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    FLYER ASSEMBLY
    181.
    发明申请
    FLYER ASSEMBLY 审中-公开
    飞机装配

    公开(公告)号：WO02032762A2

    公开(公告)日：2002-04-25

    申请号：PCT/US2001/031631

    申请日：2001-10-11

    IPC: B64C39/02 ,  F42B15/10 ,  B64C

    CPC classification number: F42B15/105 ,  B64C39/024 ,  B64C2201/042 ,  B64C2201/084 ,  B64C2201/102 ,  B64C2201/127 ,  B64C2201/146 ,  B64C2201/165 ,  B64C2201/185 ,  B64C2201/201

    Abstract: A flyer assembly is adapted for launching with, transit in, and deployment from an artillery shell having a central void region extending along a ballistic shell axis. The flyer assembly includes a jettisonable shroud and a flyer. The shroud extends along a shroud axis, and is positionable within the central void region with the shroud axis substantially parallel to the shell axis. The flyer is adapted to withstand a launch acceleration force along a flyer axis when in a first state, and to effect aerodynamic flight when in a second state. When in the first state, the flyer is positionable within the shroud with the flyer axis parallel to the shroud axis and the shell axis. The flyer includes a body member disposed about the flyer axis, and a foldable wing assembly mounted to the body member. The wing assembly is configurable in a folded state characterized by a plurality of nested wing segments when the flyer is in the first state. The wing assembly is configurable in an unfolded state characterized by a substantially uninterrupted aerodynamic surface when the flyer is in the second state. The flyer assembly is adapted to be launched from a ballistic delivery system such as an artillery cannon, and can thus reach a target quickly, without expending system energy stored within the flyer. During launch, the flyer is coupled to the shroud so as to maintain a portion of the flyer in tension during an acceleration of the flyer along the flyer axis resulting from the launch. The flyer assembly is adapted to withstand the high g-load an high temperature environments of a cannon launch, and can tolerate a set-back g load of about 16,000 g.

    Abstract translation: 飞行器组件适用于从具有沿弹道壳轴线延伸的中心空隙区域的炮弹发射，转移和展开。 传单组件包括可喷射的护罩和传单​​。 护罩沿护罩轴线延伸，并且可定位在中心空隙区域内，护罩轴线基本上平行于外壳轴线。 飞行器适于在处于第一状态时承受沿飞行器轴的发射加速力，并且在处于第二状态时实现空气动力学飞行。 当处于第一状态时，传单可定位在护罩内，飞翼轴线平行于护罩轴线和外壳轴线。 传单包括围绕飞翼轴设置的主体部件和安装到主体部件的可折叠翼组件。 机翼组件可配置成折叠状态，其特征在于当传单处于第一状态时由多个嵌套翼段组成。 机翼组件可配置为展开状态，其特征在于当传单处于第二状态时基本上不间断的空气动力学表面。 飞行器组件适于从诸如炮兵炮的弹道传送系统发射，并且因此可以快速到达目标，而不会消耗存储在飞行物内的系统能量。 在发射期间，传单联接到护罩上，以便在飞行物沿着由发射引起的飞翼轴的加速期间，使传单的一部分保持张紧。 飞行器组件适于承受大炮发射的高温环境的高负载，并且可以承受大约16,000g的安装载荷。

    AIRCRAFT WITH VERTICAL TAKEOFF AND LANDING AND ITS OPERATING PROCESS
    182.
    发明公开
    AIRCRAFT WITH VERTICAL TAKEOFF AND LANDING AND ITS OPERATING PROCESS 审中-公开

    公开(公告)号：EP3390224A1

    公开(公告)日：2018-10-24

    申请号：EP16831647.9

    申请日：2016-12-16

    Applicant: IOSIF, Taposu ,  RAZVAN, Sabie

    Inventor： RAZVAN, Sabie

    IPC: B64C39/00

    CPC classification number: B64C39/001 ,  B64C2201/027 ,  B64C2201/14 ,  B64C2201/162 ,  B64C2201/167 ,  B64C2201/185

    Abstract: The invention relates to an aircraft with vertical takeoff and landing and its operation method. Aircraft with vertical takeoff and landing of aerodyne type according to the invention comprises a circular symmetrical aerodynamic body (1) having an internal stiffening platform (2) located on the chord of the aerodynamic profile and which supports the components of the aircraft, at least four vertical ducted propellers (3a), (3b), (3c), (3d) arranged symmetrically to the central vertical axis of the carrier body (1), but also to the predetemined flight axis and to the transverse axis of the carrier body (1), propellers (3a) and (3c) having the same rotational direction opposite to that of propellers (3b) and (3d) at least two horizontal ducted propellers (4) with opposite rotation directions located inside the carrier body or outside of it, placed parallel symmetrical with the predetermined flight axis and on both sides of it, vector nozzles (5), one for each horizontal propeller (4), which provides vector orientation to jets of the horizontal ducted propellers (4), the means of power supply (6), which are designed to provide electricity necessary to operate all engines and all electrical and electronic devices on board, an electronic control and management flight module (7) and a landing gear (9), which aims to promote contact between the aircraft and the ground.

