公开(公告)号：EP3006286A1

公开(公告)日：2016-04-13

申请号：EP15189107.4

申请日：2015-10-09

申请人： Goodrich Corporation

发明人： Himmelmann, Richard A.

IPC分类号： B60V3/02 ,  B64D9/00

CPC分类号： B64D9/00 ,  B60V3/025 ,  B64D2009/006 ,  B65G51/03 ,  B65G2814/0398

摘要： An air cushion cargo shuttle for loading and unloading cargo on an airplane is described. The air cushion cargo shuttle includes a first inner air curtain defining a first volume of pressurized air. The air cushion cargo shuttle also includes a noise barrier curtain enclosing the first inner air curtain. The noise barrier curtain is adapted to trap air leaking from the first inner air curtain.

摘要翻译： 描述了一种用于在飞机上装卸货物的气垫货运班车。 气垫货运班车包括限定第一体积的加压空气的第一内部空气幕。 气垫货物梭子还包括围绕第一内部空气幕的隔音幕。 隔音屏幕适于捕集从第一内部空气幕泄漏的空气。

公开(公告)号：EP3368414A1

公开(公告)日：2018-09-05

申请号：EP16788070.7

申请日：2016-10-25

申请人： Deutsche Post AG

发明人： PRUSKI, Matthäus ,  VORWERK, Felix ,  DAUTZ, Christoph

IPC分类号： B64C39/02 ,  B64D9/00 ,  B64F1/32

CPC分类号： B64F1/32 ,  B64C39/02 ,  B64C39/024 ,  B64C2201/128 ,  B64D9/00 ,  B65G67/00 ,  B65G2814/0398

摘要： The invention relates to a method by means of which an unmanned transport device (3) docked on a receiving container (1) is loaded with a payload container (7) for a consignment (4), having a loading device (8) for loading the transport device (3) with the payload container (7), wherein the payload container (7) has a bearing means (9) at its first end (8a), the transport device (3) has a loading opening (6) on its underside (5) for receiving the payload container (7), and the loading opening (6), at its front end (19), has a mating contour (20) corresponding to the bearing means (9), and the method has the following steps: the payload container (7), arranged on the loading device (8), is pivoted in relation to the horizontal by the loading device (8) such that the first end (8a) is elevated in relation to a second, opposite end (14) of the payload container (7), the loading device (8) is raised until the payload container (7) ends up at least with its first end (8a) located within and/or beneath the loading opening (6), and the payload container (7) is pivoted by the loading device into the horizontal for introduction into the loading opening (6) such that, first of all, the bearing means (9) comes into engagement with the mating contour (20) and, subsequently, the second end (14) of the payload container (7) comes into engagement with a rear end (22) of the loading opening (6).

公开(公告)号：EP3337725A1

公开(公告)日：2018-06-27

申请号：EP15754396.8

申请日：2015-08-17

申请人： John Bean Technologies Corporation

发明人： RODENKIRCH, Mark, James

IPC分类号： B64F1/32

CPC分类号： B64F1/32 ,  B65G39/04 ,  B65G69/22 ,  B65G2814/0398

摘要： An aircraft loader (54) includes an upper loading platform (50) and an underlying frame (52) with the frame utilizing the bogey suspension system (60), as well as carrying auxiliary lift system (400) at the rearward end thereof for assisting in the initial lifting of the platform relative to the frame. Powered roller assemblies (100,110,120, and 130), composed of hollow drive shafts, may be conveniently assembled and disassembled from the underside of loading platform (50). A plurality of upwardly convex-shaped static slider elements (200) facilitate unidirectional movement of loads on the platform (50). At the forward end of the platform, a guard or side rail (316) is rotatable from a retracted position within the confines of a control platform (68) to a forwardly directed position toward the fuselage of the aircraft. The side rail (316) is shaped to resemble the exterior cross-sectional shape of the fuselage, thereby to close the gap between the forward end of the loading platform and the fuselage, for the protection of loader personnel.