Blade arrangement for a gas turbine and method for operating such a blade arrangement
AssigneeALSTOM Technology Ltd
InventorsSascha Justl, Carlos Simon-Delgado, Herbert Brandl
Life of this patent
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AssigneeALSTOM Technology Ltd
InventorsSascha Justl, Carlos Simon-Delgado, Herbert Brandl
Estimating the term…
A blade arrangement is provided for a gas turbine, in which blade leaves, having a leading edge and a trailing edge and also a pressure side and a suction side, are assembled sealingly with platforms configured as separate components. A peripheral sealing arrangement is provided between the blade leaves and the associated platforms, which seals off an interspace between the blade leaves and platforms against hot gas flowing around the blade leaves. A directed site-dependent supply of cooling air for purging the sealing arrangement is provided on a side of the sealing arrangement which faces away from the hot gas. A method of operating the above blade arrangement is also provided. The method includes supplying cooling air for purging the sealing arrangement at a pressure which decreases from the leading edge of the blade leaves to the trailing edge.
A blade arrangement for a gas turbine, in which comprising:
A method for operating a blade arrangement for a gas turbine, including blade leaves, having a leading edge, a trailing edge, a pressure side and a suction side, platforms configured as separate components, the blade leaves sealingly assembled with respective platforms, a peripheral sealing arrangement provided between the blade leaves and the respective platforms for sealing off an interspace between the blade leaves and the respective platforms against gas flowing around the blade leaves, a directed site-dependent supply of cooling air for purging the sealing arrangement provided on a side of the sealing arrangement which faces away from the hot gas, wherein the cooling air supply includes cooling ducts which run between the blade leaves and the respective platforms, the cooling ducts arranged, in each case, on the pressure side and the suction side of each blade leaf, the method comprising:
A method for operating a blade arrangement for a gas turbine, including blade leaves, having a leading edge, a trailing edge, a pressure side and a suction side, platforms configured as separate components, the blade leaves sealingly assembled with respective platforms, a peripheral sealing arrangement provided between the blade leaves and the associated platforms for sealing off an interspace between the blade leaves and respective platforms against gas flowing around the blade leaves, a directed site-dependent supply of cooling air for purging the sealing arrangement provided on a side of the sealing arrangement which faces away from the hot gas, the method comprising:
Dependencies are inferred from the claim text.