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:
Feb. 03, 2026

Filed:

Dec. 28, 2023
Applicant:

Subaru Corporation, Tokyo, JP;

Inventors:

Mizuki Nakamura, Tokyo, JP;

Shuzou Hakuta, Tokyo, JP;

Hirotoshi Tsukamoto, Tokyo, JP;

Masafumi Sasaki, Tokyo, JP;

Ryusuke Sakamoto, Tokyo, JP;

Takumi Shinotsuka, Tokyo, JP;

Mitsunori Fukudome, Tokyo, JP;

Hiroshi Nagai, Tokyo, JP;

Hiroshi Taguchi, Tokyo, JP;

Toshihiro Yokoyama, Tokyo, JP;

Assignee:

SUBARU CORPORATION, Tokyo, JP;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/12 (2006.01); B64C 27/82 (2006.01);
U.S. Cl.
CPC ...
B64C 27/12 (2013.01); B64C 27/82 (2013.01); B64C 2027/8263 (2013.01);
Abstract

A vertical tail of a helicopter has a leading edge and a trailing edge concave toward the leading edge. The helicopter includes a main rotor and a tail rotor for generating anti-torque to cancel torque generated by rotation of the main rotor. The trailing edge is concave within a range within which the vertical tail overlaps a circular region, formed as a rotation range of the tail rotor, in a rotation axis direction of the tail rotor.


Find Patent Forward Citations

Nakamura, Mizuki. (2026). Helicopter (U.S. Patent No. 12539961). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12539961

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

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