Patent ID: 11959401
Assignee: HONEYWELL INTERNATIONAL INC.
Field: Engines, pumps, turbines (Mechanical engineering)
Classification: CPC F | IPC F

Claim 0:
1. A deswirl system for a gas turbine engine, comprising:
a deswirl shroud;
at least one deswirl vane having a leading end and a trailing end; and
a deswirl hub spaced apart from the deswirl shroud by the at least one deswirl vane, the at least one deswirl vane coupled to the deswirl shroud and the deswirl hub such that the deswirl shroud is radially outboard of the deswirl hub, the deswirl hub including a hub body that extends at a first angle and a hub extension that extends beyond the trailing end of the at least one deswirl vane and beyond an end of the deswirl shroud, the hub extension extending from the hub body at a second angle, and the first angle is different than the second angle.