Turbine and manufacturing method therefor

F - Mech Eng,Light,Heat,Weapons – 01 – D

Patent

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F01D 11/12 (2006.01) B21D 53/28 (2006.01) F01D 5/20 (2006.01)

Patent

CA 2411156

A tip of rotor blade which rotates is an abradable surface (14). An inner wall of a shroud (20) as a jacket for the rotor blade is an abrasive surface (23). A part of an abrasive particle (13) protrudes from the abradable surface (14). When the tip of the rotor blade which rotates contacts the inner wall of the shroud, the protruding section (13a) of the abrasive particle slides with the abrasive surface (23) so as to be ground. By doing this, a turbine which can maintain an appropriate clearance between the rotor blade and the shroud and can be used for a long period under high-temperature conditions with easy restoration and remaking thereof.

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