发明名称 Method of rapid hole transfer to replacement parts
摘要 A method of replacing an existing part or parts on a structure such as an aircraft. The structure is inducted for modification. An existing part is removed and a new part is temporarily installed. Hole locations are digitally transferred to the new part, e.g., photographically captured in a three-dimensional coordinate measurement system, converted to targets printable in a laser projection system. Targets are laser projected or printed on the replacement part. Holes are drilled at each printed target. The holes drilled at printed targets match hole locations on the existing part. Then, the new/replacement part is permanently attached to the structure.
申请公布号 US7668616(B2) 申请公布日期 2010.02.23
申请号 US20070752353 申请日期 2007.05.23
申请人 THE BOEING COMPANY 发明人 PIASSE MICHAEL L.;FARNIOK CRAIG M.;STECKEL RICHARD J.;NOBLES ORVAL M.
分类号 G06F19/00;B23P19/04;B64F5/00 主分类号 G06F19/00
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