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公开(公告)号：EP0184226B1
公开(公告)日：1988-09-14
申请号：EP85116421.0
申请日：1983-10-12
Applicant: DORNIER GMBH
Inventor： Friedel, Franz , Frühauf, Werner , Harms, Günter , Heise, Georg, Dipl.-Ing. , Lükewille, Heinrich, Dipl.-Ing.
CPC classification number: F42B10/64 , B64C39/024 , B64C2201/028 , B64C2201/044 , B64C2201/165 , B64C2201/201 , F16D7/021 , F42B15/105
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公开(公告)号：EP0184226A3
公开(公告)日：1987-05-06
申请号：EP85116421
申请日：1983-10-12
Applicant: DORNIER GMBH
Inventor： Friedel, Franz , Frühauf, Werner , Harms, Günter , Heise, Georg, Dipl.-Ing. , Lükewille, Heinrich, Dipl.-Ing.
CPC classification number: F42B10/64 , B64C39/024 , B64C2201/028 , B64C2201/044 , B64C2201/165 , B64C2201/201 , F16D7/021 , F42B15/105
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公开(公告)号：EP0184226A2
公开(公告)日：1986-06-11
申请号：EP85116421.0
申请日：1983-10-12
Applicant: DORNIER GMBH
Inventor： Friedel, Franz , Frühauf, Werner , Harms, Günter , Heise, Georg, Dipl.-Ing. , Lükewille, Heinrich, Dipl.-Ing.
CPC classification number: F42B10/64 , B64C39/024 , B64C2201/028 , B64C2201/044 , B64C2201/165 , B64C2201/201 , F16D7/021 , F42B15/105
Abstract: Unbemannter Flugkörper, der in einem Behälter transportiert und aus dem Behälter mittels eines Hilfsantriebes nach Lösung einer Arretierung gestartet wird und der während des Marschfluges durch ein Propellertriebwerk antreibbar ist, wobei eine Reibschlußkupplung (64, 65) am Flugkörper vorgesehen ist, die ohne Zuführung von Energie von aussen mittels des Antriebes (7) den innerhalb des Behälters (1') stillstehenden Propeller (6) mit dem bereits im Behälter laufenden Antriebsmotor (7) nach Verlassen des Behälters kuppelt.
Abstract translation: 这是在一个容器中的锁定机构的释放和后运送并从容器推出由辅助驱动装置无人驾驶飞机是由一个螺旋桨发动机，其特征在于，摩擦离合器（64，65）被设置在导弹，巡航飞行期间驱动其中没有能量的供给 从由所述驱动装置的外侧（7），所述容器（1“）的螺旋桨（6）与当前容器内部的固定到驱动马达（7）在离开容器后脱离。
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公开(公告)号：US20190193839A1
公开(公告)日：2019-06-27
申请号：US13984688
申请日：2012-01-13
Applicant: Andreas Voss
Inventor： Andreas Voss
CPC classification number: B64C15/00 , B64C17/04 , B64C39/024 , B64C39/028 , B64C39/066 , B64C39/068 , B64C2201/104 , B64C2201/165
Abstract: The invention pertains to a remote-controlled miniature aircraft with at least one lift surface (17), with at least one pair of propeller drives (12, 13) and with a weight element (20), the position of which can be varied in the longitudinal direction of the miniature aircraft (10) in order to change the center of gravity of the miniature aircraft (10). In order to realize a more compact and more robust construction with improved flying characteristics, the lift surface (17) of the miniature aircraft (10) is arranged above a plane defined by the rotational axes of the propeller drives (12, 13) in order to generate a lifting force for taking off and/or landing from a standstill.
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公开(公告)号：US20180327090A1
公开(公告)日：2018-11-15
申请号：US15776489
申请日：2016-11-18
Applicant: CHOUETTE
Inventor： Cyril De CHASSEY , Charles NESPOULOUS
CPC classification number: B64C39/024 , A63H27/12 , B64C2201/027 , B64C2201/042 , B64C2201/165
Abstract: Drone comprising a central body and a plurality of arms, preferably at least three arms, each arm comprising a first end mounted on the central body, each arm comprising, in the vicinity of a second end, at least one electric motor and at least one propeller coupled to said electric motor, each arm accommodating at least one electric battery.
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Patent Agency Ranking
306.发明申请公开(公告)号：US20180304981A1
公开(公告)日：2018-10-25
申请号：US15493463
申请日：2017-04-21
Applicant: Avigilon Corporation
Inventor： Kevin Piette , Pietro Russo , Bo Yang Yu
CPC classification number: B64B1/66 , B60L11/1816 , B60L2200/10 , B64B1/30 , B64C39/024 , B64C2201/022 , B64C2201/127 , B64C2201/165 , B64D47/08 , H04N5/2252 , H04N7/185
Abstract: A surveillance drone is disclosed. The surveillance drone includes a gas-filled container and propellers for aerial mobility. The surveillance drone also includes an electronic surveillance sensing device positioned below the gas-filled container. The gas-filled container may be filled with a lighter than air gas such as, for example, helium.
