Airbus Operations Gmbh

Hensoldt Sensors Gmbh

Oliver Nuessen

Dennis Fischer

Uwe Panzram

Dirk Meiranke

Sascha Nowarre

Matthias Horst

Martin Guse

Peter Sander

Peter Leopold Pirklbauer

Sven Scherenberger

Volker Hasbach

Hubert Piontek

Johannes Petz

Daniel Preis

Cosima Eggers

A dynamically controlled cargo loading system for an aircraft includes electrical cargo conveying devices for conveying cargo items on a cargo loading deck; speed sensors, which are configured to capture current conveying speeds of the cargo conveying devices and/or the conveyed cargo items; electrical measuring devices, which are configured to capture current electrical parameters of the cargo conveying devices; and a control device which is configured to control the cargo conveying devices depending on the captured current conveying speeds and/or the recoded current electrical parameters such that at least one of the following variables is optimized: the electrical power consumption of the cargo conveying devices, the mechanical wear of the cargo conveying devices, the mechanical load action on the cargo items, the conveying time of the cargo items and the noise generation during the conveying of the cargo items.

Dynamically controlled cargo loading system for an aircraft

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.

Latches for cargo hold loading and storage system and associated methods

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.

Baseplates for keyed installation of components in a cargo hold and loading and storage system and associated methods

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.

Bi-stable power drive unit (PDU) for a cargo hold loading and storage system and associated methods

A disruption device for fixing to an aerial vehicle. The disruption device is adapted to disrupt at least one radio path between at least one receiving unit of an unmanned flying body and at least one transmitting unit provided for controlling the flight path of the unmanned flying body. An aerial vehicle having the disruption device is further provided.

Drone defense system

Disclosed here is a cargo drive unit for a cargo hold of an aircraft. The cargo drive unit includes at least one driven power transmission element, which is configured to transmit drive forces to a load arranged in the cargo hold, in order to move the load inside the cargo hold. The cargo drive unit also includes a sensor unit configured to acquire at least one movement parameter of the load. The cargo drive unit also includes a control unit configured to control the power transmission element according to the acquired movement parameter. Also disclosed here is a cargo hold that includes such a cargo drive unit, and a related method for operating such a cargo hold.

Cargo drive unit with acquisition of a load movement

There is disclosed inter alia a transport goods monitoring device having a cover which is configured to cover transport goods received by a transport goods receptacle, the cover comprising a conductor arrangement, the conductor arrangement being in a first state when the cover is intact, the conductor arrangement being transformable from the first state into a second state by damage of the cover and the conductor arrangement being connectable to a detector which is configured to detect the existence of the second state. Furthermore, there is disclosed an arrangement comprising a transport goods receptacle which is configured to receive transport goods, and such a transport goods monitoring device, the cover of the transport goods monitoring device covering the transport goods receptacle and optionally transport goods arranged thereon. Also disclosed is the use of such a transport goods monitoring device for safeguarding transport goods received by a transport goods receptacle.

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Hamburg, Germany

Oliver Nuessen