The Boeing Company

Craig Alan Vyeson

Kurt Randall Kraft

Brad Alan Kauffman

Robin William Stebbins

Kurt Poechlauer

Quentin Theodor Pietersen

Darryl Hitoshi Nakamura

Roger Probert-Baker

A computer implemented method, apparatus, and computer usable program code for a mobile tail support control system. An apparatus comprises a data processing system, an output device, a set of load sensors, a set of position sensors, and a computer program product executing on the data processing system. The output device is capable of generating signals for managing movement of a mobile tail support apparatus. The set of load sensors may be coupled to the data processing system and may be capable of detecting loads associated with a swing tail cargo door. The set of position sensors are coupled to the data processing system and detect a position of the mobile tail support apparatus relative to the swing tail cargo door. The computer program product may receive information from the set of load sensors and the set of position sensors and generate signals to manage the mobile tail support apparatus.

Method and apparatus for moving a swing tail cargo door on an aircraft

A method and apparatus for a mobile tail support vehicle moving a swing tail cargo door of a swing tail aircraft. A mobile tail support apparatus is engaged to the swing tail cargo door on the swing tail aircraft. The swing tail cargo door is moved from a first position to a second position using the mobile tail support apparatus. Vertical reaction occurs to vertical loads on the swing tail cargo door during movement of the swing tail aircraft by the mobile tail support apparatus. Loads on a hinge and/or swing tail cargo door are reduced during the movement of the swing tail cargo door using the mobile tail support apparatus.

Compliance mechanism

A method and apparatus for aligning a swing tail cargo door. An alignment system comprises an alignment ramp, a set of pull-in hook mechanisms, and a set of lock trains. The alignment ramp may be configured for initial alignment between a swing tail cargo door and an aircraft fuselage during closing of the swing tail cargo door. The set of pull-in hook mechanisms may be disposed along an interface between the swing tail cargo door and the aircraft fuselage and may be capable of a final alignment between the swing tail cargo door and the aircraft fuselage during the closing of the swing tail cargo door. The set of lock trains may be disposed along the interface and may be capable of locking a plurality of latch actuators in the latched position.

Method and apparatus for closing a swing tail on an aircraft

Growing community of inventors

Everett, WA, United States of America

Craig Alan Vyeson