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:
Aug. 06, 2019

Filed:

Oct. 30, 2015
Applicant:

Rolls-royce Corporation, Indianapolis, IN (US);

Inventor:

Benjamin M. Iwrey, Indianapolis, IN (US);

Assignee:

Rolls-Royce Corporation, Indianapolis, IN (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 11/20 (2006.01); F02C 7/04 (2006.01); F01D 11/08 (2006.01); F04D 29/16 (2006.01); F04D 29/68 (2006.01); F01D 5/20 (2006.01);
U.S. Cl.
CPC ...
F02C 7/04 (2013.01); F01D 5/20 (2013.01); F01D 11/08 (2013.01); F04D 29/164 (2013.01); F04D 29/687 (2013.01); F05D 2270/172 (2013.01); Y02T 50/671 (2013.01); Y02T 50/673 (2013.01);
Abstract

A gas turbine engine system includes a drive shaft and a compressor located in a compressor case. The compressor has a number of rotors. Each rotor includes a number of blades radially extending from a rotor wheel and terminating in a blade tip. The blade tip terminates in close proximity to the case and defines a tip clearance. An air flow control system is coupled to the compressor. The air flow system includes inductive coils and plasma actuators coupled to the case and magnets coupled to the blade. The plasma actuators induce air flows in order to, for example, mitigate air flow leakage around the tip of the blade.


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