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公开(公告)号：US20180050785A1
公开(公告)日：2018-02-22
申请号：US15675046
申请日：2017-08-11
Applicant: JG Entrepreneurial Enterprises LLC
Inventor： John GOELET
IPC: B64B1/68 , B64B1/34 , B64B1/58 , B64B1/22 , B64B1/20 , B64B1/60 , B64C25/56 , B64B1/12 , B64C25/32 , B64B1/00 , B64B1/14 , B64B1/06
CPC classification number: B64B1/68 , B64B1/00 , B64B1/06 , B64B1/12 , B64B1/14 , B64B1/20 , B64B1/22 , B64B1/34 , B64B1/58 , B64B1/60 , B64B2201/00 , B64C25/32 , B64C25/56 , B64D2211/00 , Y02T50/55
Abstract: An airship is provided. The airship includes a hull configured to contain a gas, at least one propulsion assembly coupled to the hull and including a propulsion device, and at least one aerodynamic component including a plurality of fairing structures including one or more slats, wherein the at least one aerodynamic component is associated with the hull and is configured to direct airflow around the airship.
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102.发明授权公开(公告)号：US09852644B2
公开(公告)日：2017-12-26
申请号：US15193033
申请日：2016-06-25
Applicant: Bee Robotics Corporation
Inventor： Vladimir Salnikov , Anatoly Filin , Harm Burema
IPC: G08G5/00 , A01B79/00 , A01C21/00 , A01C7/00 , A01M9/00 , B64B1/40 , B64C39/02 , B64D1/16 , G05D1/00 , G08G5/04 , A01B79/02 , A01C7/04 , G05D1/10
CPC classification number: G08G5/0043 , A01B79/005 , A01B79/02 , A01C7/04 , A01C21/00 , B64B1/40 , B64B2201/00 , B64C39/024 , B64C2201/022 , B64C2201/027 , B64C2201/042 , B64C2201/101 , B64C2201/108 , B64C2201/12 , B64C2201/126 , B64C2201/141 , B64C2201/145 , B64C2201/146 , B64D1/00 , B64D1/16 , G05D1/104 , G08G5/04 , Y10S901/01
Abstract: Modern farming is currently being done by powerful ground equipment or aircraft that weigh several tons and treat uniformly tens of hectares per hour. Automated farming can use small, agile, lightweight, energy-efficient automated robotic equipment that flies to do the same job, even able to farm on a plant-by-plant basis, allowing for new ways of farming. A hybrid airship-drone has both passive lift provided by a gas balloon and active lift provided by propellers. A hybrid airship-drone may be cheaper, more stable in flight, and require less maintenance than other aerial vehicles such as quadrocopters. However, hybrid airship-drones may also be larger in size and have more inertia that needs to be overcome for starting, stopping and turning.
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公开(公告)号：US09745042B2
公开(公告)日：2017-08-29
申请号：US15242223
申请日：2016-08-19
Applicant: LTA CORPORATION
Inventor： John Goelet
IPC: B64B1/02 , B64B1/68 , B64B1/06 , B64B1/12 , B64B1/14 , B64B1/20 , B64B1/22 , B64B1/34 , B64B1/60 , B64C25/32 , B64C25/56 , B64B1/00 , B64B1/58
CPC classification number: B64B1/68 , B64B1/00 , B64B1/06 , B64B1/12 , B64B1/14 , B64B1/20 , B64B1/22 , B64B1/34 , B64B1/58 , B64B1/60 , B64B2201/00 , B64C25/32 , B64C25/56 , B64D2211/00
Abstract: An airship is provided. The airship includes a hull configured to contain a gas, at least one propulsion assembly coupled to the hull and including a propulsion device, and at least one aerodynamic component including a plurality of fairing structures including one or more slats, wherein the at least one aerodynamic component is associated with the hull and is configured to direct airflow around the airship.
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公开(公告)号：US09738369B2
公开(公告)日：2017-08-22
申请号：US15322933
申请日：2015-06-29
Inventor： Timur A. Mirzeabasov , Lidia N. Shkolina , Svetlana T. Romanova , Dimitrii O. Belov , Valery M. Volynkin , Vadim Y. Golovan , Fail N. Suleymanov , Igor Vodyanoy
CPC classification number: B64B1/66 , A62B5/00 , B64B1/06 , B64B1/14 , B64B1/22 , B64B1/34 , B64B2201/00 , B64C37/02 , B64D27/24
Abstract: The invention relates to a multipurpose airship and, more particularly, to a hybrid dirigible. The airship comprises a body (2) having a parallelepiped shape and docking means (8) comprising four rods connected by a frame and designed to be extractable from the body (2), the ends of these rods being provided each with at least one vacuum cup for adhering to a substantially vertical surface of a building. The docking means (8) are provided with grips adapted to engage with the docking means (8) of another airship of the same design. The invention also relates to a set of airships including at least two said airships. The proposed airship does not require a lot of space for its takeoff and provides fast and secure evacuation of people from tower buildings. In addition, the invention provides the possibility of varying the airship payload directly in flight depending of specific needs.
