TURBINE BLADE AND GAS TURBINE
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United States of America Patent
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Issued Date -
Aug 25, 2016
app pub date -
Sep 4, 2014
filing date -
Oct 10, 2013
priority date (Note) -
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status (Latency Note)
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Abstract
A turbine blade with a turbine blade aerofoil, a turbine blade root and a turbine blade platform located between the turbine blade aerofoil and the turbine blade root and having, in its underside, an insertion groove for the insertion of a sealing plate; the sealing plate can be secured by a securing element supported on the turbine blade platform, and the turbine blade platform has a material cut-out with two support edges located opposite each other in such a way that the securing element can be secured on both sides to the turbine blade across the axial extension of the turbine blade root.
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