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. 05, 2023

Filed:

Oct. 15, 2020
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Sridhar Adibhatla, Glendale, OH (US);

Stefan Joseph Cafaro, Maineville, OH (US);

Robert Jon McQuiston, Cincinnati, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 7/00 (2006.01); B64D 45/00 (2006.01); B32B 7/022 (2019.01); B64C 1/12 (2006.01); B64C 1/38 (2006.01); B64D 27/12 (2006.01); F01D 5/14 (2006.01); F01D 5/18 (2006.01); F01D 5/30 (2006.01); F01D 9/04 (2006.01); F01D 15/10 (2006.01); F01D 15/12 (2006.01); F01D 17/16 (2006.01); F01D 25/12 (2006.01); F02C 6/20 (2006.01); F02C 7/264 (2006.01); F02C 7/32 (2006.01); F02C 7/36 (2006.01); F02C 9/00 (2006.01); F02C 9/22 (2006.01); F02K 1/66 (2006.01); F02K 1/76 (2006.01); B64C 1/00 (2006.01); F02C 3/113 (2006.01);
U.S. Cl.
CPC ...
B64D 45/00 (2013.01); B32B 7/022 (2019.01); B64C 1/12 (2013.01); B64C 1/38 (2013.01); B64D 27/12 (2013.01); F01D 5/146 (2013.01); F01D 5/187 (2013.01); F01D 5/30 (2013.01); F01D 5/3007 (2013.01); F01D 7/00 (2013.01); F01D 9/041 (2013.01); F01D 15/10 (2013.01); F01D 15/12 (2013.01); F01D 17/162 (2013.01); F01D 25/12 (2013.01); F02C 6/206 (2013.01); F02C 7/264 (2013.01); F02C 7/32 (2013.01); F02C 7/36 (2013.01); F02C 9/00 (2013.01); F02C 9/22 (2013.01); F02K 1/66 (2013.01); F02K 1/76 (2013.01); B32B 2307/558 (2013.01); B32B 2307/72 (2013.01); B32B 2307/732 (2013.01); B32B 2571/02 (2013.01); B32B 2605/18 (2013.01); B64C 2001/0072 (2013.01); F02C 3/113 (2013.01); F05D 2220/323 (2013.01); F05D 2220/325 (2013.01); F05D 2230/60 (2013.01); F05D 2240/12 (2013.01); F05D 2240/24 (2013.01); F05D 2240/60 (2013.01); F05D 2250/37 (2013.01); F05D 2260/201 (2013.01); F05D 2260/30 (2013.01); F05D 2260/4031 (2013.01); F05D 2260/70 (2013.01); F05D 2270/05 (2013.01); F05D 2270/051 (2013.01); F05D 2270/121 (2013.01); F05D 2270/304 (2013.01); F05D 2270/71 (2013.01); F05D 2270/81 (2013.01);
Abstract

A computing system for an unducted rotor engine with a variable pitch vane assembly in aerodynamic relationship with an unducted rotor assembly, including a sensor-based controller configured to execute a first set of operations and a model-based controller configured to execute a second set of operations. The first set of operations includes obtaining a first signal corresponding to a commanded low spool speed; obtaining a second signal indicative of a pitch angle corresponding to thrust output from the unducted rotor assembly and variable pitch vane assembly; generating a pitch feedback signal corresponding to a commanded adjustment to the pitch angle based at least on one or both of a variable blade pitch angle or a variable vane pitch angle. The second set of operations include obtaining a desired thrust output via a throttle input; determining, at least via a power management block, a commanded thrust output signal; receiving the commanded thrust output signal; and generating an output signal.


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