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公开(公告)号：US20160185447A1
公开(公告)日：2016-06-30
申请号：US14947871
申请日：2015-11-20
Applicant: AeroVironment, Inc.
Inventor： Carlos Thomas Miralles
CPC classification number: B64C13/16 , B64B2201/00 , B64C39/024 , B64C2201/04 , B64C2201/121 , B64C2201/141 , B64C2201/165 , F41G7/2253 , F41G7/2286 , F41G7/2293 , G05D1/12
Abstract: A system comprising an unmanned aerial vehicle (UAV) having wing elements and tail elements configured to roll to angularly orient the UAV by rolling so as to align a longitudinal plane of the UAV, in its late terminal phase, with a target. A method of UAV body re-orientation comprising: (a) determining by a processor a boresight angle error correction value bases on distance between a target point and a boresight point of a body-fixed frame; and (b) effecting a UAV maneuver comprising an angular role rate component translating the target point to a re-oriented target point in the body-fixed frame, to maintain the offset angle via the offset angle correction value.
Abstract translation: 一种包括具有翼元件和尾部元件的无人飞行器（UAV）的系统，其被配置成滚动以通过滚动来成角度地定向UAV，以便在其后期终点阶段将UAV的纵向平面与目标对准。 一种UAV身体重定向的方法，包括：（a）由处理器确定基于身体固定框架的目标点和视轴之间的距离的视轴角度误差校正值; 和（b）实现UAV机动，其包括将目标点平移到身体固定框架中的重定向目标点的角度角色率分量，以经由偏移角度校正值来保持偏移角度。
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Patent Agency Ranking
公开(公告)号：US20160137281A1
公开(公告)日：2016-05-19
申请号：US14898708
申请日：2014-06-26
Applicant: Plimp, Inc.
Inventor： James C. Egan , Joel D. Egan
CPC classification number: B64B1/20 , B64B1/14 , B64B1/22 , B64B1/28 , B64B1/30 , B64B1/34 , B64B1/38 , B64B1/58 , B64B1/60 , B64B1/70 , B64B2201/00 , B64C39/024 , B64C2201/022 , B64C2201/101 , B64C2201/104
Abstract: A hybrid VTOL vehicle having an envelope configured to provide hydrostatic buoyancy, a fuselage attached to the envelope and having at least one pair of wings extending from opposing sides thereof to produce dynamic lift through movement, and a thrust generation device on each wing and configured to rotate with each wing about an axis that is lateral to a longitudinal axis of the envelope to provide vertical takeoff or landing capabilities. Ideally, the envelope provides negative hydrostatic lift to enhance low-speed and on-the-ground stability.
Abstract translation: 一种具有被配置成提供静压浮力的封套的混合式垂直起落车，其附接到所述封套的机身，并且具有从其相对侧延伸的至少一对翼片，以产生通过运动的动力升降;以及每个机翼上的推力产生装置， 围绕围绕纵向轴线的侧壁的轴线旋转，以提供垂直起飞或着陆能力。 理想情况下，信封提供负静液压升力，以提高低速和地面的稳定性。
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公开(公告)号：US20160052614A1
公开(公告)日：2016-02-25
申请号：US14835196
申请日：2015-08-25
Applicant: Aether Industries, LLC.
Inventor： Benjamin Wesley Longmier , John Mark Guthery , John Patrick Sheehan , Benjamin Natan Wachs
CPC classification number: B64B1/02 , B64B2201/00 , G01W1/08 , G05D1/105
Abstract: A payload delivery and recovery system, having a payload including a data collection device arranged to collect data, and a controllable ascent vehicle comprising a controllable lighter than air (LTA) mechanism detachably coupled to the payload and used during an ascent phase to deliver the payload to a pre-determined altitude. The payload delivery and recovery system also having a controllable descent mechanism releasably attached to the controllable ascent vehicle and that can be used during a descent phase for reducing a rate of descent of the payload subsequent to release of the payload at the pre-determined altitude and including a control system for navigating the payload to a desired ground location during a recovery phase.
