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:
Oct. 04, 2022

Filed:

Dec. 02, 2020
Applicant:

Brunswick Corporation, Mettawa, IL (US);

Inventors:

Brian J. Fregonese, Fond du Lac, WI (US);

Trevor George, Savoy, IL (US);

Andrew C. Gunderson, Fond du Lac, WI (US);

Jeffrey D. Reifsnyder, Fond Du Lac, WI (US);

David M. Schmidt, Omro, WI (US);

Assignee:

Brunswick Corporation, Mettawa, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B63H 21/32 (2006.01); B63H 1/20 (2006.01);
U.S. Cl.
CPC ...
B63H 21/32 (2013.01); B63H 1/20 (2013.01);
Abstract

A propeller device has a propeller hub which is elongated along the rotational axis and a propeller blade which radially extends from the propeller hub. The propeller hub and propeller blade are configured so that when the propeller device is forwardly rotated, a first portion of the propeller hub on a first side of the propeller blade encounters a positive pressure and a second portion of the propeller hub on an opposite, second side of the blade encounters a relatively lower pressure or suction, and further so that when the propeller device is reversely rotated, the second portion of the propeller hub encounters a positive pressure and the first portion of the propeller hub encounters a relatively lower pressure or suction. An exhaust vent hole is located in the first portion of the propeller hub and configured to vent exhaust gases from the marine drive via the propeller hub as the propeller device is reversely rotated, thereby enhancing reverse thrust performance of the propeller device.


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