The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Dec. 01, 2020

Filed:

Feb. 28, 2018
Applicant:

Rolls-royce North American Technologies, Inc., Indianapolis, IN (US);

Inventor:

Michael P. Dougherty, Indianapolis, IN (US);

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 17/16 (2006.01); F04D 27/02 (2006.01); F02C 9/20 (2006.01); F04D 29/56 (2006.01); F01D 9/04 (2006.01);
U.S. Cl.
CPC ...
F01D 17/162 (2013.01); F01D 9/041 (2013.01); F02C 9/20 (2013.01); F04D 27/0246 (2013.01); F04D 29/563 (2013.01); F05D 2240/12 (2013.01); F05D 2260/407 (2013.01); F05D 2260/57 (2013.01); F05D 2270/44 (2013.01); F05D 2270/62 (2013.01); F05D 2270/66 (2013.01); F05D 2270/808 (2013.01); F05D 2300/505 (2013.01);
Abstract

An improved system, apparatus and method for controlling vane angles in a gas turbine engine, and more specifically, for correcting vane angle error in a gas turbine engine. An active synchronization ring comprises a plurality of micro-actuators coupled to the synchronization ring to correct distortion in the synchronization ring. The micro-actuators apply a bending moment to the synchronization ring to cancel or compensate for synchronization ring distortion. The micro-actuators may be controlled open loop or closed loop. Strain sensors measure ring distortion and provide signals to the controller for closed loop control.


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