Aviation blade cross section molded line contour parameter evaluation method and system
An aviation blade and evaluation method technology, applied in character and pattern recognition, special data processing applications, instruments, etc., can solve the problems of torsion angle and offset evaluation, complex calculation, and numerous parameters, and achieve accurate and reliable evaluation
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[0052] In order to make the objects, technical solutions and advantages of the present invention, the present invention will be described in further detail below with reference to the accompanying drawings and examples. It is to be understood that the specific embodiments described herein are intended to explain the present invention and is not intended to limit the invention. Moreover, various embodiments of the invention described below involved the technical features as long as no conflict with one another can be configured in combination with each other.
[0053] like figure 1 , The present invention provides a method for evaluating a cross-sectional profile line of the vane aviation parameter profile, comprising the steps of:
[0054] (1) a contact type measurement method to obtain the coordinate measuring machine measuring point data of each section of the blade, the airfoil profile points set consisting of Q;
[0055] (2) using the ICP algorithm seeks to point relationship ...
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