Lockheed Martin Corporation
TURBINE ENGINE SECONDARY EJECTOR SYSTEM

Last updated:

Abstract:

According to an aspect, an ejector member includes an annular member; a vent arranged at the annular member, the vent having an inlet at a first surface of the annular member, the vent further having an outlet arranged radially inward from a second surface of the annular member; and a vane extending radially inward from the second surface of the annular member.

Status:
Application
Type:

Utility

Filling date:

19 May 2020

Issue date:

25 Nov 2021