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公开(公告)号：US20180273170A1
公开(公告)日：2018-09-27
申请号：US15927847
申请日：2018-03-21
Applicant: Regents of the University of Minnesota
Inventor： Ruben Raphael D'Sa , Nikolaos Papanikolopoulos , Devon Jenson , Travis Henderson , John Kilian
CPC classification number: B64C29/02 , B64C3/32 , B64C3/56 , B64C11/30 , B64C13/18 , B64C39/024 , B64C2201/042 , B64C2201/06 , B64C2201/102 , B64C2201/162 , B64C2201/165 , B64D27/24 , B64D2211/00
Abstract: An unmanned aerial vehicle (UAV) including wing sections and hinge assemblies. Each wing section includes an airfoil and a propulsion unit. The wing sections are arranged side-by-side, pivotably connected by the hinge assemblies to define an airframe module. The airframe module is transitionable between a fixed-wing state and a rotor state. In the fixed-wing state, the airframe module has an elongated shape extending between opposing, first and second ends. In the rotor state, the first end is immediately proximate the second end. With this construction, the UAV provides two distinct modes of flight (fixed-wing for low power flight, and rotor for high maneuverability flight (including hover)). The wing sections can carry solar cells and a battery. A maximum power point tracker (MPPT) can be provided for optimizing the match between the solar array and the battery. The propulsion unit can include a variable pitch propeller.
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公开(公告)号：US20180273166A1
公开(公告)日：2018-09-27
申请号：US15995419
申请日：2018-06-01
Applicant: Paul E. ARLTON , David J. ARLTON
Inventor： Paul E. ARLTON , David J. ARLTON
CPC classification number: B64C27/605 , B64C7/00 , B64C27/10 , B64C27/14 , B64C39/024 , B64C2027/8236 , B64C2027/8281 , B64C2201/027 , B64C2201/042 , B64C2201/082 , B64C2201/102 , B64C2201/108 , B64C2201/141 , B64C2201/146 , B64C2201/165 , B64C2201/201 , B64C2201/203 , B64C2201/205
Abstract: A rotary wing vehicle includes a body structure having an elongated tubular backbone or core, and a counter-rotating coaxial rotor system having rotors with each rotor having a separate motor to drive the rotors about a common rotor axis of rotation. The rotor system is used to move the rotary wing vehicle in directional flight.
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公开(公告)号：US20180254565A1
公开(公告)日：2018-09-06
申请号：US15755619
申请日：2016-08-25
Applicant: UVISION AIR LTD
Inventor： YEHUDA KOL
CPC classification number: H01Q25/005 , B64C39/024 , B64C2201/021 , B64C2201/122 , B64C2201/165 , H01Q1/286 , H01Q3/24 , H01Q9/0421
Abstract: Antennas configuration for unmanned aerial vehicle (UAV) comprising at least one pair of patch antennas. Each patch antenna having a patch mounted on a ground plane. A UAV body having at least one portion constructed of material that minimally attenuates the electromagnetic signal transmitted or received by said plurality of antennas. Wherein the at least one pair of Cpatch antennas are mounted within the UAV body and near the inner surface of the UAV body. Each antenna from the pair of patch antennas further installed opposite to one another and each of the patches facing outside from the UAV body.
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公开(公告)号：US10053213B1
公开(公告)日：2018-08-21
申请号：US15589409
申请日：2017-05-08
Applicant: Pinnacle Vista, LLC
Inventor： Haofeng Tu
CPC classification number: B64C27/26 , B64C27/82 , B64C29/0025 , B64C39/024 , B64C39/12 , B64C2027/8236 , B64C2201/021 , B64C2201/027 , B64C2201/042 , B64C2201/066 , B64C2201/088 , B64C2201/104 , B64C2201/108 , B64C2201/128 , B64C2201/165 , G05D1/0202 , G05D1/042 , G05D1/0858
Abstract: A multi-copter lift body aircraft has a push or pull propeller and a lift body that has a first airfoil shape on a front to rear cross-section and a second airfoil shape on a left to right cross-section. The lift body is made from a top shell and a bottom shell. The lift body has a nose and a tail. Multi-copter propellers are attached to the lift body. The multi-copter propellers provide a lift at low speeds and the lift body provides a lift at high speeds. Avionics can be stored in a hollow cavity of the lift body. The avionics may include a control circuit, batteries, and a radio receiver. The multi-copter has a lift body made from an upper shell and a lower shell. The lift body has an optimum attack angle at a cruising speed, and the lift body provides a combined lift mode.
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