中科微点-全球专利检索

  1. Login
  2. Sign Up

Search Results

119 records (took 0.025 seconds)

    MORPHING AIRCRAFT
    62.
    发明申请
    MORPHING AIRCRAFT 有权
    MORPHING飞机

    公开(公告)号：US20110155840A1

    公开(公告)日：2011-06-30

    申请号：US13061019

    申请日：2009-08-25

    Applicant: Richard Charles Lind, JR. ,  Daniel Thurmond Grant ,  David Eaton

    Inventor： Richard Charles Lind, JR. ,  Daniel Thurmond Grant ,  David Eaton

    IPC: B64C39/02 ,  B64C13/24 ,  B64C3/56 ,  B64C5/12 ,  B64C5/06 ,  B64C11/00 ,  G09F3/00 ,  B64C27/04 ,  B64C27/50

    CPC classification number: B64C39/024 ,  B60F3/00 ,  B64C37/00 ,  B64C2001/0045 ,  B64C2201/022 ,  B64C2201/027 ,  B64C2201/102 ,  B64C2201/108 ,  B64C2201/203

    Abstract: A morphing aircraft that is achieves multi-modality location and camouflage for payload emplacement The morphing aircraft includes a substantially cylindrical fuselage including a shape configured as a packaging container with a first end and a second end A set of wings is coupled to the fuselage The set of wings includes a first position where the set of wings is extended outwards from the fuselage and a second position where the set of wings is retracted inwards towards the fuselage A tail is coupled to the second end of the cylindrical fuselage The tail includes a first position where the tail is extended outward from the fuselage and a second position where the tail is retracted inward towards the fuselage A propeller is mounted to the first end of the fuselage An engine is mechanically coupled to the propeller The engine is enclosed within the fuselage and powers the propeller.

    Abstract translation: 实现多模式位置和伪装用于有效载荷的变形飞机变形飞机包括基本上圆柱形的机身，其包括被配置为具有第一端和第二端的包装容器的形状。一组翼结合到机身。该组 的翼部包括第一位置，其中所述一组翼从机身向外延伸，并且第二位置，其中该组翼向内朝向机身A缩回。尾部联接到圆柱形机身的第二端。尾部包括第一位置 其中尾部从机身向外延伸，而第二位置则是尾部朝向机身向内缩进。螺旋桨安装在机身的第一端。发动机机械地联接到螺旋桨。发动机被封闭在机身内并且动力 螺旋桨

    Unmanned Aerial Surveillance Device
    63.
    发明申请
    Unmanned Aerial Surveillance Device 审中-公开
    无人机空中监控装置

    公开(公告)号：US20100282897A1

    公开(公告)日：2010-11-11

    申请号：US11464973

    申请日：2006-08-16

    Applicant: Samuel de la Torre

    Inventor： Samuel de la Torre

    IPC: B64C3/56 ,  B64C3/00 ,  G01C21/00 ,  F42B25/00 ,  H04N7/18

    CPC classification number: B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/102 ,  B64C2201/105 ,  B64C2201/107 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/141 ,  B64C2201/201 ,  B64C2201/203

    Abstract: An aerial surveillance device is provided, comprising an image capturing device capable of being supported by an airframe structure above the ground. The airframe structure includes a body portion defining a longitudinal axis and configured to support the image-capturing device. A tail portion having control surfaces is operably engaged with the body portion along the axis. Transversely-extending wing portions are directly engaged with the body portion. Each wing portion is defined by longitudinally-opposed spars extending from a spaced-apart disposition at the body portion to a common connection distally from the body portion. The spars have a fabric extending therebetween to provide a wing surface. A support member extends along an aerodynamic center, transversely to the body portion, of each wing portion, to tension and rigidify the wing portions so as to provide a positive camber for the wing portions and to form an airfoil.

    Abstract translation: 提供了一种空中监视装置，包括能够由地面上方的机身结构支撑的图像捕获装置。 机身结构包括限定纵向轴线并被配置为支撑图像捕获装置的主体部分。 具有控制表面的尾部部分沿着轴线与主体部分可操作地接合。 横向延伸的翼部直接与主体部分接合。 每个翼部分由纵向相对的翼梁限定，纵向相对的翼梁从主体部分处的间隔设置延伸到远离主体部分的公共连接。 翼梁具有在其间延伸的织物以提供机翼表面。 支撑构件沿着空气动力学中心横向于每个翼部的主体部分延伸，以使翼部被张紧和刚化，以便为翼部提供正弧形并形成翼型。

    Stowable design for unmanned aerial vehicle
    64.
    发明申请
    Stowable design for unmanned aerial vehicle 审中-公开
    无人驾驶飞机的可存储设计

    公开(公告)号：US20060226280A1

    公开(公告)日：2006-10-12

    申请号：US11305524

    申请日：2005-12-16

    Applicant: James Alman

    Inventor： James Alman

    IPC: B64C1/00 ,  B64C3/00

    CPC classification number: B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/044 ,  B64C2201/105 ,  B64C2201/107 ,  B64C2201/121 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/146 ,  B64C2201/165 ,  B64C2201/201 ,  B64C2201/203

