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:
Aug. 04, 2026

Filed:

May. 30, 2025
Applicant:

General Electric Company, Evendale, OH (US);

Inventors:

Jeffrey D. Rambo, Mason, OH (US);

Brandon W. Miller, Middletown, OH (US);

Arthur W. Sibbach, Boxford, MA (US);

Scott D. Hunter, Seattle, WA (US);

Ryan T. Roehm, West Chester, OH (US);

Assignee:

GENERAL ELECTRIC COMPANY, Evendale, OH (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 21/00 (2006.01); F02C 7/06 (2006.01); F02C 9/26 (2006.01); F04C 2/08 (2006.01); F15B 13/04 (2006.01);
U.S. Cl.
CPC ...
F01D 21/006 (2013.01); F02C 7/06 (2013.01); F02C 9/26 (2013.01); F04C 2/084 (2013.01); F15B 13/04 (2013.01); F05D 2260/902 (2013.01); F05D 2260/98 (2013.01);
Abstract

A turbine engine includes a turbo-engine, a fan including a plurality of fan blades that rotate about a longitudinal centerline axis, a rotational component coupled to the fan, a fluid circuit for supplying a fluid to the turbine engine, and a hydraulic fan brake in fluid communication with the fluid circuit. The hydraulic fan brake includes a hydraulic actuator fluidly coupled to the fluid circuit and a brake pad operably coupled to the hydraulic actuator such that the hydraulic actuator moves the brake pad, relative to the rotational component, between a disengaged position, in which the brake pad disengages the rotational component and allows rotation of the rotational component, and an engaged position, in which the brake pad engages the rotational component and prevents rotation of the rotational component, thus preventing rotation of the fan.


Find Patent Forward Citations

Rambo, Jeffrey. (2026). Gas turbine engine having a hydraulic fan brake (U.S. Patent No. 12698724). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12698724

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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