COMPONENT ARRANGEMENT FOR A GAS TURBINE
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United States of America Patent
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Issued Date -
Dec 31, 2015
app pub date -
Jun 4, 2015
filing date -
Jun 6, 2014
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Abstract
The present invention relates to a component arrangement for a gas turbine, having a first component of a gas turbine duct casing; a second component, connected to it, of a gas turbine duct casing with a flange; a rocker with an articulated section, which is rotatably mounted in a groove on the first component, which, in a cross section perpendicular to the groove longitudinal direction, has two groove flanks that lie opposite each other in the groove width direction, a groove base connecting these groove flanks, and a groove edge that lies opposite the groove base in a groove depth direction; and a setting screw. The flange of the second component is clamped between the first component and an arm of the rocker, which is tightened against the flange by the setting screw.
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