发明名称 METHOD OF MEASURING SHAPE DEFECT OF AIRCRAFT STRUCTURAL PANEL AND SYSTEM FOR IMPLEMENTING SAID METHOD
摘要 FIELD: physics. ^ SUBSTANCE: method of measuring the shape defect on an aircraft structural panel involves the following operations: projection of a target drawing on the location of the defect on the panel, where the said drawing is a set of black and white spots of different sizes lying arbitrarily next to each other; obtaining at least two images of this projected target drawing; processing these two images through stereoscopic correlation to obtain measurement values of the geometry of the defect. The disclosed system which enables implementation of this method includes: a projecting device configured to project the target drawing on the location of the defect on the panel, where the said drawing is a set of black and white spots of different sizes lying arbitrarily next to each other; at least two detachable devices, each of which is configured to obtain the image of the target drawing. The system also includes apparatus for processing these two images of the target drawing. ^ EFFECT: avoiding deposition of the drawing onto the structural panel of the aircraft. ^ 16 cl, 3 dwg
申请公布号 RU2414683(C2) 申请公布日期 2011.03.20
申请号 RU20080106924 申请日期 2006.07.24
申请人 EHRBJUS FRANS 发明人 FURN'E NIKOLJA
分类号 G01B11/25 主分类号 G01B11/25
代理机构 代理人
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