Cooling of gas turbine shroud rings

Rotary kinetic fluid motors or pumps – With changing state confined heat exchange mass

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415115, 415139, 60266, 60912, F01B 322

Patent

active

051785145

ABSTRACT:
A gas turbine engine is provided with an annular array of rotor blades which are surrounded by a shroud ring. The shroud ring includes a number of adjacent heat pipes which are of the variable conductance type. The heat pipes each have a portion which is externally of the shroud ring which portion is in turn divided into two parts. The first part is exposed to a flow of cooling air while the second part contains a buffer which operationally varies the conductance of the heat pipe, in accordance with the temperature of air which is tapped from the high pressure compressor of the engine. This serves to ensure that the shroud ring remains substantially isothermal and provides control over the clearance between the tips of the rotary blades and the shroud ring through thermal control of the shroud ring.

REFERENCES:
patent: 2633327 (1953-03-01), McDowell
patent: 3751909 (1973-08-01), Kohler
patent: 3756020 (1973-09-01), Moskowitz et al.
patent: 3864056 (1975-02-01), Gabriel et al.
patent: 3957391 (1976-05-01), Vollinger
patent: 4136516 (1979-01-01), Corsmeier
patent: 4149824 (1979-04-01), Adamson
patent: 4155680 (1979-05-01), Linko, III et al.
patent: 4292008 (1981-09-01), Grosjean et al.
patent: 4505639 (1985-03-01), Groess et al.
patent: 4566851 (1986-01-01), Comeau et al.

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