Aecc Commercial Aircraft Engine Co., Ltd.

Aecc Shanghai Commercial Aircraft Engine Manufacturing Co., Ltd.

Xiaoshi Zhang

Fan Wu

Chuanjun Cao

Zeyong Yin

Jibao Li

Jinchun Wang

Yixuan Jiang

Zhilong Zhai

A method includes simplifying flowing of airflow at root of a rotor blade into flowing of free jet, and determining an airflow expansion angle according to Mach number of incoming flow at root of a stator vane; calculating a radial height difference between a first end point on a leading edge of a stator platform and a trailing edge of an adjacent rotor platform by using an axial distance thereof, the angle and a deviation coefficient; determining position of the first end point with radial height difference; determining intersection point of the leading edge and the stator platform as position of a second end point on the leading edge; and determining a profile line between the points by bridging spline curves, so that the tail end thereof is tangent to the intersection line, and the starting end thereof is kept on same plane as side wall of the leading edge.

Method for configuring a leading edge of a compressor stator platform and the corresponding stator platform

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Shanghai, China

Xiaoshi Zhang