Joining structure for interior panel for aircraft
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United States of America Patent
Stats
-
Sep 13, 2016
Grant Date -
Nov 19, 2015
app pub date -
Dec 18, 2013
filing date -
Dec 19, 2012
priority date (Note) -
In Force
status (Latency Note)
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Abstract
A joining structure for an interior panel for an aircraft includes two interior panels, each provided with a corner portion formed on an internal-side surface plate by an edge of an end portion of an external-side surface plate and an edge of an end portion of an internal-side surface plate being attached, the corner portion extending in the direction the edges extend. Strip-shaped connection pieces are provided at the corner portion and are formed across an entire length of the corner portion by a portion, with gaps between the strip-shaped connection pieces. The two interior panels are joined when brought together, with the connection pieces of the two interior panels passing through the gaps between the connection pieces of the other interior panels and being adhered to the external-side surface plate of the other interior panels by an adhesive.
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