Honda Motor Co., Ltd.
Variable stator vane structure of axial compressor

Last updated:

Abstract:

In an axial compressor including a row of rotor blades (70) provided on a rotational shaft (20) around a central axial line of the rotational shaft at a prescribed pitch, and a row of stator vanes (40) provided on a casing around the central axial line at a prescribed pitch so as to adjoin the row of rotor blades on an upstream or downstream side thereof, the rotor blades each extend along a radial line (R) emanating from the central axial line, and the stator vanes each extend along a slanted line (I) that is slanted with respect to a corresponding radial line in a circumferential direction.

Status:
Grant
Type:

Utility

Filling date:

18 Mar 2019

Issue date:

19 Jan 2021