中科微点-全球专利检索

  1. Login
  2. Sign Up

Search Results

279 records (took 0.028 seconds)

    VERTICAL NON-BLADDERED FUEL TANK FOR A DUCTED FAN VEHICLE
    31.
    发明申请
    VERTICAL NON-BLADDERED FUEL TANK FOR A DUCTED FAN VEHICLE 有权
    垂直非叶轮燃油舱用于导向风扇

    公开(公告)号：US20100116827A1

    公开(公告)日：2010-05-13

    申请号：US12269132

    申请日：2008-11-12

    Applicant: Daniel Ross Collette

    Inventor： Daniel Ross Collette

    IPC: B65D88/12

    CPC classification number: B64C27/20 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/162 ,  B64D37/04 ,  B64D37/06 ,  B64D37/22 ,  Y10T137/86212 ,  Y10T137/86348

    Abstract: A vertical non-bladdered fuel tank for a ducted fan vehicle comprising: a pod that releasably connects to a core vehicle of a ducted fan vehicle, a vertical fuel tank contained by the pod, wherein the vertical fuel tank is centered between the fore and aft sides of the pod, an outlet in a floor of the vertical fuel tank located adjacent to a sidewall on the fore side of the vertical fuel tank, wherein the outlet is coupled to a draw tube contained by the core vehicle, and a pressure release vent located at the highlight of the pod's duct.

    Abstract translation: 一种用于管道式风扇车辆的垂直非风扇燃料箱，包括：可释放地连接到管道式风扇车辆的核心车辆的舱，由舱架容纳的垂直燃料箱，其中垂直燃料箱在前后之间居中 所述荚的侧面是垂直燃料箱的位于垂直燃料箱前侧的侧壁附近的出口，其中所述出口连接到由所述核心车辆容纳的牵引管，以及压力释放口 位于荚管道的高处。

    Ducted fan air vehicle with deployable wings
    32.
    发明授权
    Ducted fan air vehicle with deployable wings 失效
    带有可展翅膀的风扇飞机

    公开(公告)号：US07681832B2

    公开(公告)日：2010-03-23

    申请号：US11947585

    申请日：2007-11-29

    Applicant: John C. Colclough

    Inventor： John C. Colclough

    IPC: B64C15/00

    CPC classification number: B64C3/54 ,  B64C27/20 ,  B64C29/02 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/088 ,  B64C2201/102 ,  B64C2201/162 ,  Y02T50/14

    Abstract: A ducted fan air vehicle and method of operation is disclosed for obtaining aerodynamic lift and efficiency in forward flight operation without significantly impacting hover stability. One or more retractable wings are included on the ducted fan air vehicle and are deployed during forward flight to provide aerodynamic lift. The wing or wings are retracted when the vehicle hovers to reduce the impact the wings have on stability in a wind. Each wing may conform to the curvature or profile of the vehicle when retracted, and may be constructed in one or more wing sections. The wing or wings may be deployed and retracted automatically or at the command of an operator. Each wing and related components may be integrated into the vehicle or may be detachable.

    Abstract translation: 公开了一种管道风扇空气动力车辆和操作方法，用于在前进飞行操作中获得空气动力学提升和效率，而不会显着影响悬停稳定性。 一个或多个伸缩翼包括在管道式风扇飞行器上，并且在向前飞行期间部署以提供空气动力学提升。 当车辆悬停时，翼或翼缩回，以减少翼对风中的稳定性的影响。 每个翼可以在缩回时符合车辆的曲率或轮廓，并且可以构造在一个或多个翼部中。 机翼或机翼可以自动部署和撤回，或者在操作员的指令下进行。 每个翼和相关部件可以集成到车辆中或者可以是可拆卸的。

    GYRO-STABILIZED AIR VEHICLE
    33.
    发明申请
    GYRO-STABILIZED AIR VEHICLE 审中-公开
    GYRO稳定的空气车

    公开(公告)号：US20100012790A1

    公开(公告)日：2010-01-21

    申请号：US12426162

    申请日：2009-04-17

    Applicant: Nicolae Bostan

    Inventor： Nicolae Bostan

    IPC: B64C29/04

    CPC classification number: B64C3/385 ,  B64C17/06 ,  B64C27/20 ,  B64C29/0033 ,  B64C29/02 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/044 ,  B64C2201/048 ,  B64C2201/088 ,  B64C2201/104 ,  B64C2201/108 ,  B64C2201/127 ,  B64C2201/146 ,  B64C2201/162 ,  B64C2201/165 ,  Y02T50/14

    Abstract: A vertical takeoff and landing (VTOL) air vehicle disclosed. The air vehicle can be manned or unmanned. In one embodiment, the air vehicle includes two shrouded propellers, a fuselage and a gyroscopic stabilization disk installed in the fuselage. The gyroscopic stabilization disk can be configured to provide sufficient angular momentum, by sufficient mass and/or sufficient angular velocity, such that the air vehicle is gyroscopically stabilized during various phases of flight. In one embodiment the fuselage is fixedly attached to the shrouded propellers. In another embodiment, the shrouded propellers are pivotably mounted to the fuselage.

