Aeronautics and astronautics – Aircraft structure – Details
Patent
1986-09-30
1988-04-26
Barefoot, Galen
Aeronautics and astronautics
Aircraft structure
Details
49 34, 49465, 160 88, 52507, B64C 114
Patent
active
047399554
ABSTRACT:
A mounting assembly for the insulation and interior panels of an aircraft. The mounting assembly includes an upper retainer for securing the upper edge of the cabin panel to the aircraft, and a lower releasable latch assembly which connects the lower end of the cabin panel to the aircraft. The curved aircraft panels, which are made of a resilient bendable material, are installed so that the panels are further resiliently bent into a tensioned state which acts to resiliently engage the panels between the upper retainer and the lower latch assembly. A shock absorber and insulation retainer is attached to the aircraft between the aircraft frame and the cabin panel to prevent vibration of the cabin panel and to secure the insulation between the aircraft panel and the aircraft frame.
REFERENCES:
patent: 1637018 (1927-07-01), Bayley
patent: 1921051 (1933-08-01), Trauf
patent: 2009132 (1935-07-01), Gehris
patent: 2256961 (1941-09-01), Pearson et al.
patent: 2263919 (1941-11-01), Darragh, Jr.
patent: 2476451 (1949-07-01), Murphy et al.
patent: 3325951 (1967-06-01), Johnson
patent: 4637188 (1987-01-01), Crothers
Aquino Roberto
Kirk Anthony I. C.
Starling John C.
Webb Thomas E. A. H.
Barefoot Galen
The Boeing Company
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