The Boeing Company

Herbert E Hamilton

Thomas H Shorey

Tom M Jensen

Michael E Abdelmaseh

An automatically retractable restraint assembly for vertically restraining a body by engagement with its side. The centerline restraint (10) includes a pair of normally upright positioned inside heads (20), each head having an outwardly extending toggle (76) for engaging the side of a cargo body (14). The inside heads are automatically retractable into the frame (24) upon engagement by the cargo body after the preceding engagement of either of a pair of release wings (30). The inside heads are also spring loaded outwardly along the longitudinal centerline of the centerline restraint to maintain contact between the toggle and the cargo body should it attempt to move out of engagement. A pair of normally upright positioned and automatically retractable outside heads (22) are included to engage a cargo body of lesser widthwise dimension.

Automatically retractable centerline restraint

An elevator system for use in a wide-body commercial aircraft having multiple levels within the aircraft provides an elevator shaft that extends through at least two of the levels of the aircraft. The elevator shaft communicates with an opening in the hull of the aircraft. An elevator car is mounted within the shaft and controls and a drive unit are associated with the car to move it within the shaft and also out through the opening in the hull to provide access to and from the aircraft. At least a portion of the car remains in the shaft at all times to provide some lateral stability to the car.

Personnel elevator for commercial aircraft

Disclosed is an aircraft cargo loader that is folded for stowage against the interior surface of an aircraft cargo door and is extended between the sill of the cargo door and the surface of the ground for loading and unloading baggage and other relatively small cargo items. The cargo loader includes an endless conveyor belt, with the cargo loader and the conveyor belt being configured so that the conveyor belt remains under relatively constant tension when cargo loaded is extended and when the cargo loader is folded for stowage. An L-shaped deployment track is attached to the upper end of the cargo loader and fastened between the cargo loader deck and ceiling when the cargo loader is deployed. The L-shaped deployment track facilitates cargo loader deployment and retraction in which the folded cargo loader is swung through the cargo opening while extending from the vertical leg of the deployment track; rotated to extend from the horizontal leg of the deployment track; and, while extending from the horizontal leg, folded or unfolded. Both power and manual drives are included for moving the cargo loader along the L-shaped deployment track; for folding and unfolding the cargo loader; for locking the cargo loader in the extended, deployed position; and for extending and retracting a ground support assembly that supports the lower end of the cargo loader above the surface of the ground.

Growing community of inventors

Edmonds, WA, United States of America

Herbert E Hamilton