    Abstract translation: 一架垂直起降（VTOL）的空中客车。 机动车可以载人或无人驾驶。 在一个实施例中，空中交通工具包括安装在机身中的两个被覆盖的螺旋桨，机身和陀螺仪稳定盘。 陀螺稳定盘可以被配置成通过足够的质量和/或足够的角速度来提供足够的角动量，使得在飞行的各个阶段期间航空器的陀螺仪稳定。 在一个实施例中，机身固定地附接到被覆盖的螺旋桨。 在另一个实施例中，被覆盖的螺旋桨可枢转地安装在机身上。

    Airborne acoustic sensor array
    34.
    发明授权
    Airborne acoustic sensor array 失效
    机载声传感器阵列

    公开(公告)号：US07548488B2

    公开(公告)日：2009-06-16

    申请号：US11135931

    申请日：2005-05-23

    Applicant: Dan T. Horak ,  Richard A. Burne

    Inventor： Dan T. Horak ,  Richard A. Burne

    IPC: G01S3/80

    CPC classification number: B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/127 ,  B64C2201/141 ,  B64C2201/162 ,  B64C2201/165 ,  F42B12/365 ,  G01S3/8083

    Abstract: Embodiments for determining the bearings to targets from a remote location are disclosed. The apparatus consists of an array of acoustic sensors that is capable of autonomous flight. The array may be large in diameter, approximately one meter or greater. The apparatus is capable of navigating its flight to arrive at a predetermined location, measuring acoustic sound waves emitted by targets both during flight and after landing. The apparatus may then calculate the bearings to the targets and transmit this information to a remote location.

    Abstract translation: 公开了从远程位置确定到目标​​的轴承的实施例。 该装置由能够自主飞行的声学传感器阵列组成。 该阵列的直径可以大，大约一米或更大。 该装置能够导航其飞行到达预定位置，测量在飞行中和着陆之后目标发出的声音波。 然后，设备可以计算到目标的轴承并将该信息传送到远程位置。

    CARGO AIRCRAFT
    35.
    发明申请
    CARGO AIRCRAFT 有权
    货运飞机

    公开(公告)号：US20090026314A1

    公开(公告)日：2009-01-29

    申请号：US11782850

    申请日：2007-07-25

    Applicant: ELIE HELOU, JR.

    Inventor： ELIE HELOU, JR.

    IPC: B64C1/20 ,  B64C1/00

    CPC classification number: B64C1/10 ,  B64C1/00 ,  B64C1/061 ,  B64C1/065 ,  B64C39/02 ,  B64C39/024 ,  B64C2001/0072 ,  B64C2201/021 ,  B64C2201/048 ,  B64C2201/086 ,  B64C2201/104 ,  B64C2201/128 ,  B64C2201/162 ,  B64C2201/167 ,  B64C2211/00 ,  Y02T50/43

    Abstract: An aircraft for carrying at least one rigid cargo container includes a beam structure with a forward fuselage attached to the forward end of the beam structure and an empennage attached to the rearward end of the beam structure. Wings and engines are mounted relative to the beam structure and a fairing creates a cargo bay able to receive standard sized intermodal cargo containers. Intermodal cargo containers of light construction and rigid structure are positioned within the cargo bay and securely mounted therein. The beam structure is designed to support flight, takeoffs and landings when the aircraft is empty but requires the added strength of the containers securely mounted to the beam structure when the aircraft is loaded. The aircraft is contemplated to be a drone.

    Abstract translation: 用于承载至少一个刚性货物集装箱的飞机包括具有附接到梁结构的前端的前机身的梁结构和附接到梁结构的后端的后轮。 翼和发动机相对于梁结构安装，整流罩产生能够接收标准尺寸的联运货物集装箱的货舱。 轻型结构和刚性结构的多式联运集装箱定位在货舱内并牢固地安装在货舱内。 梁结构设计用于在飞机空置时支持飞行，起飞和着陆，但是当飞机加载时，需要将集装箱的强度牢固地安装到梁结构上。 飞机被认为是无人机。

    Umanned Helicopter
    36.
    发明申请
    Umanned Helicopter 有权
    无人直升机

    公开(公告)号：US20080251631A1

    公开(公告)日：2008-10-16

    申请号：US10572023

    申请日：2005-05-27

    Applicant: Hans-Georg Schiebel

    Inventor： Hans-Georg Schiebel

    IPC: B64C27/04

    CPC classification number: B64C39/024 ,  B64C2201/024 ,  B64C2201/108 ,  B64C2201/127 ,  B64C2201/146 ,  B64C2201/162 ,  B64C2201/165

    Abstract: The invention relates to an unmanned helicopter comprising an internal combustion engine and an associated fuel tank. The unit (1) formed by the internal combustion engine and the gearbox is arranged essentially in a self-supporting housing (2) which is at least partially closed all the way round, and preferably consists of carbon fibre-reinforced plastic (CFK), a nose body (3) being connected to the front of said housing. In this way, a compact structure can be achieved.

