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:
Sep. 20, 2022

Filed:

May. 20, 2019
Applicant:

Sp Tech, St. Helen's, OR (US);

Inventors:

Stephen R. Topaz, St. Helen's, OR (US);

Peter A. Topaz, Scappoose, OR (US);

Warren L. Powers, Woodburn, OR (US);

Assignee:

SP TECH, St. Helen's, OR (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/14 (2006.01); F04D 29/38 (2006.01); F04D 29/18 (2006.01); B64C 11/18 (2006.01); B63H 1/26 (2006.01); F04D 29/32 (2006.01);
U.S. Cl.
CPC ...
F04D 29/384 (2013.01); B63H 1/26 (2013.01); B64C 11/18 (2013.01); F04D 29/181 (2013.01); F01D 5/141 (2013.01); F04D 29/324 (2013.01); Y02E 10/72 (2013.01);
Abstract

A propeller blade includes a body configured to extend radially from the hub of a propeller. The body can include a front surface, a back surface, a leading edge, and a trailing edge. The top of the body can form a tippet that generally transitions the front and back surfaces from extending in a generally radial direction to a generally axial direction. The tippet can reduce radial flow and force losses, redirect the radial flow in an axial direction, reduce the exit flow area of the propeller, and increase the inlet flow area of the propeller. The front surface of the blade can have a planar configuration that prevents or reduces the creation of low or negative pressure across the front surface of the blade and associated cavitation.


Find Patent Forward Citations

Loading…