公开(公告)号：US09452901B2

公开(公告)日：2016-09-27

申请号：US14303979

申请日：2014-06-13

Applicant: Airbus Operations GmbH ,  Airbus S.A.S.

Inventor： Uwe Panzram ,  Joerg Klockgether ,  Philippe Le Bigot ,  Peter Esteie ,  Netra Gowda

IPC: B65G67/00 ,  B64D9/00 ,  B64C1/20

CPC classification number: B65G67/00 ,  B64C1/20 ,  B64D9/00 ,  B64D2009/006

Abstract: A system for loading and unloading a cargo compartment of a vehicle, such as an aircraft, with a cargo receiving device is provided. The system includes a cargo receiving device including a base structure arrangement having a horizontal lower contact surface, and a locking mechanism configured to engage one or more corresponding holding members provided in a cargo compartment of a vehicle. The system also includes a transport device including a horizontal upper contact surface configured to be disposed in abutting contact to said lower contact surface, a drive unit configured to initiate horizontal movement of the transport device, a lift unit configured to initiate vertical movement of the upper contact surface, and an actuating unit configured to actuate the locking mechanism of the cargo receiving device.

Abstract translation: 提供了一种用于装载和卸载诸如飞机的车辆的货舱与货物接收装置的系统。 该系统包括货物接收装置，该货物接收装置包括具有水平下接触表面的基部结构装置，以及锁定机构，其构造成接合设置在车辆的货舱中的一个或多个对应的保持构件。 该系统还包括一个输送装置，该输送装置包括构造成与所述下接触表面邻接接触的水平上接触表面;驱动单元，构造成启动输送装置的水平运动;升降单元，其构造成启动上部 接触表面以及构造成致动货物接收装置的锁定机构的致动单元。

公开(公告)号：US12049327B2

公开(公告)日：2024-07-30

申请号：US17361934

申请日：2021-06-29

Applicant: Airbus Operations GmbH

Inventor： Oliver Nuessen ,  Martin Guse ,  Dirk Meiranke ,  Sascha Nowarre ,  Dennis Fischer ,  Uwe Panzram ,  Matthias Horst

IPC: B64D9/00 ,  B64C1/20

CPC classification number: B64D9/003 ,  B64C1/20 ,  B64D2009/006

Abstract: In an aircraft, latches are used to secure cargo within the cargo hold of the aircraft. Such latches include a base plate configured for rigid attachment to a surface of the cargo hold, a latch head attached to the base plate and configured to prevent a movement of at least one cargo unit in a Y-direction and a Z-direction and to allow a movement of the at least one cargo unit in an X-direction, and a roller assembly attached to the base plate, opposite the latch head, and comprising at least one roller, the roller being configured to provide a vertical support to the at least one cargo unit in the Z-direction while allowing the movement of the at least one cargo unit in the X-direction.

公开(公告)号：US11459082B2

公开(公告)日：2022-10-04

申请号：US16146231

申请日：2018-09-28

Applicant: Airbus Operations GmbH

Inventor： Peter Leopold Pirklbauer ,  Peter Sander ,  Uwe Panzram ,  Jan Reh ,  Michael Sillus

IPC: B64C1/22 ,  B64D9/00

Abstract: A cargo hold comprises at least one luggage holder having at least one luggage compartment, wherein, when the hatch is in the closed state, the luggage holder is arranged in the cargo hold, and wherein, when the hatch is in the opened state, the luggage holder can be brought out of the cargo hold and can be introduced therein again by means of a guide mechanism in such a manner that the luggage holder, when it is brought out of the cargo hold, is arranged substantially radially to the substantially elliptical cross section of the fuselage.

公开(公告)号：US20210394905A1

公开(公告)日：2021-12-23

申请号：US17361999

申请日：2021-06-29

Applicant: Airbus Operations GmbH

Inventor： Oliver Nuessen ,  Martin Guse ,  Dirk Meiranke ,  Sascha Nowarre ,  Dennis Fischer ,  Uwe Panzram ,  Matthias Horst

IPC: B64D9/00 ,  B64C1/20

Abstract: A system for ensuring proper installation of components of a cargo management system within a cargo hold has cleats rigidly attached to a floor of the cargo hold, a first subset of the cleats having insets of a first shape, a second subset of cleats having insets of a second shape, keys and rotatable fasteners attached to the components of the cargo management system, a first subset of the keys having the first shape and a second subset of the keys having the second shape. The first subset of keys can only engage with the first subset of cleats and the second subset of keys can only engage with the second subset of cleats and the rotatable fasteners utilize a rotary movement to secure the components of the cargo management system to a respective cleat, against which the rotary fastener is engaged.

公开(公告)号：US20210354828A1

公开(公告)日：2021-11-18

申请号：US17362052

申请日：2021-06-29

Applicant: Airbus Operations GmbH

Inventor： Oliver Nuessen ,  Martin Guse ,  Dirk Meiranke ,  Sascha Nowarre ,  Dennis Fischer ,  Uwe Panzram ,  Matthias Horst

IPC: B64D9/00 ,  B64C1/20

Abstract: In an aircraft, bi-stable power drive units (PDUs) move and secure cargo within an aircraft cargo hold. Such a PDU includes a frame, by which the PDU is rigidly attached to the cargo hold floor; a body pivotably attached, via a hinge, at a first end of the frame at least one drive roller attached at a second end of the body; and an actuator attached to the body and which causes a pivoting angular movement of the body, relative to the frame, about the hinge. The actuator maintains an angular position of the body relative to the frame even upon a loss of power to the PDU. The body is movable between and including a retracted position and a deployed position. A cargo management system includes a plurality of such PDUs, at least one having a controlled area network (CAN) bus interface to control and communicate with a controller.

公开(公告)号：US09340286B2

公开(公告)日：2016-05-17

申请号：US14516788

申请日：2014-10-17

Applicant: Airbus Operations GmbH

Inventor： Uwe Panzram ,  Sascha Nowarre ,  Hans-Joachim Schoen ,  Claudio Uriarte ,  Patrick Dittmer ,  Thies Andreas Ernst-Friedrich Beinke

IPC: B64D9/00 ,  B64C1/20

CPC classification number: B64D9/00 ,  B64C1/20 ,  B64D2009/006 ,  Y02T50/46

Abstract: An automated transport device for moving a cargo unit within an aircraft cargo compartment is provided. The transport device comprises a base body and shifting means, wherein the base body is to carry the cargo unit. The shifting means is to generate a movement of the base body along a floor of the cargo compartment perpendicular to the longitudinal axis of the aircraft and, after that, along the longitudinal axis of the aircraft without rotation of the base body.

Abstract translation: 提供一种用于在货物舱内移动货物单元的自动运送装置。 输送装置包括基体和移动装置，其中基体承载货物单元。 移动装置是沿垂直于飞行器的纵向轴线的货物舱底板产生基体的运动，此后沿着飞行器的纵轴不产生基体旋转。