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公开(公告)号：US09908638B1
公开(公告)日：2018-03-06
申请号：US15167424
申请日：2016-05-27
Applicant: Kitty Hawk Corporation
Inventor： Zachais Vawter , Todd Reichert
IPC: B64C27/00 , B64D45/04 , B64D1/12 , B64D1/10 , B64C39/02 , B64D17/80 , B64D17/72 , B64D25/08 , G05D1/10 , B64D45/00
CPC classification number: B64D45/04 , B64C39/024 , B64C2201/042 , B64C2201/185 , B64D1/10 , B64D1/12 , B64D17/725 , B64D17/80 , B64D25/08 , B64D2045/008 , G05D1/101
Abstract: A ballistic parachute is released to slow descent of a cabin and an airframe where the airframe supports a plurality of rotors and the cabin removably attaches to the airframe. A ground condition is detected and it is decided whether to detach the airframe from the cabin. The airframe is detached from the cabin in response to the decision.
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公开(公告)号：US09908629B2
公开(公告)日：2018-03-06
申请号：US15436604
申请日：2017-02-17
Applicant: Indemnis, Inc.
Inventor： Alan Jamal Erickson
CPC classification number: B64D17/72 , B64C39/024 , B64C2201/027 , B64C2201/185 , B64D17/80 , B64D25/00 , B64D2201/00
Abstract: A system and method that reduces the descent velocity of an aerial vehicle, the system including a control system, an inflation device, and a deployable, inflatable cage. The control system detects a descent condition, such as an uncontrolled descent and activates the inflation device to inflate the cage to at least partially encase the aerial vehicle and protect the vehicle during descent and landing. The inflatable cage includes a main fill tube, a perimeter tube, and support tubes. The support tubes are connected between the main fill tube and the perimeter tube, and enable gas to flow from the inflation device through the support and perimeter tubes and into the perimeter tube. A drag inducing material enclosure is connected to the inflatable cage and structured to induce drag to reduce a descent speed of the aerial vehicle.
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公开(公告)号：US20170313433A1
公开(公告)日：2017-11-02
申请号：US15521560
申请日：2015-07-07
Applicant: Yanmar Co., Ltd.
Inventor： Eiichi OZAKI
CPC classification number: B64D27/24 , B64C25/32 , B64C27/08 , B64C39/024 , B64C2025/325 , B64C2201/024 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/185 , B64D17/80 , B64D2201/00 , Y02T50/44 , Y02T50/64
Abstract: A multicopter (100) having a plurality of propellers (1) is configured to be electrically operated. The multicopter (100) is provided with electric motors (2), at least one main battery (3), a generator (4), an engine (5), and a battery condition detecting section (71). The electric motors (2) drive the propellers (1). The main battery (3) is a first electric power source that supplies the electric power to the electric motors (2). The generator (4) is a second electric power source that supplies the electric power to the electric motors (2). The engine (5) drives the generator (4). The battery condition detecting section (71) detects abnormality of the main battery (3). When the battery condition detecting section (71) detects the abnormality of the main battery (3), the generator (4) supplies the electric power that has been converted from motive power from the engine (5) directly to the electric motors (2).
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公开(公告)号：US20170197725A1
公开(公告)日：2017-07-13
申请号：US15400796
申请日：2017-01-06
Applicant: Singapore Technologies Aerospace Ltd
Inventor： Chi Hui Frederic FOO , Han Lin HSI
CPC classification number: B64C39/024 , B64C2039/105 , B64C2201/063 , B64C2201/082 , B64C2201/104 , B64C2201/121 , B64C2201/141 , B64C2201/182 , B64C2201/185 , Y02T50/12
Abstract: An apparatus and method for aerial recovery of an unmanned aerial vehicle (UAV) are provided. The apparatus includes a rigid base having a first section and a second section, wherein the first section is securely mounted to a floor of an aircraft. The apparatus further includes a servicing platform moveably mounted to the base and configured to move along a direction parallel to a longitudinal axis of the aircraft such that in an extended position, the servicing platform at least partially protrudes from a rear cargo door of the aircraft, wherein the servicing platform comprises a capturing mechanism configured to capture the UAV in the extended position.
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公开(公告)号：US20170158337A1
公开(公告)日：2017-06-08
申请号：US15436604
申请日：2017-02-17
Applicant: Indemnis, Inc.
Inventor： Alan Jamal Erickson
CPC classification number: B64D17/72 , B64C39/024 , B64C2201/027 , B64C2201/185 , B64D17/80 , B64D25/00 , B64D2201/00
Abstract: A system and method that reduces the descent velocity of an aerial vehicle, the system including a control system, an inflation device, and a deployable, inflatable cage. The control system detects a descent condition, such as an uncontrolled descent and activates the inflation device to inflate the cage to at least partially encase the aerial vehicle and protect the vehicle during descent and landing. The inflatable cage includes a main fill tube, a perimeter tube, and support tubes. The support tubes are connected between the main fill tube and the perimeter tube, and enable gas to flow from the inflation device through the support and perimeter tubes and into the perimeter tube. A drag inducing material enclosure is connected to the inflatable cage and structured to induce drag to reduce a descent speed of the aerial vehicle.