    Abstract: An unmanned aerial vehicle (UAV) having a design for optimum stowability and low cost. The UAV having a collapsible wing section which can be easily removed from the fuselage, allowing for quick assembly and disassembly and ease of portability. The unmanned aerial vehicle includes a primary wing assembly, a fuselage, a means for propelling the unmanned aerial vehicle, and means for remotely controlling the unmanned aerial vehicle. The primary wing assembly includes a wing having a center spar and two outwardly diverging side spars. The wing also has a pliable flexible material supported by the center spar and the at least two outwardly diverging side spars. The pylon is connected to the wing and supports the wing. The fuselage is connected to the pylon such that the pylon extends away from the fuselage and spaces the wing a distance from the fuselage. The fuselage includes a tail having a rudder located along a trailing edge and elevators located along the trailing edge.

    Abstract translation: 无人飞行器（UAV）具有最佳的可收藏性和低成本的设计。 无人机具有可折叠的机翼部分，可以方便地从机身中移除，从而实现快速组装和拆卸，便于携带。 无人飞行器包括主翼组件，机身，用于推动无人驾驶飞行器的装置，以及用于远程控制无人驾驶飞行器的装置。 主翼组件包括具有中心翼梁和两个向外发散的侧翼的翼。 机翼还具有由中心翼梁和至少两个向外发散的侧翼支撑的柔韧的柔性材料。 塔架连接到机翼并支撑机翼。 机身连接到挂架，使得吊架远离机身延伸，并将机翼与机身隔开一段距离。 机身包括尾部，尾部沿着后缘设有方向舵，沿着后缘设有电梯。

    Stealthy duffel bag airplane
    66.
    发明授权
    Stealthy duffel bag airplane 失效
    隐形行李袋飞机

    公开(公告)号：US06892981B2

    公开(公告)日：2005-05-17

    申请号：US10408981

    申请日：2003-04-08

    Applicant: Jay Lipeles

    Inventor： Jay Lipeles

    IPC: B64C3/30 ,  B64C3/56 ,  B64C39/02 ,  B64C39/10 ,  B64D33/04 ,  B64C39/00

    CPC classification number: B64C39/024 ,  B64C3/30 ,  B64C3/56 ,  B64C39/10 ,  B64C2201/028 ,  B64C2201/044 ,  B64C2201/046 ,  B64C2201/105 ,  B64C2201/127 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/203 ,  B64C2201/22 ,  B64D33/04 ,  B64D2033/045

    Abstract: The Duffel Bag Airplane is an inflatable flying wing unmanned airborne vehicle (UAV). The fuselage will house everything but the wings. The wing can be rolled up around the fuselage into a small package when deflated for easy transportation, such as by being carried in a duffle bag. Fabric construction, a small internal combustion engine with cooled exhaust, and wing warping controls combine to make the airplane inexpensive and extremely stealthy. All the usual signatures have been suppressed, which allow it to be used to make observations from close range under combat conditions. Control of this airplane is accomplished by warping the wings and is supplemented with stability augmentation.

    Abstract translation: Duffel Bag飞机是一种充气飞翼无人机载机（UAV）。 机身将会容纳除翅膀之外的所有东西。 机翼可以卷绕在机身周围，当放气以便于运输时，例如通过携带在行李箱中，成为小包装。 织物结构，具有冷却排气的小型内燃机和机翼翘曲控制相结合，使飞机廉价而且非常隐蔽。 所有通常的签名已经被压制，这允许它用于在战斗条件下从近距离观察。 这架飞机的控制是通过扭转机翼来实现的，并补充了稳定性增强。

    Payload delivery system
    67.
    发明申请
    Payload delivery system 审中-公开
    有效载送系统

    公开(公告)号：US20020066825A1

    公开(公告)日：2002-06-06

    申请号：US09884852

    申请日：2001-06-18

    Inventor： Carlos T. Miralles ,  Bart D. Hibbs

    IPC: B64C003/56

    CPC classification number: B64G1/222 ,  B64C1/30 ,  B64C3/56 ,  B64C39/024 ,  B64C2201/042 ,  B64C2201/082 ,  B64C2201/102 ,  B64C2201/126 ,  B64C2201/127 ,  B64C2201/128 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/148 ,  B64C2201/185 ,  B64C2201/203 ,  B64G1/105 ,  B64G1/62

    Abstract: Disclosed is a spacecraft carrying a number of pods, each containing an aircraft that has been folded to fit in the pod. Each aircraft has a vertical stabilizer and outboard wing-portions that fold around fore-and-aft axes. Each aircraft also has a fuselage that folds around a lateral axis. The spacecraft releases one or more of the pods into an atmosphere. Each of the pods is configured with an ablative heat shield and parachutes to protect its aircraft when the pod descends through the atmosphere. The pod releases its aircraft at a desired altitude or location, and the aircraft unfolds while free-falling. The aircraft then acquires and follows a flight path, and activates scientific experiments and instruments that it carries. The aircraft relays results and readings from the experiments and instruments to the spacecraft, which in turn relays the results and readings to a mission command center.

