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70 条记录 (耗时 0.019 秒)

    Steerable container delivery system
    42.
    发明公开
    Steerable container delivery system 审中-公开
    Steuerbares Frachtcontainerausgabesystem

    公开(公告)号：EP2565120A3

    公开(公告)日：2016-11-23

    申请号：EP12181639.1

    申请日：2012-08-24

    申请人： The Boeing Company

    发明人： Riley, David Ray ,  Nielsen, Zachary Anton

    IPC分类号： B64D1/14 ,  B64D1/08 ,  B64D17/34

    CPC分类号： B64D1/08 ,  B64D1/14 ,  B64D17/34

    摘要： A steerable container delivery system ("CDS") includes a pallet (130) configured with inflatable fins (135) for steering a CDS cargo bundle (115) during free fall when airdropped. The inflatable fins (135) are inflated shortly after deployment using compressed air carried by a tank in the pallet (133). A flight management computer ("FMS") continuously monitors the location of the CDS bundle (115) using GPS technology and determines a vector to a drop location based on stored GPS measurements. The FMC continuously monitors and positions the CDS bundle (115) over the drop location, and is able to independently rotate the fins (135) to control the position of the CDS bundle, either by rotating the CDS bundle (115) or laterally moving it. At the appropriate altitude, the FMC causes the main parachute to open to slow the descent of the CDS bundle for impact.

    摘要翻译： 可操纵的容器输送系统（“CDS”）包括配置有用于在自由落体时转向CDS货物束（115）的可充气翅片（135）的托盘（130）。 使用由托盘（133）中的罐携带的压缩空气使充气翅片（135）在展开后不久膨胀。 飞行管理计算机（“FMS”）使用GPS技术连续地监视CDS束（115）的位置，并且基于存储的GPS测量确定向下降位置的向量。 FMC连续监测和定位CDS束（115）在液滴位置上，并且能够独立地旋转翅片（135）以通过旋转CDS束（115）或横向移动CDS束来控制CDS束的位置 。 在适当的高度，FMC会使主降落伞打开，以减缓CDS束的影响。

    WIND PARAMETER INDICATION
    45.
    发明公开
    WIND PARAMETER INDICATION 有权
    WIND参数显示屏

    公开(公告)号：EP2812719A1

    公开(公告)日：2014-12-17

    申请号：EP13747169.4

    申请日：2013-01-14

    申请人： Ventus-Product Development & Consulting Ltd.

    发明人： HALFON, Itzhak ,  GALIM, Itay ,  GLOZMAN, Yaniv

    IPC分类号： G01S1/00 ,  G01S19/15 ,  G01S5/00 ,  G01W1/00 ,  B64D17/00

    CPC分类号： G01W1/02 ,  B64D1/08 ,  B64D17/00 ,  B64D45/00 ,  G01C5/00 ,  G01C17/00 ,  G01F1/76 ,  G01S7/003 ,  G01S17/023 ,  G01S17/88 ,  G01S17/95 ,  G01S19/14 ,  G01S19/15 ,  G01W1/08 ,  Y02A90/19

    摘要： Wind parameter indication device and method for providing an indication of wind speed and wind direction. The device is deployed along an aerial trajectory toward a ground surface, such as after being ejected from an aircraft in flight. The device includes an anemometer, an altimeter, a compass, a processor and a transmitter. The anemometer obtains local wind speed and local wind direction measurements along the trajectory. The altimeter obtains altitude measurements along the trajectory. The compass obtains direction measurements along the trajectory. The device may further include an accelerometer, for obtaining acceleration measurements along the trajectory. The processor determines a wind speed value and a wind direction value associated with a predetermined altitude of the device. The transmitter transmits the determined wind speed value and wind direction value to a remotely located receiver. The device may further include a stabilizing decelerator to stabilize and decelerate the device along the trajectory.

    AIRBORNE COOLING SYSTEM
    46.
    发明公开
    AIRBORNE COOLING SYSTEM 有权
    基于空气的冷却系统

    公开(公告)号：EP2691304A2

    公开(公告)日：2014-02-05

    申请号：EP12765288.1

    申请日：2012-03-28

    申请人： Rolls-Royce North American Technologies, Inc.

    发明人： GAGNE, Steven

    IPC分类号： B64D33/10 ,  B64D1/12

    CPC分类号： B64D1/08 ,  B64D13/00 ,  B64D33/10 ,  B64D2013/0614 ,  B64D2013/0674 ,  F28D5/00 ,  F28D2021/0021 ,  F41H13/0043 ,  F42B15/34

    摘要： An aircraft having a cooling system is disclosed. The cooling system can he used to cool a heat emitting component In one form the cooling system is a refrigerant system and includes a relatively high temperature device such as, but not limited to, a condenser. The relatively high temperature component is placed In thermal communication with a passing air flow. In one embodiment the aircraft includes a pod in which at least a portion of the cooling system is disposed. For example, a condenser of a vapor cycle refrigerant system can be located in the pod and in thermal communication with the air flow. The cooling system can also include a device capable of delivering a cooling fluid into the air flow and/or to the relatively high temperature component. The cooling fluid can he evaporated to provided additional cooling.

    APPARATUS FOR SUPPORTING A PARACHUTE FLIGHT CONTROLLER AND FLIGHT CONTROLLER FOR A PARACHUTE
    47.
    发明公开
    APPARATUS FOR SUPPORTING A PARACHUTE FLIGHT CONTROLLER AND FLIGHT CONTROLLER FOR A PARACHUTE 审中-公开
    装置用于支撑降落伞飞行控制器和飞行控制单元适用于降落伞

    公开(公告)号：EP2429899A1

    公开(公告)日：2012-03-21

    申请号：EP10774465.8

    申请日：2010-05-17

    申请人： Mist Mobility Integrated Systems Technology, Inc.

    发明人： McCANN , Sean ,  BAUMEISTER , Peter

    IPC分类号： B64D17/22 ,  B64D17/00

    CPC分类号： B64D17/025 ,  B64D1/08 ,  B64D17/343

    摘要： An apparatus for supporting a parachute flight controller from a parachute comprises a bearing member, for example a pulley, a load-bearing coupling, for example a harness, connected to the bearing member and including a connector for connecting the coupling to a parachute flight controller. The coupling includes a load-bearing connector for connecting a payload thereto, and the bearing member is adapted to enable relative movement, controlled by the flight controller, between the bearing member and a support member, for example a flexible coupling line or web for supporting the bearing member connected between first and second suspension lines of a parachute. The flight controller may include one or more control lines connected to the support member or suspension lines which can be wound in or out of the flight controller to effect relative movement between the bearing member and the support member and thereby control the direction of the parachute.

    AERIAL DELIVERY DEVICE
    48.
    发明公开
    AERIAL DELIVERY DEVICE 审中-公开
    航空运输设备

    公开(公告)号：EP2043915A2

    公开(公告)日：2009-04-08

    申请号：EP07808679.0

    申请日：2007-07-13

    申请人： Concept Solutions Limited

    发明人： REYNOLDS, Brad, Michael ,  KEPPEL, Matthew, John, Joseph

    IPC分类号： B64D1/02

    CPC分类号： B64D19/02 ,  B64D1/08

    摘要： An aerial delivery device which includes a carrier configured to carry an item for delivery, and one or more wings attached to the carrier and arranged to extend therefrom; wherein said aerial delivery device is configured to provide a controlled aerial descent under gravity, such that during the descent the aerial delivery device, or the or each wing, auto rotates.