    Abstract translation: 本发明涉及一种包括内燃机和相关燃料箱的无人直升机。 由内燃机和齿轮箱形成的单元（1）基本上设置在自支撑壳体（2）中，该自支撑壳体（2）至少部分地完全闭合，并且优选地由碳纤维增强塑料（CFK）， 鼻体（3）连接到所述壳体的前部。 以这种方式，可以实现紧凑的结构。

    Air vehicle assembly and an associated control system and method
    37.
    发明授权
    Air vehicle assembly and an associated control system and method 有权
    机动车组件及相关控制系统及方法

    公开(公告)号：US07357352B2

    公开(公告)日：2008-04-15

    申请号：US11270342

    申请日：2005-11-09

    Applicant: Thomas E. Speer ,  Richard D. Jones

    Inventor： Thomas E. Speer ,  Richard D. Jones

    IPC: B64C37/02 ,  B64D5/00

    CPC classification number: B64C39/024 ,  B64C2201/027 ,  B64C2201/028 ,  B64C2201/088 ,  B64C2201/104 ,  B64C2201/108 ,  B64C2201/126 ,  B64C2201/162 ,  B64C2201/165 ,  B64D5/00

    Abstract: An air vehicle assembly and a corresponding method for launching an air vehicle assembly are provided, along with corresponding control systems and methods. The air vehicle assembly may include a plurality of air vehicles releasably joined to one another during a portion of the flight, such as during take-off and landing. By being releasably joined to one another, such as during take-off and landing, the air vehicles can rely upon and assist one another during the vertical take-off and landing while being designed to have a greater range and higher endurance following the transition to forward flight, either while remaining coupled to or following separation from the other air vehicles. By taking into account the states of the other air vehicles, the control system and method also permit the air vehicles of an air vehicle assembly to collaborate.

    Abstract translation: 提供了一种用于发射空中车辆组件的机动车组件和相应的方法，以及相应的控制系统和方法。 空中车辆组件可以包括在飞行的一部分期间例如在起飞和着陆期间可释放地彼此连接的多个空中飞行器。 通过可释放地彼此接合，例如在起飞和着陆期间，空中车辆可以在垂直起飞和着陆期间依靠和协助彼此，同时被设计成在过渡到 同时保持与其他空中客车分离的距离或距离。 通过考虑其他机动车辆的状态，控制系统和方法还允许机动车组件的空中车辆协作。

    Air vehicle assembly and an associated control system and method
    38.
    发明申请
    Air vehicle assembly and an associated control system and method 有权
    机动车组件及相关控制系统及方法

    公开(公告)号：US20070102565A1

    公开(公告)日：2007-05-10

    申请号：US11270342

    申请日：2005-11-09

    Applicant: Thomas Speer ,  Richard Jones

    Inventor： Thomas Speer ,  Richard Jones

    IPC: B64C29/00 ,  B64C37/02

    CPC classification number: B64C39/024 ,  B64C2201/027 ,  B64C2201/028 ,  B64C2201/088 ,  B64C2201/104 ,  B64C2201/108 ,  B64C2201/126 ,  B64C2201/162 ,  B64C2201/165 ,  B64D5/00

    Abstract: An air vehicle assembly and a corresponding method for launching an air vehicle assembly are provided, along with corresponding control systems and methods. The air vehicle assembly may include a plurality of air vehicles releasably joined to one another during a portion of the flight, such as during take-off and landing. By being releasably joined to one another, such as during take-off and landing, the air vehicles can rely upon and assist one another during the vertical take-off and landing while being designed to have a greater range and higher endurance following the transition to forward flight, either while remaining coupled to or following separation from the other air vehicles. By taking into account the states of the other air vehicles, the control system and method also permit the air vehicles of an air vehicle assembly to collaborate.

    Abstract translation: 提供了一种用于发射空中车辆组件的机动车组件和相应的方法，以及相应的控制系统和方法。 空中车辆组件可以包括在飞行的一部分期间例如在起飞和着陆期间可释放地彼此连接的多个空中飞行器。 通过可释放地彼此接合，例如在起飞和着陆期间，空中车辆可以在垂直起飞和着陆期间依靠和协助彼此，同时被设计成在过渡到 同时保持与其他空中客车分离的距离或距离。 通过考虑其他机动车辆的状态，控制系统和方法还允许机动车组件的空中车辆协作。

Patent Agency Ranking