A method for measuring the profile of an aeroengine blade
A technology of aero-engine, measurement method
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[0059] The present invention is a measurement method of aeroengine blade profile. First, the measurement method is based on a measurement system (disclosed prior art), see figure 1 As shown, the measurement system includes computer A, binocular industrial cameras (B1, B2), projector C, turntable D and positioning plane E. Among them, the computer A is used to control the action of the turntable D, the projector C and the binocular industrial camera (B1, B2), and the computer A is provided with a corresponding data processing program, and the measurement data collected by the scan is processed through the processing program. deal with. The projector C is used to project structured light onto the object to be measured on the turntable D-the blade F (that is, the blade of the aircraft engine). Binocular industrial cameras (B1, B2) are used to capture the deformed fringe pattern generated after the projector C is projected onto the measured object-the blade F. The positioning pla...
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