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:
Apr. 09, 2019

Filed:

Sep. 28, 2016
Applicant:

General Electric Company, Schenectady, NY (US);

Inventor:

David Allen Gutz, Wenham, MA (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
G05D 1/00 (2006.01); G05D 3/00 (2006.01); G05D 13/00 (2006.01); G05D 1/08 (2006.01); B64D 37/00 (2006.01); B64D 27/10 (2006.01); F02C 9/44 (2006.01); F02C 9/00 (2006.01); F02C 9/26 (2006.01); F02C 9/28 (2006.01); F02C 9/42 (2006.01); G06F 15/00 (2006.01);
U.S. Cl.
CPC ...
B64D 37/00 (2013.01); B64D 27/10 (2013.01); F02C 9/00 (2013.01); F02C 9/26 (2013.01); F02C 9/28 (2013.01); F02C 9/42 (2013.01); F02C 9/44 (2013.01); G06F 15/00 (2013.01);
Abstract

A system for an aircraft having a first gas turbine engine and a second gas turbine engine includes a first engine controller comprising a first motion sensor. The first motion sensor defines a first orthogonal coordinate system, and is configured for determining first motion sensor data indicating motion of the aircraft along at least one axis of the first orthogonal coordinate system. The system further includes a second engine controller comprising a second motion sensor spaced apart from the first motion sensor. The second motion sensor defines a second orthogonal coordinate system, and is configured for determining second motion sensor data indicating motion of the aircraft along at least one axis of the second orthogonal coordinate system. In addition, the second engine controller is communicatively coupled to the first engine controller such that the first engine controller receives the second motion sensor data.


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