Decompression panel for aircraft partition

Details Decompression panel for aircraft partition Decompression panel for aircraft partition

1988-05-09

1990-02-13

Barefoot, Galen

Aeronautics and astronautics

Aircraft structure

Passenger or crew accommodation

2441294, 292 19, 292259R, 52 1, 52 98, 137 70, 137 681, B64C 114

Patent

active

048999601

ABSTRACT:
Decompression in a partition separating passenger from cargo compartments in aircraft, there being a particular opening in the partition, receiving a decompression blowout/in panel; a frame circumscribes the decompression panel and has an outer contour inserted into the panel opening, one side of the frame is provided with a flange, being sealed as against the decompression panel as well as against the partitions adjacent the opening, the other side of the frame is provided with a plurality of T-shaped holding springs engaging the partition as well as the decompression panel; each of the springs is provided with predetermined fracture points.

REFERENCES:
patent: 2209399 (1940-07-01), Hall
patent: 2355485 (1944-08-01), Tinnerman
patent: 3571977 (1971-03-01), Abeel
patent: 3864881 (1975-02-01), Wolf
patent: 3972442 (1976-08-01), Malcolm
patent: 4027436 (1977-06-01), Daly
patent: 4553559 (1985-11-01), Short, III
patent: 4656793 (1987-04-01), Fons
patent: 4703908 (1987-11-01), Correge et al.

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