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 代理人
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