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公开(公告)号：US20170233070A1
公开(公告)日：2017-08-17
申请号：US15256140
申请日：2016-09-02
Applicant: RALPH C. STARACE , ROBERT A. AUGUST , DOUGLAS L. FRONIUS , FRANCOIS CREASMAN
Inventor： RALPH C. STARACE , ROBERT A. AUGUST , DOUGLAS L. FRONIUS , FRANCOIS CREASMAN
CPC classification number: B64C29/02 , B64C3/56 , B64C9/00 , B64C27/57 , B64C39/024 , B64C2201/088 , B64C2201/102 , B64C2201/108 , B64C2201/141 , B64C2201/146 , G05D1/0011 , G05D1/0088 , G05D1/0858
Abstract: One example embodiment includes a vertical takeoff and landing (VTOL) unmanned aerial vehicle (UAV). The VTOL UAV includes a flight control system configured to provide avionic control of the VTOL UAV in a hover mode and in a level-flight mode. The VTOL UAV also includes a body encapsulating an engine and the flight control system. The VTOL UAV further includes a rotor disk coupled to the engine and configured to provide vertical thrust and cyclic pitch control in the hover mode and to provide horizontal thrust for flight during the level-flight mode.
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公开(公告)号：US20170217585A1
公开(公告)日：2017-08-03
申请号：US15328611
申请日：2015-07-21
Applicant: ATMOS UAV B.V.
Inventor： Sander HULSMAN , Jurjen DE GROOT , Maarten MILIS , Dirk Lucas Eduard DOKTER , Joost Leon BOUMAN , Ruud KNOOPS
CPC classification number: B64C29/02 , B64C39/024 , B64C2201/028 , B64C2201/042 , B64C2201/088 , B64C2201/104 , B64C2201/108 , B64C2201/165
Abstract: An aircraft, in particular an unmanned aerial vehicle with wing-borne flight mode and hover flight mode, comprises a wing structure (4) having a left (6), middle (7), and right wing section (8). A support structure extends from the wing structure (4), and has an upper and lower support section. Each one of the left and right wing section (6, 8), and upper and lower support section (18, 20) has a thrust unit (10, 12, 22, 24). Left and right wingtip sections are rotatable relative to a left and right wing base section, respectively, around an axis extending substantially in a lengthwise direction of the wing structure. The thrust units (10,12) of the left and right wing sections(6, 8) are provided at the respective wingtip sections, in particular at the extremities thereof.
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73.发明申请公开(公告)号：US20170190443A1
公开(公告)日：2017-07-06
申请号：US15466012
申请日：2017-03-22
Applicant: AeroVironment, Inc.
CPC classification number: B64F1/005 , B64C29/02 , B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/066 , B64C2201/088 , B64C2201/104 , B64C2201/12 , B64C2201/141 , B64C2201/165 , B64C2201/18 , B64C2201/201 , B64F1/12
Abstract: A vertical take-off and landing (VTOL) unmanned aerial vehicle (UAV) system including: a rearward facing tang extending from a rear fuselage portion of a VTOL UAV; one or more metallic contacts disposed on an exterior surface of the tang; a UAV pod including a landing surface; and an opening disposed in the landing surface to receive the tang.
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公开(公告)号：US20170158354A1
公开(公告)日：2017-06-08
申请号：US15360116
申请日：2016-11-23
Applicant: Sikorsky Aircraft Corporation
Inventor： Frederick L. Bourne , Peter James Waltner , Simon Gharibian
CPC classification number: B64C27/04 , B64C39/022 , B64C39/024 , B64C2027/8236 , B64C2201/027 , B64C2201/042 , B64C2201/06 , B64C2201/088 , B64C2201/12 , B64C2201/148 , B64D27/24 , B64D2027/026 , B64F1/36 , B64F3/02 , Y02T50/64
Abstract: A detachable power transfer device for a rotary-wing aircraft includes a docking station integrated into the rotary-wing aircraft. A power pod of the detachable power transfer device is constructed and arranged to detachably connect to the docking station for transferring power to the rotary-wing aircraft.
