Axial flow turbine mechanical blade parameterization method applicable to bending, twisting and sweeping
A turbomachinery, parametric technology, applied in the direction of mechanical equipment, blade support components, engine components, etc.
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[0074] The present invention will be further described in detail below in conjunction with the accompanying drawings. However, it should not be understood that the scope of the above-mentioned subject matter of the present invention is limited only to the following content. Without departing from the above idea of the present invention, various replacements or changes made according to common technical knowledge and customary means in this field shall be included in the scope of the present invention.
[0075] Such as figure 1 As shown, the key defining parameters of the airfoil section for a certain blade height include: leading edge radius R le , trailing edge radius R te , Axial chord length C x , tangential chord length C t , Inlet geometry angle β in , exit geometric angle β out , leading edge half-wedge angle ε in , trailing edge semi-wedge angle ε out . The axial chord length C of the blade x refers to the lateral distance between the front and rear frontal ...
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