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Patent Agency Ranking
公开(公告)号：US20170139420A1
公开(公告)日：2017-05-18
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：US20170108861A1
公开(公告)日：2017-04-20
申请号：US15391730
申请日：2016-12-27
Applicant: GoPro, Inc.
Inventor： Joseph Anthony Enke
CPC classification number: G05D1/0044 , B64C39/024 , B64C2201/024 , B64C2201/027 , B64C2201/108 , B64C2201/127 , B64C2201/141 , B64C2201/145 , B64C2201/146 , B64C2201/18 , B64C2201/185 , B64C2201/20 , G01C23/00 , G05D1/0022 , G05D1/0038 , G05D1/0088 , G05D1/101 , G05D1/102 , G07C5/08 , G08G5/0013 , G08G5/0021 , G08G5/0026 , G08G5/0034 , G08G5/0039 , G08G5/006 , G08G5/0069 , G08G5/0078 , G08G5/0086 , G08G5/0091 , G08G5/045 , H04B7/18504 , H04W84/042 , H04W84/12
Abstract: Disclosed is a configuration to control automatic return of an aerial vehicle. The configuration stores a return location in a storage device of the aerial vehicle. The return location may correspond to a location where the aerial vehicle is to return. One or more sensors of the aerial vehicle are monitored during flight for detection of a predefined condition. When a predetermined condition is met a return path program may be loaded for execution to provide a return flight path for the aerial vehicle to automatically navigate to the return location.
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公开(公告)号：US20170066537A1
公开(公告)日：2017-03-09
申请号：US14847332
申请日：2015-09-08
Applicant: Altus IP Limited
Inventor： Shaun Gordon MITCHELL , Ryan Harley CADWALLADER
CPC classification number: B64D17/80 , B64C39/024 , B64C2201/027 , B64C2201/108 , B64C2201/185 , B64D17/72
Abstract: A parachute deployment apparatus for use with an aircraft, including a deployment body with an internal cavity, the deployment body configured to house a parachute to be deployed through an upper opening of the internal cavity, a firing mechanism configured to release a pressurized gas into the internal cavity of the deployment body, wherein the apparatus includes a cap that engages with the upper opening to close it prior to deployment and is configured to be projected from the upper opening upon release of the pressurized gas into the internal cavity of the deployment body, and wherein the cap is connected to the parachute.
Abstract translation: 一种与飞行器一起使用的降落伞展开装置，包括具有内部空腔的展开体，所述展开体构造成容纳通过所述内部空腔的上部开口展开的降落伞;构造成将加压气体释放到 所述设备包括盖子，所述盖子与所述上部开口接合，以在展开之前将其封闭，并且构造成在将所述加压气体释放到所述展开体的内部空腔中时从所述上部开口突出， 并且其中所述盖连接到所述降落伞。
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公开(公告)号：US09557738B2
公开(公告)日：2017-01-31
申请号：US15134284
申请日：2016-04-20
Applicant: GoPro, Inc.
Inventor： Joseph Anthony Enke
CPC classification number: G05D1/0044 , B64C39/024 , B64C2201/024 , B64C2201/027 , B64C2201/108 , B64C2201/127 , B64C2201/141 , B64C2201/145 , B64C2201/146 , B64C2201/18 , B64C2201/185 , B64C2201/20 , G01C23/00 , G05D1/0022 , G05D1/0038 , G05D1/0088 , G05D1/101 , G05D1/102 , G07C5/08 , G08G5/0013 , G08G5/0021 , G08G5/0026 , G08G5/0034 , G08G5/0039 , G08G5/006 , G08G5/0069 , G08G5/0078 , G08G5/0086 , G08G5/0091 , G08G5/045 , H04B7/18504 , H04W84/042 , H04W84/12
Abstract: Disclosed is a configuration to control automatic return of an aerial vehicle. The configuration stores a return location in a storage device of the aerial vehicle. The return location may correspond to a location where the aerial vehicle is to return. One or more sensors of the aerial vehicle are monitored during flight for detection of a predefined condition. When a predetermined condition is met a return path program may be loaded for execution to provide a return flight path for the aerial vehicle to automatically navigate to the return location.
Abstract translation: 公开了一种用于控制飞行器的自动返回的配置。 该配置将返回位置存储在飞行器的存储装置中。 返回位置可以对应于飞行器返回的位置。 在飞行中监视航空器的一个或多个传感器以检测预定义的状况。 当满足预定条件时，可以加载返回路径程序以执行以提供飞行器自动导航到返回位置的返回飞行路径。
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公开(公告)号：US09555885B2
公开(公告)日：2017-01-31
申请号：US15231579
申请日：2016-08-08
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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