Aircraft interior shell
Number of patents in Portfolio can not be more than 2000
United States of America Patent
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-
Apr 13, 1993
Issued Date -
N/A
app pub date -
Nov 15, 1991
filing date -
Nov 15, 1991
priority date (Note) -
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status (Latency Note)
Importance
Abstract
An aircraft interior skeleton spaced apart from the aircraft frame is formed from multiple spaced apart upright U-shaped ribs attached to horizontal intercostal U-shaped members conforming to the aircraft frame members, but not contacting such frame members. Multiple interior honeycomb side panels and overhead panels are hinged from the interior skeleton and interlocked with adjacent panels. An overhead connecting member is attached to a top end of each rib and a dampening device connects the bottom end of each rib to an aircraft frame member. Adjustable cable connectors position the interior skeleton within the aircraft by connecting the horizontal intercostal members to the aircraft frame members.
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