TURBOMACHINE WITH COOLED ANNULAR SEGMENTS Russian patent published in 2009 - IPC F01D5/08 

Abstract RU 2347079 C2

FIELD: engines and pumps.

SUBSTANCE: turbomachine comprises body, rotor and multiple cooled annular segments, which are installed between specified body and specified rotor. Every annular segment comprises the main cooling cavity and is fixed to turbine body with the help of fastening devices. Fastening devices comprise binding screws, which are installed approximately in radial direction and press annular segment to specified body. Channel for cooling air passes through specified binding screw, and is connected to specified cooling cavity of annular segment.

EFFECT: higher cooling efficiency.

12 cl, 6 dwg

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RU 2 347 079 C2

Authors

Marshi Mark Rozhe

Rodriges Pol'

Rosse Patris Zhan-Mark

Tajan Zhan Klod Kristian

Arija Zhan Batist

Dates

2009-02-20Published

2004-03-05Filed