Abstract translation: 一种有效载荷递送和恢复系统，其具有包括布置成收集数据的数据收集装置的有效载荷，以及包括可拆卸地耦合到有效载荷并在上升阶段期间用于传递有效载荷的空气（LTA）机构的可控的轻量级车辆 到一个预定的高度。 有效载荷递送和恢复系统还具有可释放地附接到可控升降车辆的可控下降机构，并且可以在下降阶段期间使用，用于在预定高度释放有效载荷之后降低有效载荷的下降速率，以及 包括用于在恢复阶段将有效载荷导航到所需地面位置的控制系统。
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公开(公告)号：US20160023748A1
公开(公告)日：2016-01-28
申请号：US14341184
申请日：2014-07-25
Applicant: Scott R. Kempshall
Inventor： Scott R. Kempshall
CPC classification number: B64C3/46 , B64B1/08 , B64B1/14 , B64B1/26 , B64B1/58 , B64B2201/00 , B64C3/48 , B64C3/54 , B64C3/546 , B64C2201/022 , B64C2201/101 , B64C2201/105 , F03D1/04 , F03D9/25 , F03D9/32 , F05B2240/921 , Y02E10/725
Abstract: The present invention is a variable geometry lighter-than-air (LTA) aircraft that is adapted to morph its shape from a symmetric cross-section buoyant craft to an asymmetric lifting body and even to a symmetric zero lift configuration. The basic structure is a semi rigid airship with movable longerons. Movement of the longerons adjusts the camber of the upper and/or lower surfaces to achieve varying shapes of the lifting-body. This transformation changes both the lift and drag characteristics of the craft to alter the flight characteristics. The transformation may be accomplished while the craft is airborne and does not require any ground support equipment.
Abstract translation: 本发明是一种可变几何型轻型空中（LTA）飞机，其适于将其形状从对称横截面浮力工艺变形到非对称提升体，甚至变形成对称零升力构造。 基本结构是具有可移动隆起的半刚性飞艇。 仰角的运动调节上表面和/或下表面的弯度，以实现提升体的变化形状。 这种转变改变了飞行器的升力和阻力特性，以改变飞行特性。 转换可以在飞行器机载时完成，并且不需要任何地面支撑设备。
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公开(公告)号：US09211947B2
公开(公告)日：2015-12-15
申请号：US14016602
申请日：2013-09-03
Applicant: AEROVIRONMENT, INC.
Inventor： Carlos Miralles
CPC classification number: B64C13/16 , B64B2201/00 , B64C39/024 , B64C2201/04 , B64C2201/121 , B64C2201/141 , B64C2201/165 , F41G7/2253 , F41G7/2286 , F41G7/2293 , G05D1/12
Abstract: A system comprising an unmanned aerial vehicle (UAV) having wing elements and tail elements configured to roll to angularly orient the UAV by rolling so as to align a longitudinal plane of the UAV, in its late terminal phase, with a target. A method of UAV body re-orientation comprising: (a) determining by a processor a boresight angle error correction value bases on distance between a target point and a boresight point of a body-fixed frame; and (b) effecting a UAV maneuver comprising an angular role rate component translating the target point to a re-oriented target point in the body-fixed frame, to maintain the offset angle via the offset angle correction value.
Abstract translation: 一种包括具有翼元件和尾部元件的无人飞行器（UAV）的系统，其被配置成滚动以通过滚动来成角度地定向UAV，以便在其后期终点阶段将UAV的纵向平面与目标对准。 一种UAV身体重定向的方法，包括：（a）由处理器确定基于身体固定框架的目标点和视轴之间的距离的视轴角度误差校正值; 和（b）实现UAV机动，其包括将目标点平移到身体固定框架中的重定向目标点的角度角色率分量，以经由偏移角度校正值来保持偏移角度。
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公开(公告)号：US20150353180A1
公开(公告)日：2015-12-10
申请号：US14264022
申请日：2014-04-28
Applicant: Scott A. Strozier
Inventor： Scott A. Strozier
CPC classification number: B64B1/58 , B64B1/06 , B64B1/62 , B64B2201/00 , B64C2201/101 , B64C2201/104
Abstract: Lighter than air apparatuses include at least one ballast container having an electrically insulated and fire resistant, an envelop containing a gas and a plasma generating and heating assembly, where the containers provide lift by generating a plasma within the envelop. In certain embodiments, the envelop includes an expandable portion.
Abstract translation: 比空气装置更轻，包括至少一个具有电绝缘和防火的压载容器，包含气体的包络和等离子体产生和加热组件，其中容器通过在封套内产生等离子体来提供升力。 在某些实施例中，包络包括可扩张部分。
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