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75.发明申请公开(公告)号：US20170158327A1
公开(公告)日：2017-06-08
申请号：US15370592
申请日：2016-12-06
Applicant: AAI Corporation
Inventor： Neal H. Willford
CPC classification number: B64C39/024 , B64C25/34 , B64C27/50 , B64C29/02 , B64C2201/021 , B64C2201/042 , B64C2201/088 , B64C2201/104 , B64C2201/108 , B64C2201/162 , B64C2201/165 , B64D17/80 , G05D1/0055 , G05D1/0816 , G05D1/0858
Abstract: A technique is directed to operating an unmanned aerial vehicle (UAV) having a fuselage defining a flight direction of the UAV and wing-plate assemblies that propel the UAV in the flight direction defined by the fuselage. The technique involves providing, while the flight direction defined by fuselage of the UAV points vertically from a takeoff location on the ground, thrust from propulsion units of the wing-plate assemblies to fly the UAV along a vertical takeoff path. The technique further involves maneuvering, after the UAV flies along the vertical takeoff path, the UAV to align the flight direction along a horizontal flight path that is perpendicular to the vertical takeoff path. The technique further involves providing, after the UAV flies along the horizontal flight path, thrust from the propulsion units of the wing-plate assemblies to land the UAV along a vertical landing path that is perpendicular to the horizontal flight path.
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Patent Agency Ranking
公开(公告)号：US09632501B1
公开(公告)日：2017-04-25
申请号：US15180027
申请日：2016-06-12
Inventor： Jianjun Yang , Lin Yang
CPC classification number: G05D1/0011 , B64C19/00 , B64C39/024 , B64C2201/088 , B64C2201/108 , B64C2201/123 , B64C2201/146 , B64F1/007 , G05D1/0661 , G05D1/0669 , G06F3/017
Abstract: A method for controlling an unmanned aerial vehicle (UAV) is provided. The UAV comprises at least one rotor. The method includes receiving a take-off preparatory signal; controlling a rotation speed of the at least one rotor with an idle speed rotation in response to the take-off preparatory signal; increasing the rotation speed of the at least one rotor up to a rated speed rotation under predetermined conditions.
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77.发明申请POD COVER SYSTEM FOR A VERTICAL TAKE-OFF AND LANDING (VTOL) UNMANNED AERIAL VEHICLE (UAV) 审中-公开用于垂直起落架（垂直起降）的无人驾驶飞机（UAV）的POD覆盖系统公开(公告)号：US20170021942A1
公开(公告)日：2017-01-26
申请号：US15041758
申请日：2016-02-11
Applicant: AeroVironment, Inc.
CPC classification number: B64F1/005 , B64C29/02 , B64C39/024 , B64C2201/021 , B64C2201/088 , B64C2201/141 , B64C2201/201
Abstract: An unmanned aerial vehicle (UAV) storage and launch system includes a UAV pod having an open position and a closed position, the closed position establishing an interior that is weather resistant to an environment external to the UAV pod and a vertical takeoff and landing (VTOL) UAV enclosed in the UAV pod so that the UAV pod in the closed position provides a weather resistant interior for the VTOL UAV.
Abstract translation: 无人飞行器（UAV）存储和发射系统包括具有打开位置和关闭位置的无人机舱，该关闭位置建立了对无人机舱外部环境的耐候性和垂直起飞和着陆（VTOL ）无人机包围在无人机舱内，使无人机舱在关闭位置为VTOL无人机提供耐候性内部。
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78.发明申请POD OPERATING SYSTEM FOR A VERTICAL TAKE-OFF AND LANDING (VTOL) UNMANNED AERIAL VEHICLE (UAV) 审中-公开垂直起落架（VTOL）无人驾驶航空器（UAV）的POD操作系统公开(公告)号：US20170021941A1
公开(公告)日：2017-01-26
申请号：US15040940
申请日：2016-02-10
Applicant: AeroVironment, Inc.
