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:
Mar. 08, 2022

Filed:

Jun. 10, 2019
Applicant:

Subaru Corporation, Tokyo, JP;

Inventors:

Wataru Kobayashi, Tokyo, JP;

Hokuto Yamane, Tokyo, JP;

Hirotaka Hayashi, Tokyo, JP;

Hiroshi Taguchi, Tokyo, JP;

Assignee:

SUBARU CORPORATION, Tokyo, JP;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/46 (2006.01); B64C 27/473 (2006.01); B64C 23/06 (2006.01); F04D 29/38 (2006.01); F04D 29/66 (2006.01);
U.S. Cl.
CPC ...
B64C 27/463 (2013.01); B64C 23/069 (2017.05); B64C 27/473 (2013.01); F04D 29/384 (2013.01); F04D 29/667 (2013.01);
Abstract

A rotor blade for an aircraft includes first and second blade tips, a blade body, and a vortex-generating blade. The blade body has an end forming the first blade tip of the rotor blade and an airfoil section configured such that during rotation, pressure acting on a lower surface of the blade body is greater than pressure acting on an upper surface of the blade body. The vortex-generating blade is disposed at an end of the rotor blade and forms the second blade tip. The vortex-generating blade also has an airfoil section configured such that during rotation, pressure acting on a lower surface of the vortex-generating blade is smaller than pressure acting on an upper surface of the vortex-generating blade.


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