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