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:
Jul. 04, 2023

Filed:

Sep. 10, 2021
Applicants:

General Electric Company, Schenectady, NY (US);

GE Avio S.r.l., Rivalta di Torino, IT;

Inventors:

Roberto Maddaleno, Lanzo Torinese, IT;

Antonio Giuseppe D'Ettole, Rivoli, IT;

Matteo Renato Usseglio, Turin, IT;

Alessandra Torri, Turin, IT;

Darek Tomasz Zatorski, Fort Wright, KY (US);

Assignees:

General Electric Company, Schenectady, NY (US);

GE Avio S.r.l., Turin, IT;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 21/02 (2006.01); F01D 21/00 (2006.01);
U.S. Cl.
CPC ...
F01D 21/02 (2013.01); F01D 21/003 (2013.01); F05D 2260/40311 (2013.01); F05D 2260/902 (2013.01); F05D 2270/021 (2013.01); F05D 2270/304 (2013.01);
Abstract

A turbomachine, a computing system for a turbomachine, and a method for overspeed protection are provided. The turbomachine includes a first rotor assembly interdigitated with a second rotor assembly together operably coupled to a gear assembly. A plurality of sensors is configured to receive rotor state data indicative of one or more of a speed, geometric dimension, or capacitance, or change thereof, or rate of change thereof, relative to the first rotor assembly or the second rotor assembly. A controller executes operations including receiving rotor state data from the plurality of sensors; comparing rotor state data to one or more rotor state limits; and contacting one or more of the first rotor assembly or the second rotor assembly to a contact surface adjacent to the respective first rotor assembly or the second rotor assembly if the rotor state data exceeds the rotor state limit.


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