Housing-side structure of a turbomachine
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United States of America Patent
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Jan 10, 2017
Grant Date -
Jul 18, 2013
app pub date -
Aug 29, 2011
filing date -
Sep 1, 2010
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Abstract
A housing-side structure of a turbomachine, in particular of a gas turbine, including an in particular segmented jacket ring (16), which carries an abradable lining for radially outer ends of rotor-side moving blades of a moving blade ring, wherein the jacket ring (16) carrying the abradable lining is connected by means of at least one constriction (18) to a stator-side housing part (19), which is radially adjacent to the jacket ring (16) on the outside and the jacket ring is thermally decoupled from said stator-side housing.
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