和前机身部分横向邻近主机身。 这提供了小尺寸的小尺寸用于在罐内的装载。 当部署为飞行时，机翼与主机身倾斜大角度，并且机身前体位于主机身的上游，以建立与展开机翼相邻的车辆重心。 折叠板安装在主翼板顶端的弦向铰链上。 这些面板与收起的结构中的主翼板重叠，在罐内或甲板上，并且在飞行配置中延伸部署的主面板的跨度和面积。 提供飞行部署以发射具有减小的跨度和面积的VG-RPV，折叠面板放置在主面板下方。 在发射后，但在慢速飞行之前，折叠板的空气动力学飞行中部署有助于折叠板上的拖尾。
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公开(公告)号：US20230202679A1
公开(公告)日：2023-06-29
申请号：US17562992
申请日：2021-12-27
Applicant: Industrial Technology Research Institute
Inventor： Ming-Hsuan HO , Hon-Yue CHOU , Yi-Yuan CHEN
CPC classification number: B64F1/005 , B64C39/024 , B64F1/04 , B64C2201/066 , B64C2201/201
Abstract: A container device of a UAV is provided. The container device is configured to receive a cargo and be connected to a UAV. The container device includes an outer housing, an inner housing, and a power supply. The outer housing is connected to the UAV. The inner housing is detachably connected to the outer housing, and configured to receive the cargo. The power supply is disposed in the inner housing. When the outer housing is connected to the UAV and the inner housing is connected to the outer housing, the power supply is electrically connected to a battery of the UAV. A transport system of a UAV is also provided.
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公开(公告)号：US20190241282A1
公开(公告)日：2019-08-08
申请号：US16329833
申请日：2017-08-29
Applicant: Armin Strobel
Inventor： Armin Strobel
CPC classification number: B64F1/222 , B64C39/024 , B64C39/062 , B64C2201/145 , B64C2201/18 , B64C2201/201 , B64D37/005 , B64F1/362
Abstract: A ducted fan unmanned aerial vehicle (UAV) docking station is provided. The docking station comprises: a guide sized to receive a ducted fan UAV; and a housing communicatively coupled to the guide. The housing comprises: a storage assembly comprising: at least one compartment sized to store the UAV; and at least one dampening system coupled to the at least one storage compartment for cushioning the UAV.
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公开(公告)号：US20180319496A1
公开(公告)日：2018-11-08
申请号：US16024446
申请日：2018-06-29
Applicant: Hangzhou Zero Zero Technology Co., Ltd
Inventor： Tong Zhang , Mengqui Wang , Zhaozhe Wang , Xuyang Zhang , Guanqun Zhang , Shuang Gong , Yalin Zhang , Jinglong Wang , Lixin Liu
CPC classification number: B64C39/024 , B64C1/30 , B64C27/08 , B64C2201/024 , B64C2201/027 , B64C2201/042 , B64C2201/088 , B64C2201/108 , B64C2201/162 , B64C2201/20 , B64C2201/201 , B64C2201/203 , B64C2211/00
Abstract: An aerial vehicle, preferably including: a rotary wing and a protection housing enclosing the rotary wing. An aerial vehicle, preferably including: a first rotary wing module including a first rotary wing and a second rotary wing module including a second rotary wing, wherein the first rotary wing module and the second rotary wing module are preferably operable between a folded configuration and an unfolded configuration. A method of aerial vehicle operation.
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公开(公告)号：US20180305011A1
公开(公告)日：2018-10-25
申请号：US15768201
申请日：2016-10-28
Applicant: BAE Systems plc
Inventor： David Julian Wright , Nicholas Giacomo Robert Colosimo , Clyde Warsop
CPC classification number: B64C39/024 , A63H27/00 , B64C29/00 , B64C29/0033 , B64C2201/021 , B64C2201/024 , B64C2201/088 , B64C2201/104 , B64C2201/108 , B64C2201/182 , B64C2201/201
Abstract: A rotary-wing air vehicle comprising a main body (12) and at least two rotor devices (16a, 16b) arranged and configured to generate propulsion and thrust, in use, to lift and propel said air vehicle, said rotor devices (16a, 16b) being arranged and configured relative to said main body (12) such that the blades thereof do not cross through a central vertical axis of said main body (12) defining the centre of mass thereof, wherein said main body (12) is provided with an aperture (100) that extends therethrough to define a channel about said central vertical axis.
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Patent Agency Ranking
56.发明申请公开(公告)号：US20180281939A1
公开(公告)日：2018-10-04
申请号：US15941133
申请日：2018-03-30
Applicant: The Government of the United States of America, as represented by the Secretary of the Navy
Inventor： Steven K. Tayman
CPC classification number: B64C27/50 , B64C27/10 , B64C39/024 , B64C2201/024 , B64C2201/042 , B64C2201/08 , B64C2201/108 , B64C2201/126 , B64C2201/18 , B64C2201/201
Abstract: An expendable rotary wing unmanned aircraft capable of storage in a cylindrical housing includes a longitudinally extending body having an upper end and a lower end; and a pair of counter-rotating coaxial rotors each located at respective ends of longitudinally-extending body, wherein each rotor includes two or more blades, each blade rotatably coupled to a remainder of the rotor at a hinged joint and thereby extending along a length of the body in a storage configuration and extending radially outward from the body in a flight configuration.
