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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
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.
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Patent Agency Ranking
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
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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3.发明申请公开(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
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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4.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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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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