Invention Grant
- Patent Title: Impeller shroud with thermal actuator for clearance control in a centrifugal compressor
-
Application No.: US16433089Application Date: 2019-06-06
-
Publication No.: US11002284B2Publication Date: 2021-05-11
- Inventor: Michael Nesteroff , Jonathan Acker , Nate Cooper , Nathan Ottow
- Applicant: Rolls-Royce Corporation
- Applicant Address: US IN Indianapolis
- Assignee: Rolls-Royce Corporation
- Current Assignee: Rolls-Royce Corporation
- Current Assignee Address: US IN Indianapolis
- Agency: Barnes & Thornburg LLP
- Main IPC: F04D29/16
- IPC: F04D29/16 ; F01D11/24 ; F04D27/02 ; F04D29/62 ; F01D11/18 ; F01D11/08 ; F04D29/42 ; F01D11/22

Abstract:
A system for controlling the clearance distance between an impeller blade tip of a centrifugal compressor and a radially inner surface of an impeller shroud in a turbine engine. The system comprises a thermal driver coupled between the impeller shroud and engine casing by hinged linkages. The thermal driver includes an annular ring and annular seal which together define thermal driver cavity. Relatively warm or relatively cool air supplied to the thermal driver cavity cause expansion and contraction, respectively, of the annular ring which is translated by linkages into axially forward and aft motion, respectively.
Public/Granted literature
- US20190323514A1 IMPELLER SHROUD WITH THERMAL ACTUATOR FOR CLEARANCE CONTROL IN A CENTRIFUGAL COMPRESSOR Public/Granted day:2019-10-24
Information query