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:
Dec. 23, 2025
Filed:
Sep. 24, 2024
Sichuan Aerofugia Technology Development Co., Ltd., Chengdu, CN;
Zhejiang Geely Holding Group Co., Ltd., Hangzhou, CN;
Zhaohua Xu, Chengdu, CN;
Songbai Xue, Chengdu, CN;
Qiang Tu, Chengdu, CN;
Yongxiang Sha, Chengdu, CN;
Liang Guo, Chengdu, CN;
Junchang Luo, Chengdu, CN;
Shaiming Xie, Chengdu, CN;
Sichuan Aerofugia Technology Development Co., Ltd., Chengdu, CN;
ZHEJIANG GEELY HOLDING GROUP CO., LTD., Hangzhou, CN;
Abstract
A vertical take-off and landing aircraft includes a fuselage, 2N tilting rotors, and 2N fixed rotors. Wings of a fixed-wing structure are arranged on two sides of the fuselage. An empennage is arranged at a tail of the fuselage. The 2N tilting rotors are symmetrically installed on two sides of the fuselage and located on the front and rear sides of the wings respectively. The 2N fixed rotors are symmetrically installed on the wings on both sides of the fuselage, located on the front and rear sides of the wings respectively and on the outer sides of the tilting rotors. N is a natural number greater than or equal to 2. In a vertical take-off and landing configuration, projections of all the tilting rotors and all the fixed rotors on a horizontal plane are approximately centrally symmetrical about the center of gravity of the aircraft.