Abstract: An arrangement for conveying material to be conveyed along a conveying plane, in particular for freight-loading systems in freight compartments, preferably of aircraft is disclosed. The arrangement provides that driving material to be conveyed along a conveying plane, with which safe, reliable transport of the material to be conveyed is ensured with low wear of the conveying roller under widely varying operating conditions. This is achieved in that, in a drive unit, the conveying roller is connected to a first drive and an associated first activating unit for producing a requisite traction force for moving the material to be conveyed along the conveying plane.

Abstract: An airborne pneumatic launch tube ejection system to described for launching an aerospace vehicle/payload into orbit. The system can be installed in a jet transport aircraft without requiring structural modifications.

Abstract: A roller drive unit for use in the transportation of freight containers in the hold of an aircraft. The unit comprises a drive roller, which can be retracted and which can be raised into an operating position by an electric motor, for engagement with a freight container to be transported. Sensors are distributed in a ring around the drive roller so as to be able to monitor the direction of movement of a freight container approaching the roller drive unit. A controller is connected to the sensors and to the electric motor in order that the drive roller can be raised out of its lower, retracted position into an upper, operating position or conversely, according to the signals received by the controller means from the sensors.

Abstract: A basket for supporting equipment between a pair of laterally spaced-apart parallel overhead cables. The basket is provided in the form of a top open container insertable between the overhead cables. A carrying member engageable with a helicopter arm is provided for allowing the basket to be selectively transported between and away from the overhead cables. A pair of wing-like members extend laterally outwardly from opposed side walls of the container for resting on the overhead cables once the basket has been lowered to a suspended position between the overhead cables.

Abstract: A method for the exact setting down or taking up of cargo from aircraft is disclosed. When setting down persons or cargo from aircraft which has not landed, the problem arises of an exact setting down not being possible, or only with great difficulty, in particular under adverse weather conditions. The invention provides a method whereby exact and even “spot-on” setting down or taking up of a load is made possible, even if the ambient conditions do not allow the aircraft to be kept steady. With the spatial framework of ropes biased by the aircraft, the position of the load in space is clearly fixed. The load can thus be exactly lowered down to the ground or taken up from the ground, without it being necessary for the aircraft to be still. Here, the aircraft itself is located at an appropriately selected distance above the load. The invention can also be applied to transportation by airships to construction sites, to catastrophe regions, etc.

Abstract: A covering plate (5), for flooring in conveyances such as a railway car, is provided with a securing track (11) for securing seats, etc. The covering plate (5) is formed by a sandwich structure having a central core (24) arranged between an outer plate (25), which extends across the entire size of the covering plate, and second outer plates (26). The securing track (11) is formed in a profile (27) embedded in the sandwich structure so that a securing track (11) extends at a right angle to lateral edges (14) of the covering plate (5). As either end of the profile is provided with tracks (29) for receiving tight-fitting pins (30), a floor structure can be mounted easily and rapidly.

Abstract: An airframe apparatus for attaching and selectively releasing multiple payloads suspended from an aircraft. The airframe apparatus includes a collapsible loading frame that is configured to have a stabilized open position and a collapsed closed position. The loading frame is constructed from a plurality of vertical struts and horizontal struts that are hingedly interconnected at corner assemblies to allow the loading frame to be collapsed. A payload hook is connected to each of the corner assemblies by a universal joint. A plurality of legs are rotatably attached to the loading frame and can be extended below the loading frame to support the payload hooks off the ground during landing of the airframe apparatus. Shock absorbing devices are operatively attached to the legs to absorb the impact of the loading frame against the ground during landing. The airframe apparatus is used as part of a cargo management system for transporting multiple payloads suspended from an aircraft.