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公开(公告)号：US20180134412A1
公开(公告)日：2018-05-17
申请号：US15566603
申请日：2016-04-29
Applicant: Chung Kiak POH , Chung How POH
Inventor： Chung Kiak POH , Chung How POH
CPC classification number: B64F1/04 , B64C39/024 , B64C2201/021 , B64C2201/084 , B64C2201/182 , B64C2201/201 , B64F1/02 , B64F1/222 , H02S20/30
Abstract: The present invention generally relates to a system and method of a docking system (1) for fixed wing unmanned aerial vehicle, or non-fixed wing unmanned aerial vehicle (2) such as rotorcraft, or combination thereof, comprising at least a docking and/or launching pad capable of being arranged in an array or staggered manner; said pad has a surface (6) for said vehicle docking and launching, said docking and launching surface (6) comprising moveable pads (31) which include electromagnets that can be energized to capture a docking vehicle (2); and another energy harvesting surface (4) has photovoltaic panel to harness solar energy to generate electricity or hydrogen fuel for a variety of on-board applications such as to charge said vehicle (2) and to power the docking system and providing a safe stowage and protected storage for the said vehicle (2).
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公开(公告)号：US20180095460A1
公开(公告)日：2018-04-05
申请号：US15832648
申请日：2017-12-05
Applicant: NIGHTINGALE INTELLIGENT SYSTEMS
Inventor： Ian CHEN , Hugo Boyer , John Ming-Jey Hsu , Frank Berthold Alfons Gaugel , Davor Bauk , Arnd Schöter , Cyril Damm , Jack Wu
CPC classification number: G05D1/0038 , B64C39/024 , B64C2201/127 , B64C2201/146 , B64C2201/182 , B64C2201/201 , G05D1/0044 , G06K9/00637 , G06K9/00664 , G06K9/00771 , G07C5/008 , G08C17/02 , G08G5/0013 , G08G5/0026 , G08G5/0052 , G08G5/006 , G08G5/0069 , G08G5/0078 , G08G5/0086 , G08G5/045 , H04L65/4092 , H04L67/12 , H04L67/125
Abstract: An automated drone security system for surveilling a location includes one or more drones with onboard sensors and an imaging device for measuring surveillance data. The surveillance data may include images, telemetry data, infrared data, or other detectable information of the location. Drones may be capable of executing one or multiple flight operations as well as storing and transmitting the surveillance data to a server assembly operable for coordinating the drone and receiving the surveillance data. A drone dock may be included for drone launching, landing, and/or storing the drones. A user computing device may be in communication with the server assembly and the drone(s), the user computing device being capable of receiving user input and displaying surveillance data from the drone. Flight operations associated with surveilling the location may be automatically and/or manually controlled by the user computing device and/or or the server assembly in connection with the location.
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公开(公告)号：US09845020B2
公开(公告)日：2017-12-19
申请号：US15392838
申请日：2016-12-28
Applicant: SWIFT ENGINEERING, INC.
Inventor： Andrew Streett
CPC classification number: B60L11/182 , B64C39/024 , B64C2201/141 , B64C2201/146 , B64C2201/201 , B64C2201/205 , B64F1/222 , G05D1/0011 , G05D1/0088 , H02J7/35
Abstract: 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 after the UAV returns from a mission. The recharging station may be directly or indirectly connected to one or more solar panels that generate energy to power the recharging station. The ground station may be deployed virtually anywhere, from any vehicle (e.g., plane, train, boat, truck, etc.), and may operate over an extended period of time without human intervention.
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60.发明申请公开(公告)号：US20170327214A1
公开(公告)日：2017-11-16
申请号：US15433697
申请日：2017-02-15
Applicant: Hood Technology Corporation
Inventor： Andreas H. von Flotow , Corydon C. Roeseler , Daniel Pepin Reiss
CPC classification number: B64C27/48 , B64C25/08 , B64C27/001 , B64C27/08 , B64C27/26 , B64C27/32 , B64C39/024 , B64C2027/003 , B64C2201/021 , B64C2201/024 , B64C2201/027 , B64C2201/042 , B64C2201/082 , B64C2201/108 , B64C2201/12 , B64C2201/146 , B64C2201/182 , B64C2201/201 , B64D1/00 , B64D1/02 , B64D1/12 , B64D3/00 , B64D5/00 , B64D35/02 , B64F1/02 , B65D25/10 , B65D85/68 , B65D2585/687
Abstract: The present disclosure provides various embodiments of a multicopter-assisted launch and retrieval system generally including: (1) a multi-rotor modular multicopter attachable to (and detachable from) a fixed-wing aircraft to facilitate launch of the fixed-wing aircraft into wing-borne flight; (2) a storage and launch system usable to store the modular multicopter and to facilitate launch of the fixed-wing aircraft into wing-borne flight; and (3) an anchor system usable (along with the multicopter and a flexible capture member) to retrieve the fixed-wing aircraft from wing-borne flight.
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