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公开(公告)号：US20190202554A1
公开(公告)日：2019-07-04
申请号：US15856301
申请日：2017-12-28
Applicant: Aurora Flight Sciences Corporation
Inventor： William Bosworth
CPC classification number: B64C39/024 , B25J5/00 , B25J15/0028 , B60L53/14 , B60L53/60 , B64C39/022 , B64C2201/027 , B64C2201/108 , B64C2201/12 , B64C2201/126 , B64C2201/187 , B64F1/007 , B64F1/16
Abstract: Disclosed herein are aircraft and landing gear systems configured to fix an aircraft to the ground. For example, the aircraft and aircraft systems configured for ground manipulation. In one aspect, an aircraft with an arm and end-effector may be fixed a ground surface to facilitate ground-based robotic manipulation tasks.
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公开(公告)号：US09977431B2
公开(公告)日：2018-05-22
申请号：US15419804
申请日：2017-01-30
Applicant: Ford Global Technologies, LLC
Inventor： John A. Lockwood , Joseph F. Stanek
CPC classification number: G05D1/0276 , B60R16/02 , B60W30/00 , B64C29/0008 , B64C29/0091 , B64C29/02 , B64C39/00 , B64C39/02 , B64C39/022 , B64C39/024 , B64C2201/00 , B64C2201/02 , B64C2201/08 , B64C2201/086 , B64C2201/088 , B64C2201/12 , B64C2201/126 , B64C2201/127 , B64C2201/14 , B64C2201/141 , B64C2201/18 , B64C2201/182 , B64C2201/185 , B64C2201/187 , B64C2201/20 , B64C2201/208 , B64C2230/00 , G05D1/0022 , G05D1/0088 , G05D1/0094 , G05D1/0202 , G05D1/0212 , G05D1/0231 , G05D1/0242 , G05D1/0255 , G05D1/0257 , G05D1/028 , G05D2201/0213 , G08C17/00 , G08G1/012 , G08G1/091
Abstract: This disclosure generally relates to an automotive drone deployment system that includes at least a vehicle and a deployable drone that is configured to attach and detach from the vehicle. More specifically, the disclosure describes the vehicle and drone remaining in communication with each other to exchange information while the vehicle is being operated in an autonomous driving mode so that the vehicle's performance under the autonomous driving mode is enhanced.
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公开(公告)号：US09694906B1
公开(公告)日：2017-07-04
申请号：US15132107
申请日：2016-04-18
Applicant: KING SAUD UNIVERSITY
Inventor： Shereef Aly Sadek
CPC classification number: B64C29/00 , B64C5/06 , B64C25/10 , B64C29/0075 , B64C39/024 , B64C39/08 , B64C39/12 , B64C2201/021 , B64C2201/042 , B64C2201/048 , B64C2201/088 , B64C2201/104 , B64C2201/162 , B64C2201/187
Abstract: The vertical takeoff and landing unmanned aerial vehicle includes a pair of selectively rotatable ducted fans and a selectively rotatable thrust vectoring nozzle providing vertical takeoff and landing for an unmanned aerial vehicle or a similar type of aircraft. A pair of fixed forward-swept wings are mounted on a rear portion of a fuselage, and a pair of canards are mounted on a top end of a forward portion of the fuselage. The pair of ducted fans are respectively mounted on free ends of the pair of canards, and are selectively rotatable about an axis parallel to a pitch axis of the fuselage. An engine is mounted in the rear portion of the fuselage, and a thrust vectoring nozzle is mounted on the rear portion of the fuselage for directing thrust exhaust from the engine. The thrust vectoring nozzle is selectively rotatable about an axis parallel to the pitch axis.
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公开(公告)号：US20170137118A1
公开(公告)日：2017-05-18
申请号：US15422105
申请日：2017-02-01
Applicant: Amazon Technologies, Inc.
