公开(公告)号：EP2815969B1

公开(公告)日：2018-08-08

申请号：EP13172301.7

申请日：2013-06-17

申请人： Airbus Operations GmbH

发明人： Lohmann, Ali ,  Köhler, André ,  Völker, Johannes ,  Grambole, Christian ,  Ulbrich, Matthias ,  Pump, Jörg ,  Hager, Sönke

IPC分类号： B64D9/00

CPC分类号： B64D9/00 ,  B60P7/0892

摘要： The invention relates to a cargo handling system (1) for loading and securing one or more freight containers (C) in a cargo hold (H) of an aircraft (A). The system (1) comprises: a plurality of bracket members (2) configured to be secured to a base or floor of the cargo hold (H); and a plurality of elongate guide members (5), each of which is mounted on and interconnects a number of the bracket members (2) arranged in a row; wherein each guide member (5) forms a restraint or a stop against lateral movement of a freight container (C) loaded in the cargo hold (H). The bracket members (2) include at least one fastening portion (3) configured for tool-less fast-release engagement and locking with a seat track profile in the base or floor (F) of the cargo hold (H). Furthermore, the bracket members (2) typically extend transversely inwards or inboard of the elongate guide members (5).

公开(公告)号：EP2907749A1

公开(公告)日：2015-08-19

申请号：EP14154866.9

申请日：2014-02-12

申请人： Airbus Operations GmbH

发明人： Pump, Jörg ,  Hager, Sönke ,  Völker, Johannes ,  Köhler, André ,  Lohmann, Ali

IPC分类号： B64D9/00 ,  B60P7/14

CPC分类号： B64D9/003 ,  B60P1/00 ,  B60P7/14

摘要： The present disclosure pertains to a cargo restraining barrier configured to be mounted to a cargo deck surface of an aircraft, the cargo restraining barrier comprising a base portion having a top side and a bottom side opposite to the top side, a barrier portion being arranged substantially perpendicular to the base portion at a first edge on the top side of the base portion, a plurality of force diverting struts being mounted in parallel along the extension of the barrier portion between a backside of the barrier portion and a second edge of the base portion opposite to the first edge of the base portion, the force diverting struts being configured to divert forces acting on the front side of the barrier portion towards the base portion, and a plurality of first latches distributed over the bottom side of the base portion, the first latches being configured to hook into tie down rings of a cargo deck surface and to direct the diverted forces from the force diverting struts into the cargo deck surface.

摘要翻译： 本公开涉及一种构造成安装在飞行器的货物甲板表面上的货物限制障碍物，货物限制屏障包括具有顶侧和与顶侧相对的底侧的基部，阻挡部分基本上布置 在所述基部的顶侧的第一边缘处垂直于所述基部的多个力转向支柱沿所述阻挡部分的延伸部平行地安装在所述阻挡部分的后侧和所述基部的第二边缘之间 所述力转向支柱构造成将作用在所述阻挡部分的前侧上的力转向所述基部，以及分配在所述基部的底侧上的多个第一闩锁， 第一闩锁被配置成钩住货物甲板表面的紧固环并且将转向的力从力转向支柱引导到c argo甲板表面。

公开(公告)号：EP2759718B1

公开(公告)日：2017-04-05

申请号：EP14151963.7

申请日：2014-01-21

申请人： Airbus Operations GmbH

发明人： Esser, Markus ,  Lohmann, Ali ,  Pump, Jörg ,  Hager, Sönke ,  Völker, Johannes

IPC分类号： F16B21/02 ,  B64C1/20 ,  B64D9/00

CPC分类号： B64C1/20 ,  B60R11/00 ,  B64D9/00 ,  B64D9/003 ,  B64D2009/006 ,  B64G1/22 ,  B65G13/00 ,  B65G13/11 ,  B65G21/02 ,  B65G21/06 ,  B65G39/12 ,  F16B21/02

