Convex compressor casing

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

Patent

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Details

F04D 29/40 (2006.01) F01D 5/14 (2006.01) F01D 25/24 (2006.01) F04D 29/16 (2006.01) F04D 29/26 (2006.01) F04D 29/52 (2006.01) F04D 29/54 (2006.01)

Patent

CA 2333809

A compressor casing (32) includes an axially convex inner surface (32a) for surrounding a row of rotor blades (14) with radial gaps therebetween. The tips (22) of the blades complement the casing contour for reducing blade tip losses and flow blockage.

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