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Inventor profile of:

Thomas C. Corke

City:

Granger, Indiana

Country:

United States

Published Applications:

Last publication date:

2021-06-03

Top Assignees for applications by Thomas C. Corke

The entities that hold a legal rights for patent applications filed by inventor Corke Thomas C.:

THE UNIVERSITY OF NOTRE DAME DU LAC 3 Notre Dame, IN United States
University of Notre Dame du Lac 2 Notre Dame, IN United States
UNIVERSITY OF NOTRE DAME DU LAC 2 South Bend, IN United States
Orbital Research Inc. 2 Cleveland, OH United States
HONEYWELL INTERNATIONAL INC. 1 Morris Plains, NJ United States
HONEYWELL INTERNATIONAL INC. 1 Morristown, NJ United States
Notre Dame University 1 South Bend, IA United States
The United States of America as Represented by the Secretary of the Air Force 1 Washington, DC United States
BELL HELICOPTER TEXTRON INC. 1 Hurst, TX United States
TEXTRON INNOVATIONS INC. 1 PROVIDENCE, RI United States

Recent patent applications by Corke Thomas C.

Thomas C. Corke from Granger, US has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2021-06-03

US20210164503A1

Mechanical engineering

Method and apparatus of plasma flow control for drag reduction

#2 | 2018-02-01

US20180031013A1

Mechanical engineering

Method and apparatus of plasma flow control for drag reduction

#3 | 2017-03-02

US20170058782A1

Mechanical engineering

PLASMA ACTUATED CASCADE FLOW VECTORING

#4 | 2014-10-30

US20140321987A1

Mechanical engineering

PLASMA ACTUATED CASCADE FLOW VECTORING

#5 | 2012-09-18

US13094872

Method of controlling aircraft, missiles, munitions and ground vehicles with plasma actuators

#6 | 2011-06-07

US12604903

Method of controlling aircraft, missiles, munitions and ground vehicles with plasma actuators

#7 | 2011-05-26

US20110121158A1

Physics

Methods and apparatus for plasma based adaptive optics for generating a first plasma gradient and a second plasma gradient

#8 | 2010-09-09

US20100224733A1

Performing operations; transporting

Plasma actuators for drag reduction on wings, nacelles and/or fuselage of vertical take-off and landing aircraft

#9 | 2009-03-12

US20090065064A1

Mechanical engineering

COMPRESSOR TIP GAP FLOW CONTROL USING PLASMA ACTUATORS

#10 | 2008-06-03

US10994029

Single dielectric barrier aerodynamic plasma actuation

#11 | 2008-05-29

US20080122252A1

Performing operations; transporting

Methods and apparatus for reducing drag via a plasma actuator

InventorID:

952427 ⎘