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. 06, 2026

Filed:

Mar. 25, 2024
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Daniel A. Niergarth, Norwood, OH (US);

Martin Manning, Cincinnati, OH (US);

Nicholas M. Daggett, Camden, ME (US);

Christopher J. Kroger, West Chester, OH (US);

Ian F. Prentice, Cincinnati, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 3/06 (2006.01); F01D 7/00 (2006.01); F02K 3/072 (2006.01); F02K 3/075 (2006.01); F02K 3/077 (2006.01); F04D 29/36 (2006.01);
U.S. Cl.
CPC ...
F02K 3/06 (2013.01); F02K 3/072 (2013.01); F04D 29/362 (2013.01); F01D 7/00 (2013.01); F02K 3/075 (2013.01); F02K 3/077 (2013.01); F05D 2220/36 (2013.01); F05D 2260/40311 (2013.01); F05D 2260/74 (2013.01);
Abstract

A turbomachinery engine can include a fan assembly with a plurality of variable pitch fan blades. The fan blades are configured such that they define a first VPF parameter and a second VPF parameter. The first VPF parameter is within a range of 0.10 to 0.40 and is defined as the hub-to-tip radius ratio divided by the fan pressure ratio. The second VPF parameter is within a range of 1-30 lbf/inand is defined as the bearing spanwise force divided by the fan area. In certain examples, the turbomachinery engine further includes a pitch change mechanism, a vane assembly, a core engine, and a gearbox.


Find Patent Forward Citations

Niergarth, Daniel. (2026). Variable pitch fans for turbomachinery engines (U.S. Patent No. 12516646). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12516646

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

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