A device for influencing the temperatures in inner ring segments of a gas turbine is provided, which includes in the circumferential direction of the gas turbine, at least one outer shell assembly having a plurality of outer ring segments and at least one inner shell assembly having a plurality of inner ring segments. The inner ring segments are equal to or greater in number than the outer ring segments. An outer ring segment gap is between each two adjacent outer ring segments. An inner ring segment gap is between each two adjacent inner ring segments. An outer ring segment gap, or at least a radial cooling air passage, is located opposite each inner ring segment gap in the radial direction of the gas turbine.
Device and method for influencing the temperatures in inner ring segments of a gas turbine
2020-03-17
Patent
Electronic Resource
English
DEVICE AND METHOD FOR INFLUENCING THE TEMPERATURES IN INNER RING SEGMENTS OF A GAS TURBINE
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