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:
Feb. 24, 2015

Filed:

Oct. 14, 2011
Applicants:

Askari Badre-alam, Apex, NC (US);

David Boswell, Raleigh, NC (US);

Donald Morris, Wendell, NC (US);

Wayne Lee Winzenz, Raleigh, NC (US);

Inventors:

Askari Badre-Alam, Apex, NC (US);

David Boswell, Raleigh, NC (US);

Donald Morris, Wendell, NC (US);

Wayne Lee Winzenz, Raleigh, NC (US);

Assignee:

LORD Corporation, Cary, NC (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 11/08 (2006.01); F01D 25/04 (2006.01); B64C 11/00 (2006.01);
U.S. Cl.
CPC ...
B64C 11/008 (2013.01); F01D 25/04 (2013.01); Y10S 416/50 (2013.01);
Abstract

An aircraft system and method with a first counterweight rotating balancing rotor mass concentration, and a second counterweight rotating balancing rotor mass concentration to balance a first aircraft propeller. The system includes an inboard electromagnetic coil driver with a first inboard electromagnetic coil, and a second inboard electromagnetic coil, the inboard electromagnetic coil driver and the first counterweight balancing rotor and the second counterweight balancing rotor centered around the aircraft propeller shaft rotating machine member. The system/method utilizes a first control system controller to control the coils and position the mass concentrations to balance the first aircraft propeller. The system/method includes a third counterweight rotating balancing rotor mass concentration, and a fourth counterweight rotating balancing rotor mass concentration to balance a second aircraft propeller which positioned and controlled by a second control system controller.


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