    Abstract translation: 公开了一种携带多个荚的飞船，每个荚都包含已折叠以适应荚的飞机。 每架飞机都有一个垂直的稳定器和外侧翼部分，它们围绕前后轴线折叠。 每架飞机还具有折叠横轴的机身。 航天器将一个或多个荚释放到气氛中。 每个荚配置有烧蚀式防护罩和降落伞，以在荚果通过大气层时保护其飞机。 吊舱将其飞机放置在所需的高度或位置，飞机在自由落体时展开。 飞机然后获得并遵循飞行路线，并激活它所携带的科学实验和仪器。 飞机将实验和仪器的结果和读数中继到航天器，然后将结果和读数中继到任务指挥中心。

    Shoulder launched unmanned reconnaissance system
    68.
    发明授权
    Shoulder launched unmanned reconnaissance system 失效
    肩膀发射无人侦察系统

    公开(公告)号：US6119976A

    公开(公告)日：2000-09-19

    申请号：US13551

    申请日：1998-01-27

    Applicant: Michael E. Rogers

    Inventor： Michael E. Rogers

    IPC: B64C39/02 ,  B64C3/56

    CPC classification number: B64C39/024 ,  B64C2201/042 ,  B64C2201/084 ,  B64C2201/102 ,  B64C2201/127 ,  B64C2201/146 ,  B64C2201/165 ,  B64C2201/203

    Abstract: A shoulder launched unmanned reconnaissance system for providing overhead visual surveillance of remote targets is disclosed. The present system includes a reconnaissance air vehicle which may be fired from a portable launcher, accelerated to flight speed, and remotely controlled using a ground control system. The vehicle is flown to the target area to enable an onboard wide angle video system to transmit video images of the target by radio or fiber optics link to the ground control system for processing and display. The ground control system enables the reconnaissance vehicle to be flown to a recovery area and to descend in a stall mode after the flight is completed for maintenance prior to reuse. The air vehicle includes collapsible wings which are deployable after launch by a spring actuated mechanism. The fuselage of the air vehicle carries an onboard video camera, an electric motor, a battery, a global positioning system receiver, flight controls, and a data link system.In an alternative embodiment, the fuselage of the air vehicle includes a storage bay with a rotary mechanism capable of deploying sensors for chemical and biological warfare agents or other dropable payloads such as dye markers for marking fleeing motor vehicles. The present system is capable of conducting overhead surveillance up to a range of approximately 10 kilometers.

    Abstract translation: 披露了发射无人侦察系统，用于提供远程目标的架空视觉监控。 本系统包括可从便携式发射器发射的加速飞行速度的遥感飞行器，并使用地面控制系统进行远程控制。 车辆飞行到目标区域，使得车载广角视频系统能够通过无线电或光纤链路将目标的视频图像传送到地面控制系统进行处理和显示。 地面控制系统使得侦察车辆能够在飞行完成之后飞行到恢复区域并以失速模式下降，以便在重新使用之前进行维护。 机动车辆包括可弹起的机翼，它们在由弹簧致动机构发射之后可部署。 机载机身载有车载摄像机，电动马达，电池，全球定位系统接收器，飞行控制和数据链接系统。 在替代实施例中，机动车辆的机身包括具有旋转机构的存储舱，该旋转机构能够部署用于化学和生物战剂或其它可下载的有效载荷的传感器，例如用于标记逃离机动车辆的染色标记。 目前的系统能够进行大约10公里范围的架空监视。

    Self-enclosed air vehicle
    69.
    发明授权
    Self-enclosed air vehicle 有权

    公开(公告)号：US11655026B2

    公开(公告)日：2023-05-23

    申请号：US17379942

    申请日：2021-07-19

    Applicant: GoPro, Inc.

    Inventor： Ryan Michael Goldstein

    IPC: B64C39/02

    CPC classification number: B64C39/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/20 ,  B64C2201/203

    Abstract: Vehicles such as unmanned air vehicles that are capable of movement from an open, flight configuration to an enclosed configuration in which all major flight components can be protected by an outer shell are disclosed. In the enclosed configuration, the vehicles can take on standard geometric shapes such as a rectangular prism, sphere, cylinder, or another shape, so as to not be recognizable as an unmanned air vehicle. Embodiments of vehicles can also include interchangeable and/or wireless motor arms, motor arms which are electrically connected to the remainder of the vehicle only when in an open configuration, remote controllers removably attached to the remainder of the vehicle, and clip or other attachment mechanisms for attachment to objects such as backpacks.

Patent Agency Ranking