发明名称 |
INTERNAL STRUCTURE VISUALIZATION METHOD AND AIRCRAFT REPAIR METHOD |
摘要 |
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. |
申请公布号 |
US2016257430(A1) |
申请公布日期 |
2016.09.08 |
申请号 |
US201615041539 |
申请日期 |
2016.02.11 |
申请人 |
MITSUBISHI AIRCRAFT CORPORATION |
发明人 |
Hayashi Shotaro;Nagase Ryuichi;Suhara Masayoshi;Okamoto Hiromu;Arikawa Kiwamu;Ishida Morimasa |
分类号 |
B64F5/00;G03B21/00 |
主分类号 |
B64F5/00 |
代理机构 |
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代理人 |
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主权项 |
1. An internal structure visualization method applied to a structure, which includes a skin with a front surface and a back surface and structural members supporting the skin from the back surface side, to visualize, when necessary, a trace map composed of lines extending along projection regions of the structural members, wherein
a developing element of the trace map is 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 developing element is provided. |
地址 |
Aichi JP |