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    MONO-RAIL CRANE SYSTEM IN AN AIRCRAFT
    64.
    发明公开
    MONO-RAIL CRANE SYSTEM IN AN AIRCRAFT 审中-公开
    单轨起重机系统在飞机上

    公开(公告)号：EP3254952A1

    公开(公告)日：2017-12-13

    申请号：EP16380027.9

    申请日：2016-06-07

    申请人： Airbus Defence and Space GmbH ,  Airbus Defence and Space, S.A.

    发明人： Lopez, Ana Rubio ,  Arias, Daniel Llanes ,  Martinez, Oscar ,  Lohmann, Ali ,  Weiß, Ulrich

    IPC分类号： B64C1/14 ,  B64C1/22 ,  B64D9/00

    CPC分类号： B64C1/22 ,  B64C1/1415 ,  B64D9/00 ,  B64F1/32 ,  B66C19/002

    摘要： The present disclosure relates to a mono-rail crane system (and a corresponding operation method) for use in an aircraft. The crane system comprises a first longitudinal mono-rail installable on the underside of a rear cargo door of the airplane parallel to the longitudinal axis of the rear cargo door; a second longitudinal mono-rail, which is installable on a cargo hold ceiling of the aircraft, and, in the fully opened state of the rear cargo door, in aligned continuity with the first longitudinal mono-rail so that the longitudinal axes of the first and second longitudinal mono-rails coincide to form one common longitudinal axis; a crane mobile equipment, CME, configured to be movable along the first and second longitudinal mono-rails in order to hoist and transfer the load; and a linear actuator configured to advance and retreat the second longitudinal monorail towards and away from the first longitudinal monorail.

    摘要翻译： 本公开涉及用于飞机中的单轨道起重机系统（以及相应的操作方法）。 起重机系统包括第一纵向单轨和第二纵向单轨，所述第一纵向单轨可平行于后货舱门的纵向轴线安装在飞机的后货舱门的下侧上; 可安装在飞机的货舱顶板上的第二纵向单轨以及在后货舱门的完全打开状态下与第一纵向单轨对准的连续性，使得第一纵向单轨的纵轴 和第二纵向单轨重合以形成一个共同的纵向轴线; 起重机移动设备CME，其被构造成可沿着第一和第二纵向单轨移动以起吊和传递负载; 以及构造成使第二纵向单轨朝向和远离第一纵向单轨前进和后退的线性致动器。

    DEFLECTOR ASSEMBLY FOR AN AIRCRAFT
    65.
    发明公开
    DEFLECTOR ASSEMBLY FOR AN AIRCRAFT 有权
    DEFLEKTORVORRICHTUNGFÜREIN FLUGZEUG

    公开(公告)号：EP3135577A1

    公开(公告)日：2017-03-01

    申请号：EP15400039.2

    申请日：2015-08-31

    申请人： AIRBUS HELICOPTERS DEUTSCHLAND GmbH

    发明人： Von-Wilmowsky, Kaspar ,  Ernst, Gerald

    IPC分类号： B64C1/22 ,  B64D1/22

    CPC分类号： B64C7/00 ,  B64C1/22 ,  B64C27/00 ,  B64D1/22

    摘要： The invention concerns a deflector assembly (3) for the rope / cable hanging from a hoist mounted on an aircraft (A).
    The deflector assembly (3) has an adjoined anchorage (7) that includes a socket face (39) that internally has a sliding bearing (15) in which is housed an innermost end (37), so that the innermost end (37) is slidably guided relative to the adjoined anchorage (7) to have one degree of freedom along a linear translation axis (LT). A remote anchorage has a support bracket for demountably mounting the remote anchorage to the fuselage.
    The rotorcraft can be chosen among: helicopters, hybrid rotary aircrafts, UAV rotorcrafts and inhabitable rotorcrafts including remote piloting functions.

