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    Noise-suppressing strut support system for an unmanned aerial vehicle
    341.
    发明公开
    Noise-suppressing strut support system for an unmanned aerial vehicle 审中-公开
    德国文艺复兴开发银行

    公开(公告)号：EP2181921A2

    公开(公告)日：2010-05-05

    申请号：EP09168642.8

    申请日：2009-08-25

    Applicant: Honeywell International, Inc.

    Inventor： BOULDIN, Bruce Dan ,  BURDISSO, Ricardo

    IPC: B64C27/20 ,  B64C39/02

    CPC classification number: B64C27/20 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/162 ,  B64D2033/0206

    Abstract: A strut support system for a ducted fan unmanned aerial vehicle (12) to suppress noise comprising: a ducted fan fuselage (14) that defines an opening (42); an engine that extends longitudinally through the opening in the fuselage; a drive mechanism rotatably mounted to the engine, wherein a fan is mounted on the drive mechanism within a duct defined by the opening; and a plurality of struts (18) extending between the ducted fan fuselage and the engine each comprising a first leg (20) and a second leg (22) joined together by a curvilinear junction (24), wherein the first leg is attached to the ducted fan fuselage and the second leg is attached to the engine, wherein the plurality of struts are positioned upstream of the fan, wherein the junction between the first leg of each of the plurality of struts and the ducted fan fuselage is outside the highlight (26) of the ducted fan fuselage's leading edge (28).

    Abstract translation: 一种用于压缩噪声的管道风扇无人机（12）的支柱支撑系统，包括：限定开口（42）的管道风扇机身（14）; 发动机纵向延伸穿过机身中的开口; 驱动机构，其可旋转地安装在所述发动机上，其中风扇安装在所述驱动机构的由所述开口限定的导管内; 以及在所述管道风扇机身和所述发动机之间延伸的多个支柱（18），每个支柱包括通过曲线连接部（24）连接在一起的第一腿部（20）和第二腿部（22），其中所述第一腿部 管道风扇机身和第二条腿连接到发动机，其中多个支柱位于风扇的上游，其中，多个支柱中的每一个的第一腿与导管的风扇机身之间的接合处在高亮部分（26 ）风扇机身的前缘（28）。

    ANNULAR AIRBORNE VEHICLE
    342.
    发明公开
    ANNULAR AIRBORNE VEHICLE 有权
    环形飞机和工作程序

    公开(公告)号：EP2137069A2

    公开(公告)日：2009-12-30

    申请号：EP08736991.4

    申请日：2008-04-16

    Applicant: GO SCIENCE LIMITED

    Inventor： GOSLING, Harry, George, Dennis

    IPC: B64C39/06 ,  B64C39/02

    CPC classification number: B64C39/062 ,  B64C39/024 ,  B64C2201/028 ,  B64C2201/162

    Abstract: An airborne vehicle (1) having a wing-body (2) which defines a wing-body axis (3) and appears substantially annular when viewed along the wing-body axis, the interior of the annulus defining a duct (5) which is open at both ends. A propulsion system is provided comprising one or more pairs of propulsion devices (9, 10), each pair comprising a first propulsion device (9) mounted to the wing-body and positioned on a first side of a plane including the wing-body axis, and a second propulsion device (10) mounted to the wing-body and positioned on a second side of the plane including the wing-body axis. A direction of thrust of the first propulsion device can be adjusted independently of the direction of thrust of the second propulsion device and/or a magnitude of thrust of the first propulsion device can be adjusted independently of the magnitude of thrust of the second propulsion device. In certain embodiments the wing-body appears swept forward when viewed from a first viewing angle, and swept backward when viewed from a second viewing position at right angles to the first viewing angle.

    CARGO AIRCRAFT
    343.
    发明公开
    CARGO AIRCRAFT 有权
    FRACHTFLUGZEUG

    公开(公告)号：EP1833721A2

    公开(公告)日：2007-09-19

    申请号：EP05857018.5

    申请日：2005-11-22

    Applicant: Helou, Elie Jr.

    Inventor： Helou, Elie Jr.

    IPC: B64C1/22

    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: In one embodiment, an aircraft for transporting at least one cargo container is disclosed. The aircraft comprises a forward fuselage, an empennage, a beam structure, and mounts to detachably and structurally engage the at least one cargo container with the beam structure. The beam structure is disposed between the forward fuselage and the empennage and the beam structure configured to receive the at least one cargo container. The beam structure and structurally engaged cargo container provide sufficient structural rigidity to support the aircraft in flight.

    Abstract translation: 在一个实施例中，公开了一种运送至少一个货物集装箱的飞机。 飞行器包括前机身，尾翼，梁结构，以及可拆卸地和结构地接合具有梁结构的至少一个货物集装箱的安装件。 梁结构设置在前机身和尾翼之间，梁结构构造成接收至少一个货物集装箱。 梁结构和结构上接合的货物集装箱提供足够的结构刚度以支持飞行中的飞机。

    Unmanned mobile device
    347.
    发明公开
    Unmanned mobile device 有权
    无人移动设备

    公开(公告)号：EP1193168A3

    公开(公告)日：2003-03-12

    申请号：EP01121573.8

    申请日：2001-09-10

    Applicant: Rafael Armament Development Authority Ltd.

    Inventor： Yavnai, Arie

    IPC: B62D57/032 ,  B62D57/04

    CPC classification number: G05D1/0038 ,  B62D57/02 ,  B62D57/04 ,  B64C27/20 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/162 ,  B64C2201/165 ,  G05D1/0044

    Abstract: A remotely-controlled unmanned mobile device (UMD) adapted to function as a robot scout to enter and reconnoiter the site of a disaster and to communicate to a rescue mission information regarding conditions prevailing at the site, making it possible for the mission to decide on rescue measures appropriate to these conditions. The UMD is operable in either of two modes. In its air-mobility mode the UMD is able to vertically take off and land, to fly to the site and then hover thereover. In its ground-mobility mode, the UMD can walk on legs over difficult terrain and through wrecked structures and ruins. The UMD is provided with condition-sensitive sensors for gathering data regarding conditions prevailing at the site, and position-sensitive sensors for avoiding obstacles in the path of the walking UMD, thereby assuring safe mobility. Other sensors govern geo-referenced navigation and flight control functions.

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