APPARATUS FOR CONTROLLED DELIVERY OF COOLING AIR TO TURBINE BLADES IN A GAS TURBINE

An apparatus for controlled delivery of cooling air to turbine blades (5) in a gas turbine (1) including a rotor unit (4), at least a first and second row of turbine blades (5), a plurality of rotor heat shield elements (23) disposed in a circumferential row between the first and second rows of turb...

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Bibliographic Details
Main Authors GARBUGLIA, Francesco, SCHNIEDER, Martin, VON ARX, Beat, KOENIG, Marcel, ZIERER, Thomas
Format Patent
LanguageEnglish
French
German
Published 29.07.2020
Subjects
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Summary:An apparatus for controlled delivery of cooling air to turbine blades (5) in a gas turbine (1) including a rotor unit (4), at least a first and second row of turbine blades (5), a plurality of rotor heat shield elements (23) disposed in a circumferential row between the first and second rows of turbine blades (5) and configured to define with said rotor unit (4) a rotor heat shield passage (33, 34, 35, 36) that is fed with cooling air, and a plurality of lock plates (41, 42, 43) disposed in a circumferential row and configured to secure at least one of said first and second rows (6, 7, 8) of turbine blades (5) to the rotor unit (4), wherein a radial portion (28) of the rotor shield elements (23) and/or the lock plates (41, 42, 43) include at least one opening (49) for controlled flow of cooling air.
Bibliography:Application Number: EP20170205756