CPC classification number: B64F1/005 , B64C29/02 , B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/088 , B64C2201/104 , B64C2201/108 , B64C2201/141 , B64C2201/146 , B64C2201/165 , B64C2201/201 , G05D1/0011 , G05D1/0022 , G05D1/102 , G08G5/0091
Abstract: A vertical take-off and landing (VTOL) unmanned aerial vehicle (UAV) storage and launch system includes a UAV pod having a UAV pod processor and a UAV selectively enclosed in the UAV pod, the UAV having only two rotors.
Abstract translation: 无人机（UAV）的垂直起降（VTOL）存储和发射系统包括一个UAV舱，其具有UAV舱处理器和UAV选择性地封闭在UAV舱内，无人机只有两个转子。
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79.发明申请POWER AND COMMUNICATION INTERFACE FOR VERTICAL TAKE-OFF AND LANDING (VTOL) UNMANNED AERIAL VEHICLES (UAVS) 有权垂直起落架（VTOL）无人机（UAVS）的动力和通讯接口公开(公告)号：US20170021923A1
公开(公告)日：2017-01-26
申请号：US15042090
申请日：2016-02-11
Applicant: AeroVironment, Inc.
CPC classification number: B64F1/005 , B64C29/02 , B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/066 , B64C2201/088 , B64C2201/104 , B64C2201/12 , B64C2201/141 , B64C2201/165 , B64C2201/18 , B64C2201/201 , B64F1/12
Abstract: A vertical take-off and landing (VTOL) unmanned aerial vehicle (UAV) system including: a rearward facing tang extending from a rear fuselage portion of a VTOL UAV; one or more metallic contacts disposed on an exterior surface of the tang; a UAV pod including a landing surface; and an opening disposed in the landing surface to receive the tang.
Abstract translation: 垂直起飞和着陆（VTOL）无人机（UAV）系统包括：从VTOL无人机的后部机身部分延伸的朝后的脚部; 设置在柄脚的外表面上的一个或多个金属触点; 包括着陆面的无人机荚; 以及设置在着陆表面中以接收柄脚的开口。
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公开(公告)号：US09550567B1
公开(公告)日：2017-01-24
申请号：US14524956
申请日：2014-10-27
Applicant: Amazon Technologies, Inc.
Inventor： Jack Erdozain, Jr. , Berk Ozturk , Nicholas Hampel Roberts , Brian C. Beckman
CPC classification number: B64C29/02 , B64C1/30 , B64C3/56 , B64C39/024 , B64C2201/021 , B64C2201/088 , B64C2201/102 , B64C2201/108 , B64C2201/128 , B64C2201/162 , B64C2201/18 , Y02T50/14
Abstract: This disclosure is directed to an unmanned aerial vehicle (“UAV”) that transitions in-flight between vertical flight configuration and horizontal flight configuration by changing an orientation of the UAV by approximately ninety degrees. The UAV may include propulsion units that are coupled to a wing. The wing may include wing segments rotatably coupled together by pivots that rotate to position the propulsion units around a center of mass of the UAV when the fuselage is oriented perpendicular with the horizon. In this vertical flight configuration, the UAV may perform vertical flight or hover. During the vertical flight, the UAV may cause the wing to extend outward via the pivots such that the wing segments become positioned substantially parallel to one another and the wing resembles a conventional fixed wing. With the wing extended, the UAV assumes a horizontal flight configuration that provides upward lift generated from the wing.
Abstract translation: 本公开涉及通过将UAV的方向改变大约九十度而在垂直飞行构型和水平飞行构型之间转换的无人驾驶飞行器（“UAV”）。 无人机可以包括联接到机翼的推进单元。 机翼可以包括通过枢转可旋转地联接在一起的翼段，当机身垂直于水平线时，枢轴旋转以将推进单元围绕UAV的质心定位。 在这种垂直飞行配置中，无人机可以执行垂直飞行或悬停。 在垂直飞行期间，UAV可以使机翼经由枢轴向外延伸，使得机翼段基本上彼此平行地定位，并且翼类似于常规的固定翼。 在机翼延伸的情况下，UAV采取水平飞行配置，提供从机翼产生的向上升力。
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