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US07690896B2 Gas turbine disk slots and gas turbine engine using same 有权
燃气轮机槽和燃气轮机使用相同的

Gas turbine disk slots and gas turbine engine using same
Abstract:
A gas turbine engine comprises a compressor section, a combustion section disposed downstream from the compressor section, and a turbine section disposed downstream from the combustion section. The turbine section includes a turbine disk defining a plurality of turbine disk slots for accommodating turbine blades. The plurality of turbine disk slots each include an inlet having a rounded periphery at a bottom portion thereof.
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