Patent ID: 11891908
Assignee: RTX CORPORATION
Field: Engines, pumps, turbines (Mechanical engineering)
Classification: CPC F  B | IPC F

Claim 10:
11. A gas turbine engine, comprising:
a bearing assembly;
a rotor rotatable about a rotational axis, the rotor journaled within the bearing assembly; and
a lubrication system arranged radially outward of and fluidly coupled with the bearing assembly, the lubrication system comprising:
a lubrication channel including an inlet and an outlet; and
a dispersion cone configured to receive lubricant from the outlet, the dispersion cone comprising an airfoil shaped spar within an interior of the dispersion cone, the airfoil shaped spar formed intergral with the dispersion cone, and the airfoil shaped spar configured to disperse the lubricant traveling through the dispersion cone.