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公开(公告)号：US11945603B2
公开(公告)日：2024-04-02
申请号：US17733660
申请日：2022-04-29
Applicant: Airbus Operations GmbH
Inventor： Ralf Schliwa , Gunda Hülsen , Uwe Panzram , Hermann Benthien , Lars Uwe Hansen , Paul Adrian Wichtmann , Dirk Meiranke , Thomas Grabow
CPC classification number: B64D9/00 , B64C1/20 , B64F1/322 , B64D2009/006
Abstract: A load carrier for an aircraft cargo hold includes a bottom element with a support surface, the load carrier being movable over a floor surface in a floor plane while the support surface faces the floor surface, the bottom element having a base surface. The support surface has rolling elements rotatable about a rotation axis oriented where a parallel to the axis runs parallel to the floor plane, and the rolling elements being retained on the bottom element where the rotation axis of each of the rolling elements can be rotated about a vertical axis running perpendicularly to the floor plane. A load carrier can include a bottom element, the support surface of which has outlet openings, through which air can exit from the support surface to form an air cushion under the support surface. A load carrier can include a bottom element the support surface of which has slider elements.
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公开(公告)号：US20130166063A1
公开(公告)日：2013-06-27
申请号：US13771724
申请日：2013-02-20
Applicant: AIRBUS OPERATIONS GMBH
Inventor： Uwe Panzram , Volker Hasbach
IPC: B65G67/00
CPC classification number: B64D9/00 , B64D9/003 , B64D2009/006
Abstract: Systems and methods are provided for the loading and unloading of cargo in transport means. In one example, a cargo loading system having a fully automated conveyor system and a fully automated bolt system for locking the cargo unit is provided. Manual interventions of the loading personnel in the cargo space may not be necessary.
Abstract translation: 提供系统和方法，用于在运输工具中装载和卸载货物。 在一个示例中，提供了具有全自动输送系统和用于锁定货物单元的全自动螺栓系统的货物装载系统。 装卸人员在货物处所的手动干预可能不是必需的。
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公开(公告)号：US20220332418A1
公开(公告)日：2022-10-20
申请号：US17733660
申请日：2022-04-29
Applicant: Airbus Operations GmbH
Inventor： Ralf Schliwa , Gunda Hülsen , Uwe Panzram , Hermann Benthien , Lars Uwe Hansen , Paul Adrian Wichtmann , Dirk Meiranke , Thomas Grabow
Abstract: A load carrier for an aircraft cargo hold includes a bottom element with a support surface, the load carrier being movable over a floor surface in a floor plane while the support surface faces the floor surface, the bottom element having a base surface. The support surface has rolling elements rotatable about a rotation axis oriented where a parallel to the axis runs parallel to the floor plane, and the rolling elements being retained on the bottom element where the rotation axis of each of the rolling elements can be rotated about a vertical axis running perpendicularly to the floor plane. A load carrier can include a bottom element, the support surface of which has outlet openings, through which air can exit from the support surface to form an air cushion under the support surface. A load carrier can include a bottom element the support surface of which has slider elements.
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公开(公告)号：US08788085B2
公开(公告)日：2014-07-22
申请号：US13771724
申请日：2013-02-20
Applicant: Airbus Operations GmbH
Inventor： Uwe Panzram , Volker Hasbach
IPC: G06F7/00
CPC classification number: B64D9/00 , B64D9/003 , B64D2009/006
Abstract: Systems and methods are provided for the loading and unloading of cargo in transport means. In one example, a cargo loading system having a fully automated conveyor system and a fully automated bolt system for locking the cargo unit is provided. Manual interventions of the loading personnel in the cargo space may not be necessary.
Abstract translation: 提供系统和方法，用于在运输工具中装载和卸载货物。 在一个示例中，提供了具有全自动输送系统和用于锁定货物单元的全自动螺栓系统的货物装载系统。 装卸人员在货物处所的手动干预可能不是必需的。
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5.发明授权公开(公告)号：US11807393B2
公开(公告)日：2023-11-07
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
CPC classification number: B64D9/003 , B64C1/20 , B64D2009/006
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.
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Patent Agency Ranking
公开(公告)号：US11807392B2
公开(公告)日：2023-11-07
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
CPC classification number: B64D9/003 , B64C1/20 , B64D2009/006
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.
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公开(公告)号：US20210354827A1
公开(公告)日：2021-11-18
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
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.
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8.发明申请公开(公告)号：US20190092446A1
公开(公告)日：2019-03-28
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
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.
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公开(公告)号：US20180251305A1
公开(公告)日：2018-09-06
申请号：US15906826
申请日：2018-02-27
Applicant: Airbus Operations GmbH
Inventor： Sascha Nowarre , Ralph Knüppel , Uwe Panzram , Stephan Kahle , Thomas Wellbrock
CPC classification number: B65G13/11 , B64C1/20 , B64D9/00 , B64D2009/006 , B65G1/02 , B65G1/023 , B65G39/12
Abstract: A roller mat includes roller elements, an upper shell which is provided with openings for receiving the roller elements, a lower shell and a foam element which is arranged between the upper shell and the lower shell. The foam element is provided with recesses which are for receiving the roller elements and which are aligned with the openings constructed in the upper shell in the region of an upper side facing the upper shell.
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公开(公告)号：US09676567B2
公开(公告)日：2017-06-13
申请号：US14303935
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
CPC classification number: B65G51/03 , B64C1/20 , B64D9/00 , B65D88/127 , B65D88/14 , B65D88/546 , B65D2590/0083
Abstract: A cargo compartment configured to be installed in an aircraft and to accommodate a plurality of cargo receiving devices is provided. The cargo compartment surrounds a compartment interior space, and includes a floor structure arrangement having a floor surface facing the compartment interior space and configured to support cargo receiving devices loaded into the cargo compartment. The cargo compartment includes two opposite side walls extending laterally of the floor structure arrangement away from the floor surface, and the side walls include an entrance opening for access to the compartment interior space. The floor structure arrangement also includes an air cushion device having a plurality of cushion nozzles distributed in the floor surface, and the cushion nozzles are configured to blow air up from the floor surface in a direction perpendicular to the floor surface.
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