Abstract: A system for controlling the clearance distance between an impeller blade tip of a centrifugal compressor and a radially inner surface of a segregated impeller shroud in a turbine engine. The system comprises a driving mechanism coupled to a portion of a segregated impeller shroud. The driving mechanism comprises a driving arm and threaded axial member configured to translate motion of an actuator ring into axially forward and aft motion of the portion of the segregated impeller shroud.
Type:
Grant
Filed:
August 1, 2019
Date of Patent:
March 2, 2021
Assignee:
Rolls-Royce Corporation
Inventors:
Nathan Ottow, Johnathan Acker, Nate Cooper, Mark Whitlock, Michael Nesteroff