RTX Corporation
Vented tangential on-board injector for a gas turbine engine
Last updated:
Abstract:
An on-board injector that delivers discharge air toward a turbine rotor of a gas turbine engine includes a second wall spaced form a first wall to define an annular inlet about an engine longitudinal axis and a multiple of airfoil shapes between the first wall and the second wall to segregate discharge air from the annular inlet, and a multiple of bypass apertures each along a radial axis transverse to the engine longitudinal axis through each of the multiple of airfoil shapes and the respective first wall, the second wall.
Status:
Grant
Type:
Utility
Filling date:
10 Jun 2020
Issue date:
16 Feb 2021