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公开(公告)号：US1769203A
公开(公告)日：1930-07-01
申请号：US35929029
申请日：1929-04-30
Applicant: BUCKLEY JOHN P
Inventor： BUCKLEY JOHN P
IPC: B64C39/02
CPC classification number: B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/121 , B64C2201/127 , B64C2201/146 , B64C2201/165 , B64C2201/185
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公开(公告)号：US10053217B2
公开(公告)日：2018-08-21
申请号：US14845988
申请日：2015-09-04
Applicant: LG ELECTRONICS INC.
Inventor： Taehoon Cho , Choonghwan Shin
IPC: B64C39/02 , B60P3/11 , B64F1/22 , A62C3/02 , G05D1/00 , G05D1/10 , G08G1/09 , G08G1/16 , B60Q1/52 , G08G1/04 , G08G1/0955 , G08G1/00
CPC classification number: B64C39/024 , A62C3/0242 , B60P3/11 , B60Q1/525 , B60Q7/00 , B60Q7/005 , B64C2201/027 , B64C2201/042 , B64C2201/08 , B64C2201/108 , B64C2201/122 , B64C2201/123 , B64C2201/126 , B64C2201/127 , B64C2201/128 , B64C2201/141 , B64C2201/185 , B64C2201/201 , B64C2201/208 , B64D1/16 , B64F1/222 , G05D1/0088 , G05D1/0094 , G05D1/101 , G08G1/04 , G08G1/09 , G08G1/0955 , G08G1/16 , G08G1/162 , G08G1/205 , G08G7/00
Abstract: An unmanned aerial vehicle according to the present invention includes a housing mounted on a vehicle and having an inner space, the housing provided with a launching unit, an unmanned aerial vehicle accommodated in the housing and configured to be launched from the housing when a driving state of the vehicle meets a preset condition, wing units mounted to the unmanned aerial vehicle and configured to allow the flight of the unmanned aerial vehicle in response to the launch from the housing, an output unit disposed on the unmanned aerial vehicle, and a controller configured to control the wing units to move the unmanned aerial vehicle to a position set based on information related to the driving state when the unmanned aerial vehicle is launched, and control the output unit to output warning information related to the driving state.
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公开(公告)号：US09963228B2
公开(公告)日：2018-05-08
申请号：US15200163
申请日：2016-07-01
Applicant: Bell Helicopter Textron Inc.
Inventor： John Richard McCullough , Paul K. Oldroyd
IPC: B64C29/00 , B64C39/08 , B64C39/02 , B64D27/12 , B64C11/28 , B64D17/80 , B64C1/28 , B64C1/32 , B64C17/02 , B64C27/26 , B64C27/28 , B64C29/02 , B64D25/12 , B64C27/30
CPC classification number: B64C29/0033 , B64C1/28 , B64C1/32 , B64C11/28 , B64C17/02 , B64C27/26 , B64C27/28 , B64C27/30 , B64C29/02 , B64C39/024 , B64C39/08 , B64C2201/088 , B64C2201/104 , B64C2201/108 , B64C2201/185 , B64C2211/00 , B64D17/80 , B64D25/12 , B64D27/12
Abstract: In some embodiments, an aircraft includes a flying frame having an airframe, a propulsion system attached to the airframe and a flight control system operably associated with the propulsion system wherein, the flying frame has a vertical takeoff and landing mode and a forward flight mode. A pod assembly is selectively attachable to the flying frame such that the flying frame is rotatable about the pod assembly wherein, the pod assembly remains in a generally horizontal attitude during vertical takeoff and landing, forward flight and transitions therebetween.
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公开(公告)号：US20180002011A1
公开(公告)日：2018-01-04
申请号：US15200163
申请日：2016-07-01
Applicant: Bell Helicopter Textron Inc.
Inventor： John Richard McCullough , Paul K. Oldroyd
CPC classification number: B64C29/0033 , B64C1/28 , B64C1/32 , B64C11/28 , B64C17/02 , B64C27/26 , B64C27/28 , B64C27/30 , B64C29/02 , B64C39/024 , B64C39/08 , B64C2201/088 , B64C2201/104 , B64C2201/108 , B64C2201/185 , B64C2211/00 , B64D17/80 , B64D25/12 , B64D27/12
Abstract: In some embodiments, an aircraft includes a flying frame having an airframe, a propulsion system attached to the airframe and a flight control system operably associated with the propulsion system wherein, the flying frame has a vertical takeoff and landing mode and a forward flight mode. A pod assembly is selectively attachable to the flying frame such that the flying frame is rotatable about the pod assembly wherein, the pod assembly remains in a generally horizontal attitude during vertical takeoff and landing, forward flight and transitions therebetween.
