Cooling system for cooling platform of gas turbine moving blade
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United States of America Patent
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Dec 15, 1998
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N/A
app pub date -
Feb 11, 1997
filing date -
Feb 11, 1997
priority date (Note) -
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Abstract
An effective cooling structure that is intended to cool a platform of a gas turbine moving blade. Cooling air passages (B1, C1, D1; B2, C2, D2; and B3, C3 and D3) are provided through the interior and along the peripheral edge of the platform (2) to thereby cause a cooling air to pass therethrough.
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