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