Inventor： Nicholas Kristofer Gentry
CPC classification number: B64C25/001 , B64C25/10 , B64C25/18 , B64C25/24 , B64C25/32 , B64C25/52 , B64C39/024 , B64C2025/008 , B64C2201/027 , B64C2201/128 , B64C2201/18 , B64C2201/187 , B64D1/02 , G05D1/102
Abstract: This disclosure describes a configuration of an unmanned aerial vehicle (UAV) landing gear assembly that includes adjustable landing gear extension that may be extended or contracted so that the body of the UAV is contained in a horizontal plane when the UAV is landed, even on sloping surfaces. For example, when a UAV is landing, the slope of the surface may be determined and the landing gear extensions adjusted based on the slope so that the body of the UAV remains approximately horizontal when the UAV lands and is supported by the landing gear extensions.
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公开(公告)号：US20170029111A1
公开(公告)日：2017-02-02
申请号：US15264487
申请日：2016-09-13
Applicant: Astigan Limited
Inventor： Andrew Charles ELSON
CPC classification number: B64D5/00 , B64B1/40 , B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/066 , B64C2201/082 , B64C2201/104 , B64C2201/122 , B64C2201/123 , B64C2201/162 , B64C2201/187 , B64D2211/00
Abstract: An embodiment of an unmanned aerial vehicle, which may be connected to a lighter-than-air carrier, may have a ratio of a lifting force of the carrier to a weight of the vehicle from 1.1:1 to 3:1. The vehicle, excluding payload, may have a mass of from 30 kg to 150 kg. The vehicle may have a wingspan of from 20 m to 60 m.
Abstract translation: 可以连接到轻型承载人的无人驾驶飞行器的实施例可以具有从1.1:1到3:1的载体的提升力与车辆重量之比。 车辆（不包括有效载荷）的质量可能为30公斤至150公斤。 车辆可能具有20米至60米的翼展。
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Patent Agency Ranking
公开(公告)号：US20160288918A1
公开(公告)日：2016-10-06
申请号：US15090571
申请日：2016-04-04
Applicant: W. Morrison Consulting Group, Inc.
Inventor： William M. YATES , Robert USSERY , Byron YOUNG
CPC classification number: B64D39/00 , B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/066 , B64C2201/104 , B64C2201/127 , B64C2201/146 , B64C2201/187 , B64D5/00 , B64D27/24
Abstract: Electric aircraft, including in-flight rechargeable electric aircraft, and methods of operating electric aircraft, including methods for recharging electric aircraft in-flight, through the use of unmanned aerial vehicle (UAV) packs flying independent of and in proximity to the electric aircraft.
Abstract translation: 电动飞机，包括飞行中可充电电动飞机，以及运行电动飞机的方法，包括通过使用独立于飞机和飞机附近飞行的无人驾驶飞行器（UAV）组件，在飞行中为电动飞机充电的方法。
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公开(公告)号：US20160272308A1
公开(公告)日：2016-09-22
申请号：US14661955
申请日：2015-03-18
Applicant: Amazon Technologies, Inc.
Inventor： Nicholas Kristofer Gentry
CPC classification number: B64C25/001 , B64C25/10 , B64C25/18 , B64C25/24 , B64C25/32 , B64C25/52 , B64C39/024 , B64C2025/008 , B64C2201/027 , B64C2201/128 , B64C2201/18 , B64C2201/187 , B64D1/02 , G05D1/102
Abstract: This disclosure describes a configuration of an unmanned aerial vehicle (UAV) landing gear assembly that includes adjustable landing gear extension that may be extended or contracted so that the body of the UAV is contained in a horizontal plane when the UAV is landed, even on sloping surfaces. For example, when a UAV is landing, the slope of the surface may be determined and the landing gear extensions adjusted based on the slope so that the body of the UAV remains approximately horizontal when the UAV lands and is supported by the landing gear extensions.
