Axial flow compressor

F - Mech Eng,Light,Heat,Weapons – 04 – D

Patent

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Details

F04D 19/00 (2006.01) F01D 5/14 (2006.01) F04D 21/00 (2006.01) F04D 29/52 (2006.01)

Patent

CA 2143879

An axial flow compressor is disclosed. The axial flow compressor has a casing defining a compression passage therein. The casing has an inner surface and a center axis extending along the elongated direction of the casing. A plurality of rotor blades fixed to a disk rotate in the compression passage around the center axis. Each of the rotor blades has a tip, and the tip defines a rotation area having a width extending in the direction along the center axis. A circular concavity is formed on the inner surface of the casing extending completely around the inner surface. The circular concavity has a continuous curved shape in a sectional view, and the circular concavity is formed at a portion corresponding to a front part of the rotation area of the rotor blades.

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