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:
Jun. 16, 2026

Filed:

Jul. 29, 2020
Applicant:

Japan Aerospace Exploration Agency, Tokyo, JP;

Inventors:

Hiroshi Kobayashi, Tokyo, JP;

Mari Nishiyama, Tokyo, JP;

Akira Nishizawa, Tokyo, JP;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 31/00 (2024.01); B64D 27/30 (2024.01); B64D 27/34 (2024.01); B64D 31/16 (2024.01);
U.S. Cl.
CPC ...
B64D 31/00 (2013.01); B64D 27/30 (2024.01); B64D 27/34 (2024.01); B64D 31/16 (2024.01); Y02T 50/60 (2013.01);
Abstract

Provided are an electric aircraft and an attitude control method therefor that are capable of generating an aerodynamic force in just proportions without impairing fuel consumption performance. In an electric aircraft, an electric propulsion system including a propeller for propulsion and an electric motor that drives the propeller for propulsion is disposed at a leading edge of a wing such that the slipstream generated by the electric propulsion system acts on the wing. A controller is capable of adjusting a thrust of the electric propulsion system to a negative value.


Find Patent Forward Citations

Kobayashi, Hiroshi. (2026). Electric aircraft and attitude control method therefor (U.S. Patent No. 12654869). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12654869

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

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