公开(公告)号：EP2815969A1

公开(公告)日：2014-12-24

申请号：EP13172301.7

申请日：2013-06-17

申请人： Airbus Operations GmbH

发明人： Lohmann, Ali ,  Köhler, André ,  Völker, Johannes ,  Grambole, Christian ,  Ulbrich, Matthias ,  Pump, Jörg ,  Hager, Sönke

IPC分类号： B64D9/00

CPC分类号： B64D9/00 ,  B60P7/0892

摘要： The invention relates to a cargo handling system (1) for loading and securing one or more freight containers (C) in a cargo hold (H) of an aircraft (A). The system (1) comprises: a plurality of bracket members (2) configured to be secured to a base or floor of the cargo hold (H); and a plurality of elongate guide members (5), each of which is mounted on and interconnects a number of the bracket members (2) arranged in a row; wherein each guide member (5) forms a restraint or a stop against lateral movement of a freight container (C) loaded in the cargo hold (H). The bracket members (2) include at least one fastening portion (3) configured for tool-less fast-release engagement and locking with a seat track profile in the base or floor (F) of the cargo hold (H). Furthermore, the bracket members (2) typically extend transversely inwards or inboard of the elongate guide members (5).

摘要翻译： 本发明涉及一种用于装载和固定飞机（A）的货舱（H）中的一个或多个货物集装箱（C）的货物处理系统（1）。 系统（1）包括：多个支架构件（2），其构造成固定到货舱（H）的底座或底板上; 以及多个细长导向构件（5），每个细长导向构件（5）安装在并排布置成一排的多个支架构件（2）上并互连; 其中每个引导构件（5）形成限制或停止以抵抗装在货舱（H）中的货物集装箱（C）的横向移动。 托架构件（2）包括至少一个紧固部分（3），其构造成用于无需工具的快速释放接合并且与货舱（H）的基座或地板（F）中的座椅轨道轮廓锁定。 此外，支架构件（2）通常横向地延伸到细长导向构件（5）的内侧或内侧。

公开(公告)号：EP2759718A1

公开(公告)日：2014-07-30

申请号：EP14151963.7

申请日：2014-01-21

申请人： Airbus Operations GmbH

发明人： Esser, Markus ,  Lohmann, Ali ,  Pump, Jörg ,  Hager, Sönke ,  Völker, Johannes

IPC分类号： F16B21/02 ,  B64C1/20 ,  B64D9/00

CPC分类号： B64C1/20 ,  B60R11/00 ,  B64D9/00 ,  B64D9/003 ,  B64D2009/006 ,  B64G1/22 ,  B65G13/00 ,  B65G13/11 ,  B65G21/02 ,  B65G21/06 ,  B65G39/12 ,  F16B21/02

摘要： The invention relates to a fastening device (6) for releasably fastening a mechanism (2) in the region of a floor (3) of an aircraft or spacecraft. The fastening device (6) comprises a base component (7) and a latch component (8). The base component (7) is provided so as to be rigidly coupled to a floor component (5) which is formed for introducing a load into the floor. The latch component (8) comprises at least one holding portion (13) comprising a latch-component-side holding face (15) and is coupled to the base component (7) in such a way that the latch component (8) is movable between an unlocked position (E) and a locked position (V) with respect to the base component (7). The latch component (8) is formed in such a way that, when the mechanism (2) is positioned in part in a predefined mounting position on the floor component (5) and/or on the base component (7), the holding portion (13) of the latch component (8) engages around a fastening portion (16), which is formed on the mechanism (2) and equipped with at least one mechanism-side holding face (24), in the region of the mechanism-side holding face (24) during the passage of the latch component (8) into the locked position (V) in such a way that the latch-component-side holding face (15) faces the mechanism-side holding face (24). The latch-component-side holding face (15) is formed in such a way that during passage of the latch component (8) from the locked position (V) into the unlocked position (E) a gap between the latch-component-side holding face (15) and the mechanism-side holding face (24) continuously widens. The invention further relates to an arrangement (1) for a cargo loading system.