Aircraft cabin divider arrangement

Details Aircraft cabin divider arrangement Aircraft cabin divider arrangement

1996-07-18

1998-10-06

Barefoot, Galen L.

Aeronautics and astronautics

Aircraft structure

Fuselage and body construction

2441185, B64C 106

Patent

active

058165347

ABSTRACT:
An arrangement for dividing an aircraft cabin that extends perpendicular to the longitudinal direction of the cabin, includes a divider wall that is guided in a position adjustable manner in guide tracks that are arranged stationarily fixed along the aircraft cabin. The divider wall includes a plurality of individual divider elements. Each divider element is held slidably by corresponding support members in at least one guide track. Each guide track is arranged in the area of joints between cabin interior components. With this arrangement, running grooves, scratches, and lubricant smears on visible furnishings or fitting in the interior of the aircraft cabin can be avoided. The cost and effort for cleaning and maintaining the aircraft cabin are thus significantly reduced. The arrangement does not restrict the open or clear cross section of the cabin, particularly in the head room area, thereby reducing a source of danger to passengers.

REFERENCES:
patent: 2752864 (1956-07-01), Mcdougal, Sr. et al.
patent: 3712663 (1973-01-01), Laven
patent: 4121790 (1978-10-01), Graham
patent: 4185799 (1980-01-01), Richards, Jr.
patent: 4597549 (1986-07-01), Ryan
patent: 4639031 (1987-01-01), Truckenbrodt
patent: 4899962 (1990-02-01), Mueller

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