Flexible coupling shaft for turbine engine
AssigneeGE Avio S.r.l.
InventorsMarco Garabello, Paolo Altamura, Gian Mario Bragallini, Alessio Gargioli, Jan Biskupski
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AssigneeGE Avio S.r.l.
InventorsMarco Garabello, Paolo Altamura, Gian Mario Bragallini, Alessio Gargioli, Jan Biskupski
Estimating the term…
The present disclosure is directed to a shaft assembly (95) for a turbine engine (10), wherein the turbine engine includes a fan or propeller assembly (14) and an engine core (20), and further wherein the fan or propeller assembly includes a gearbox (45), and wherein the engine core includes one or more rotors (32). The shaft assembly (95) includes a flexible shaft (100) defining a first end (101) and a second end (102) along the axial direction, wherein the first end is connected to the engine core (20) and the second end is connected to the gearbox (45), and wherein a plurality of splines (110) is defined at the second end (102) and coupled to a spline interface (46) at the gearbox (45); and a coupling (120) extended at least partially in the radial direction and coupled to the engine core and the flexible shaft.
A shaft assembly for a turbine engine, wherein the turbine engine includes a fan or propeller assembly and an engine core, and further wherein the fan or propeller assembly includes a gearbox, and wherein the engine core includes one or more rotors, the shaft assembly comprising:
A turbine engine defining an axial direction and a radial direction, the turbine engine comprising:
Dependencies are inferred from the claim text.