Abstract translation: 本公开描述了无人机（UAV）起落架组件的构造，其包括可调节的起落架延伸部，其可以被延伸或收缩，使得当UAV降落时UAV的车身包含在水平面中，即使在倾斜 表面。 例如，当UAV着陆时，可以确定表面的斜率，并且基于斜率来调整起落架延伸部，使得当UAV着陆并由起落架延伸部支撑时，UAV的车身保持大致水平。
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公开(公告)号：US09409644B2
公开(公告)日：2016-08-09
申请号：US14333462
申请日：2014-07-16
Applicant: Ford Global Technologies, LLC
Inventor： Joseph F. Stanek , John A. Lockwood
CPC classification number: G05D1/0276 , B60R16/02 , B60W30/00 , B64C29/0008 , B64C29/0091 , B64C29/02 , B64C39/00 , B64C39/02 , B64C39/022 , B64C39/024 , B64C2201/00 , B64C2201/02 , B64C2201/08 , B64C2201/086 , B64C2201/088 , B64C2201/12 , B64C2201/126 , B64C2201/127 , B64C2201/14 , B64C2201/141 , B64C2201/18 , B64C2201/182 , B64C2201/185 , B64C2201/187 , B64C2201/20 , B64C2201/208 , B64C2230/00 , G05D1/0022 , G05D1/0088 , G05D1/0094 , G05D1/0202 , G05D1/0212 , G05D1/0231 , G05D1/0242 , G05D1/0255 , G05D1/0257 , G05D1/028 , G05D2201/0213 , G08C17/00 , G08G1/012 , G08G1/091
Abstract: This disclosure generally relates to an automotive drone deployment system that includes at least a vehicle and a deployable drone that is configured to attach and detach from the vehicle. More specifically, the disclosure describes the vehicle and drone remaining in communication with each other to exchange information while the vehicle is being operated in an autonomous driving mode so that the vehicle's performance under the autonomous driving mode is enhanced.
Abstract translation: 本公开总体上涉及一种汽车无人机部署系统，该系统至少包括车辆和可部署的无人机，其配置为从车辆附接和分离。 更具体地，本公开描述了当车辆以自主驾驶模式操作时彼此保持通信的车辆和无人机交换信息，使得车辆在自主驾驶模式下的性能得到增强。
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公开(公告)号：US20160179097A1
公开(公告)日：2016-06-23
申请号：US14901661
申请日：2013-06-24
Inventor： Chee Nam Chua , Junwei Choon , Kok Yong Lim
CPC classification number: G05D1/0676 , B64C13/18 , B64C25/32 , B64C39/024 , B64C2201/146 , B64C2201/187 , G05D1/0011 , G05D1/0808
Abstract: Various embodiments provide a method for landing an unmanned aerial vehicle (UAV) in the presence of a wind. The method comprises: performing a first flare-maneuver whilst the UAV is flying. The flare-maneuver causes a front portion of the UAV to rise with respect to a rear portion of the UAV. The method also comprises steering the UAV along a path heading into a direction of the wind. The method further comprises performing a second flare-maneuver before the UAV impacts a landing surface to land. Various embodiments provide a corresponding UAV.
Abstract translation: 各种实施例提供了一种在存在风的情况下着陆无人驾驶飞行器（UAV）的方法。 该方法包括：在无人机飞行时执行第一次火炬弹。 火炬机动使无人机的前部相对于无人机的后部上升。 该方法还包括沿着朝向风向的路径转向无人机。 该方法还包括在UAV撞击着陆面到达之前进行第二次火炬弹。 各种实施例提供相应的无人机。
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公开(公告)号：US20160031564A1
公开(公告)日：2016-02-04
申请号：US14882254
申请日：2015-10-13
Applicant: Flight of the Century, Inc.
Inventor： William M. YATES
CPC classification number: B64D3/00 , B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/066 , B64C2201/104 , B64C2201/127 , B64C2201/187 , B64D33/00 , B64D39/00
Abstract: Electric aircraft, including in-flight rechargeable electric aircraft, and methods of operating electric aircraft, including methods for recharging electric aircraft in-flight, and method of deploying and retrieving secondary aircrafts.
Abstract translation: 电动飞机，包括飞行中可充电电动飞机，以及运行电动飞机的方法，包括为飞行中的电动飞机充电的方法，以及部署和检索二次飞机的方法。
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