Gas turbine having a high-speed low-pressure turbine and a turbine case
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United States of America Patent
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Jan 10, 2019
app pub date -
Jul 5, 2018
filing date -
Jul 5, 2018
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Abstract
A gas turbine (40) having a high-speed low-pressure turbine (24) and a turbine case (28) that bounds a flow path of a working fluid of the gas turbine (40) and an exit region (30), and extends between a rotor (32) of the high-speed low-pressure turbine (24) that is the most downstream in the through flow direction of the working fluid, and an exit opening (34) of the turbine case (28). The exit region (30) is designed to be free of exit guide vane assemblies.
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