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:
Jan. 21, 2025

Filed:

Mar. 24, 2023
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Bhaskar Nanda Mondal, Bengaluru, IN;

Narayanan Payyoor, Thrissur, IN;

Pranav Kamat, Bengaluru, IN;

Assignee:

GENERAL ELECTRIC COMPANY, Evendale, OH (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F01D 15/00 (2006.01); F01D 5/02 (2006.01); F02C 7/06 (2006.01); F02K 3/06 (2006.01);
U.S. Cl.
CPC ...
F01D 15/00 (2013.01); F01D 5/02 (2013.01); F02C 7/06 (2013.01); F02K 3/06 (2013.01); F05D 2240/60 (2013.01); F05D 2300/6033 (2013.01);
Abstract

A turbomachine engine includes an engine core including a high-pressure compressor, a high-pressure turbine, and a combustion chamber. The engine core has a length (L), and the high-pressure compressor has an exit stage diameter (D). A power turbine is in flow communication with the high-pressure turbine. A low-pressure shaft is coupled to the power turbine and characterized by a midshaft rating from one hundred fifty (ft/sec)to three hundred thirty (ft/sec). The low-pressure shaft has a redline speed between fifty and two hundred fifty feet per second. The turbomachine engine is configured to operate up to the redline speed without passing through a critical speed associated with a first-order bending mode of the low-pressure shaft. A high-pressure shaft is coupled to the high-pressure compressor and the high-pressure turbine and is characterized by a high-speed shaft rating from 1.5 to 6.2, and a ratio of L/Dis from 2.1 to 4.3.


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