    摘要翻译： 本发明涉及一种用于从安装在飞行器（A）上的起重机悬挂的绳索/缆索的偏转器组件（3）。 偏转器组件（3）具有邻接的锚固件（7），其包括内部具有滑动轴承（15）的插座面（39），其中容纳有最内端（37），使得最内端（37）为 相对于邻接的锚固件（7）滑动地被引导以沿着线性平移轴线（LT）具有一个自由度。 远程锚地有一个支撑支架，用于将远程锚固装置安装在机身上。 旋翼航空器可以选自：直升机，混合旋转飞机，无人机旋翼航空器和可居住的旋翼飞行器，包括远程驾驶功能。

    SYSTEM FOR TRANSPORTATION OF GOODS IN A LOADING SPACE
    68.
    发明公开
    SYSTEM FOR TRANSPORTATION OF GOODS IN A LOADING SPACE 审中-公开
    SYSTEM FOR货物在货运交通

    公开(公告)号：EP2139760A4

    公开(公告)日：2013-09-11

    申请号：EP08724255

    申请日：2008-03-19

    申请人： CROSSBORDER AERO TECHNOLOGIES AB

    发明人： NORDSTROEM CLAES

    IPC分类号： B64C1/22 ,  B60P1/36 ,  B60P1/38 ,  B64D9/00 ,  B64F1/32 ,  B65G21/06 ,  B65G21/14 ,  B65G25/06 ,  B65G47/88

    CPC分类号： B64F1/32 ,  B60P1/38 ,  B64D9/00 ,  B65G21/06 ,  B65G21/14 ,  B65G47/883 ,  B65G2201/0264 ,  Y02T50/46 ,  Y02T50/82

    摘要： The present invention relates to a system for transportation of goods in a loading space. The system comprises a conveyor (1) for goods which is drivable to and for in the loading space. To provide a quickly and easily fittable system for transportation of goods which is of low weight and easy to work with, the conveyor comprises a first element (3) with a goods-bearing belt and with a wall (6) disposed transversely to the driving directions of the conveyor, the goods-bearing belt being fastened to the wall via a first end portion, the wall being movable between a first extreme position (A) at or in the vicinity of an aperture to the loading space and a second extreme position at a far end of the loading space from said aperture, and a second element (4) disposed at or in the vicinity of the aperture to the loading space as a continuation of said first element of the conveyor, to which second element the goods-bearing belt is fastened via a second end portion and, during movement of said transverse wall between said extreme positions, is unwindable and windable about two elongate rollers (7, 8) supported for rotation in the vehicle at a distance from one another, so that the instantaneously uppermost strand of the goods-bearing belt wound about the rollers serves as a movable loading and unloading surface for goods between said rollers. The conveyor (1) is also configured to allow movement of the transverse wall (6) between said extreme positions and thus at the same time to unwind or wind the goods-bearing belt.

    BLENDED WING BODY CARGO AIRPLANE
    69.
    发明公开
    BLENDED WING BODY CARGO AIRPLANE 审中-公开
    混纺-WING-BODY-FRACHTFLUGZEUG

    公开(公告)号：EP2501611A1

    公开(公告)日：2012-09-26

    申请号：EP10757910.4

    申请日：2010-09-17

    申请人： The Boeing Company

    发明人： ODLE, Richard C. ,  ROMAN, Dino ,  RAWDON, Blaine Knight

    IPC分类号： B64C1/14 ,  B64C1/22 ,  B64C39/10

    CPC分类号： B64C39/10 ,  B64C1/1415 ,  B64C1/22 ,  B64C2039/105 ,  Y02T50/12

    摘要： A blended wing body cargo aircraft is disclosed. A body section defines a cargo volume, where an outer surface of the body section is shaped to provide an aerodynamic lifting surface. A cargo door and ramp structure is located in an aft end of the body section and is shaped to conform to an outer shape of the aerodynamic lifting surface when in a closed position. A control surface has a slightly cambered downward shape, and is positioned substantially near an aft end of the cargo door and ramp structure.