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:
Nov. 26, 2024

Filed:

Dec. 07, 2021
Applicant:

Zhejiang University, Hangzhou, CN;

Inventors:

Wenjie Zhao, Hangzhou, CN;

Zheng Chen, Hangzhou, CN;

Xueming Shao, Hangzhou, CN;

Jun Li, Hangzhou, CN;

Assignee:

ZHEJIANG UNIVERSITY, Hangzhou, CN;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 29/02 (2006.01); B64C 3/40 (2006.01); B64C 5/02 (2006.01); B64C 5/06 (2006.01); B64C 5/10 (2006.01); B64C 9/00 (2006.01); B64C 15/14 (2006.01); B64C 25/04 (2006.01); B64C 25/16 (2006.01); B64D 27/20 (2006.01); B64U 10/25 (2023.01); B64U 70/80 (2023.01); G05D 1/00 (2006.01); B64U 50/12 (2023.01);
U.S. Cl.
CPC ...
B64C 29/02 (2013.01); B64C 3/40 (2013.01); B64C 5/02 (2013.01); B64C 5/06 (2013.01); B64C 5/10 (2013.01); B64C 9/00 (2013.01); B64C 15/14 (2013.01); B64C 25/04 (2013.01); B64C 25/16 (2013.01); B64D 27/20 (2013.01); B64U 10/25 (2023.01); B64U 70/80 (2023.01); G05D 1/042 (2013.01); B64C 2009/005 (2013.01); B64U 50/12 (2023.01);
Abstract

Provided is a tailstock type vertical take-off and landing unmanned aerial vehicle and a control method thereof. The unmanned aerial vehicle is mainly composed of a fuselage, wings, ailerons, empennages, an elevator, a rudder, an engine, an attitude adjustment nozzle, a landing gear, and the like. The wings are symmetrically arranged on both sides of the middle of the fuselage; the ailerons are hinged to the trailing edges of the wings on the both sides; the empennages are located at the tail of the fuselage, and a form of vertical empennages+horizontal empennages or V-shaped empennages can be used; the elevator and rudder are hinged to the trailing edges of the empennages; the engine is arranged at the tail of the fuselage for producing main thrust.


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