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公开(公告)号：US09834311B2
公开(公告)日：2017-12-05
申请号：US15065963
申请日：2016-03-10
Applicant: OPTiM Corporation
Inventor： Shunji Sugaya
CPC classification number: B64D25/00 , B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/146 , B64C2201/185
Abstract: The present invention is to prevent an uninhabited airborne vehicle from crashing due to fall impact and from being damaged and to protect an object and a living being at the fall point. The uninhabited airborne vehicle 100 includes a rotary wing 10 and a buffer 111 that reduces impact on the airframe when crashed. The battery charge remaining measurement module 122 and the distance measurement module 123 measure the battery charge remaining and the distance to an object, respectively, and compare the measurement with the respective thresholds. If the measurement is less than the respective thresholds, the buffer module 111 is driven by the drive module 121.
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Patent Agency Ranking
公开(公告)号：US20170267347A1
公开(公告)日：2017-09-21
申请号：US15612789
申请日：2017-06-02
Applicant: Flirtey Holdings, Inc.
Inventor： Joseph Rinaldi , Matthew Sweeny , Tom Bass , Jess Hayden , David Hobby , Christopher Galassini , John Johnson , Henri Spaile , Seaton Mckeon , Justin Wagemakers
CPC classification number: B64D1/22 , B26F3/12 , B64C25/58 , B64C39/024 , B64C2201/021 , B64C2201/024 , B64C2201/027 , B64C2201/108 , B64C2201/128 , B64C2201/141 , B64C2201/146 , B64C2201/185 , B64D1/02 , B64D17/00 , B64D17/70 , B64D17/80 , B65D81/022 , B65D81/18 , B65D81/3825 , B66D1/60 , G01S19/13 , G06Q50/28
Abstract: Disclosed is a package delivery mechanism (PDM) of an unmanned aerial vehicle (UAV). The PDM includes a gravity activated locking mechanism to lock and unlock a package attached to the UAV based on the weight of the package. When the package is attached to suspension means of the UAV that lowers the package to the ground from the UAV, the locking mechanism automatically engages with the package and keeps the package locked to the suspension means, due to the weight of the package. When the package is lowered and reaches on the ground, the weight of the package is offloaded from the suspension means, which enables the locking mechanism to be disengaged, thereby releasing the package. The PDM includes a severing module to sever the suspension means from the UAV.
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公开(公告)号：US20170139421A1
公开(公告)日：2017-05-18
申请号：US15419814
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：US09611045B2
公开(公告)日：2017-04-04
申请号：US14850642
申请日：2015-09-10
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 for resisting an uncontrolled descent or uncontrolled flight condition of an aerial vehicle. The system includes a control system, sensors, an inflation device, and a deployable, inflatable assembly. The control system detects an uncontrolled condition using the sensors, and subsequently initiates the inflation device to inflate the inflatable assembly. The assembly includes an inflatable cage stored on and deployed from the aerial vehicle upon detection of an uncontrolled condition. The inflatable cage includes a hub, a perimeter tube, and support tubes connected between the hub and perimeter tube. Fill tubes enable inflation of the support and perimeter tubes. The assembly includes a parachute-material enclosure connected to the inflatable cage and structured to create drag to reduce a velocity of the aerial vehicle when the inflatable assembly is deployed. The assembly includes weight distribution straps physically coupled between the vehicle and the enclosure or inflatable cage.
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公开(公告)号：US20160347462A1
公开(公告)日：2016-12-01
申请号：US14723897
申请日：2015-05-28
Applicant: Kespry, Inc.
Inventor： Robert Parker Clark
CPC classification number: B64D17/62 , B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/185 , B64D17/80 , B64D43/02 , G05D1/0072 , G05D1/0077 , G05D1/0088 , G05D1/105
Abstract: An unmanned aerial vehicle includes a closely integrated emergency recovery and operation systems for an unmanned aerial vehicle with built-in levels of redundancy and independence to maximize the likelihood of a controlled velocity landing. The unmanned aerial vehicle may include multiple processors and multiple state estimating modules such as inertial measurement units to independently determine the operational and error status of the unmanned aerial vehicle. Base on predictive or projected computations, the emergency recovery system may determine a suitable time for a recovery action, such as parachute deployment, and execute the recovery action.
Abstract translation: 无人机包括紧凑的紧急恢复和操作系统，用于具有内置冗余度和独立性的无人驾驶飞行器，以最大限度地发挥受控速度着陆的可能性。 无人驾驶飞行器可以包括多个处理器和多个状态估计模块，例如惯性测量单元，以独立地确定无人驾驶飞行器的操作和错误状态。 基于预测或预计计算，紧急恢复系统可以确定恢复动作（例如降落伞部署）的合适时间，并执行恢复动作。
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公开(公告)号：US20160347452A1
公开(公告)日：2016-12-01
申请号：US15231579
申请日：2016-08-08
Applicant: Ford Global Technologies, LLC
Inventor： Joe 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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