INTERNAL STRUCTURE VISUALIZATION METHOD AND AIRCRAFT REPAIR METHOD
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United States of America Patent
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Issued Date -
Sep 8, 2016
app pub date -
Feb 11, 2016
filing date -
Mar 3, 2015
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Abstract
An object of the present invention is to visualize an internal structural members, which are covered with a skin and therefore unrecognizable to the naked eye, from the outside of the skin. There is provided an internal structure visualization method applied to a main wing of an aircraft, which includes a skin with a front surface and a back surface and structural members supporting the skin from the back surface side, to display, when necessary, a trace map composed of lines extending along projection regions of the structural members, wherein functional lines, which are a developing element of the trace map, are provided along the projection regions of the front surface, and the trace map is displayed by performing a predetermined process on a predetermined region of the front surface where the functional lines are provided.
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