    INFLATABLE PARACHUTE AIRBAG SYSTEM
    184.
    发明公开
    INFLATABLE PARACHUTE AIRBAG SYSTEM 审中-公开
    充气式PARACHUTE空气囊系统

    公开(公告)号：EP3310659A1

    公开(公告)日：2018-04-25

    申请号：EP15895843.9

    申请日：2015-10-21

    Applicant: Erickson, Alan, Jamal

    Inventor： Erickson, Alan, Jamal

    IPC: B64D17/00 ,  B64D17/62 ,  B64D17/72

    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.

    IMPACT ABSORPTION APPARATUS FOR UNMANNED AERIAL VEHICLE
    187.
    发明公开
    IMPACT ABSORPTION APPARATUS FOR UNMANNED AERIAL VEHICLE 审中-公开
    STOSSDÄFFENDEVORRICHTUNGFÜREIN UNBEMANNTES LUFTFAHRZEUG

    公开(公告)号：EP3093239A1

    公开(公告)日：2016-11-16

    申请号：EP16159247.2

    申请日：2016-03-08

    Applicant: Disney Enterprises, Inc.

    Inventor： WONG, Clifford

    IPC: B64C39/00

    CPC classification number: B64D25/00 ,  B64C39/00 ,  B64C39/024 ,  B64C2201/00 ,  B64C2201/024 ,  B64C2201/14 ,  B64C2201/146 ,  B64C2201/18 ,  B64C2201/185

    Abstract: An unmanned aerial vehicle apparatus comprises a frame. Further, the unmanned aerial vehicle apparatus comprises a propulsion mechanism coupled to the frame that propels the frame through the air. In addition, the unmanned aerial vehicle apparatus comprises a storage device that stores one or more airbags and is coupled to the frame. The unmanned aerial vehicle apparatus also comprises an inflation device coupled to the frame that receives an activation signal and inflates the one or more airbags based upon receipt of the activation signal to deploy the one or more airbags from the storage device prior to an impact of the frame with an object.

    Abstract translation: 无人驾驶飞行器装置包括一个框架。 此外，无人驾驶飞行器装置包括联接到框架的推进机构，其推动框架通过空气。 此外，无人驾驶飞行器装置包括存储一个或多个安全气囊并连接到该框架的存储装置。 无人驾驶飞行器装置还包括耦合到框架的充气装置，其接收启动信号并且基于接收到激活信号而充气该一个或多个安全气囊，以在该冲击之前部署来自存储装置的一个或多个气囊 框架与对象。

    UNATTENDED GROUND SENSORS
    190.
    发明公开
    UNATTENDED GROUND SENSORS 有权
    Unbeaufsichtigte Bodensensoren

    公开(公告)号：EP2664945A1

    公开(公告)日：2013-11-20

    申请号：EP12382178.7

    申请日：2012-05-15

    Applicant: The Boeing Company

    Inventor： Scarlatti, David ,  Esteban-Campillo, David ,  Garcia, Javier

    IPC: G01V1/16 ,  F42B12/36

    CPC classification number: G01V1/168 ,  B64C27/51 ,  B64C27/68 ,  B64C39/02 ,  B64C2201/082 ,  B64C2201/123 ,  B64C2201/185 ,  F42B12/365 ,  G01V1/16 ,  G01V1/182

    Abstract: The present invention relates to unattended ground sensors for detecting the presence of a pedestrian or vehicle in a monitored area using seismic sensors. Networks of simple and inexpensive sensors are disclosed that may be rapidly deployed from the air. Each ground sensor is provided with a rotor that slows the rate of descent of the ground sensor during deployment.

    Abstract translation: 本发明涉及无人值守地面传感器，用于使用地震传感器来检测被监视区域中行人或车辆的存在。 公开了可以从空中快速部署的简单和便宜的传感器的网络。 每个地面传感器都设有一个转子，可在展开期间减慢地面传感器的下降速度。

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