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.
Patent No.:
Date of Patent:
Apr. 29, 2025
Filed:
Sep. 07, 2020
Applicant:
Aeronext Inc., Shibuya-ku, JP;
Inventor:
Yoichi Suzuki, Shibuya-ku, JP;
Assignee:
AERONEXT INC., Shibuya-ku, JP;
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64U 10/20 (2022.12); B64C 3/42 (2005.12); B64C 27/26 (2005.12); B64C 29/00 (2005.12); B64C 39/02 (2022.12); B64D 45/04 (2005.12); B64U 50/13 (2022.12);
U.S. Cl.
CPC ...
B64U 10/20 (2022.12); B64C 3/42 (2012.12); B64C 27/26 (2012.12); B64C 29/0033 (2012.12); B64C 39/02 (2012.12); B64D 45/04 (2012.12); B64U 50/13 (2022.12);
Abstract
A flying vehicle with a flight part connected to a plurality of rotor wing parts and a main wing, wherein the main wing is configured such that the lift produced by the main wing during landing is reduced compared to the lift produced by the main wing during cruising. Furthermore, the main wing is fixed at a forward tilt with respect to the flight part. Furthermore, the rotor wing is connected at an angle that produces propulsion and lift during cruise. Furthermore, the rotor blades are connected at an angle that generates propulsive force during cruise.