A gas turbine engine has a first shaft including a first turbine rotor, and a second shaft including a second turbine rotor disposed downstream of the first turbine rotor. A third shaft includes a propulsor turbine positioned downstream of the second turbine rotor for driving a propeller. A mount ring is secured between the second turbine rotor and the propeller.
TWO SPOOL GAS GENERATOR WITH MOUNT RING
ZWEISPULENGASGENERATOR MIT HALTERING
GÉNÉRATEUR DE GAZ DOUBLE CORPS AVEC ANNEAU DE MONTAGE
2020-01-22
Patent
Elektronische Ressource
Englisch
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