WO2026103714 - VERTICAL TAKE-OFF AND LANDING AIRCRAFT
National phase entry is expected:
Publication Number
WO/2026/103714
Publication Date
21.05.2026
International Application No.
PCT/CN2025/134243
International Filing Date
12.11.2025
Title **
[English]
VERTICAL TAKE-OFF AND LANDING AIRCRAFT
[French]
AÉRONEF À DÉCOLLAGE ET ATTERRISSAGE VERTICAUX
[Chinese]
垂直起降飞行器
Applicants **
AUTOFLIGHT (KUNSHAN) CO., LTD.
Inventors
TIAN, Yu
JIN, Mingzhi
Priority Data
202411644031.0
18.11.2024
CN
Application details
| Total Number of Claims/PCT | * |
| Number of Independent Claims | * |
| Number of Priorities | * |
| Number of Multi-Dependent Claims | * |
| Number of Drawings | * |
| Pages for Publication | * |
| Number of Pages with Drawings | * |
| Pages of Specification | * |
| * | |
| Number of Office Actions | * |
| * | |
International Searching Authority |
CNIPA
* |
| Recordal of a Change of the Applicant's Name/Address |
Change of Applicant's Name and Address
* |
| Type of Assignment |
The Standard Agent's Assignment
* |
| Applicant's Legal Status |
Legal Entity
* |
| * | |
| * | |
| * | |
| * | |
| * | |
| Entry into National Phase under |
Chapter I
* |
| Patent Delivery |
Send the Letters Patent by Courier
* |
| Translation |
|
* The data is based on automatic recognition. Please verify and amend if necessary.
** IP-Coster compiles data from publicly available sources. If this data includes your personal information, you can contact us to request its removal.
Quotation for National Phase entry
| Country | Stages | Total | |
|---|---|---|---|
| China | Filing, Examination, Granting | 1577 | |
| EPO | Filing, Examination, Granting | 11551 | |
| Japan | Filing, Examination, Granting | 2000 | |
| South Korea | Filing, Examination, Granting | 1802 | |
| USA | Filing, Examination, Granting | 4740 |
Total:
21,670
Contact Us
Abstract[English]
Disclosed is a vertical take-off and landing aircraft (100), comprising: a fuselage (110); a left wing (121) and a right wing (122) connected to the fuselage; at least two pairs of linear supports (130), the pairs of linear supports being respectively connected to the left wing (121) and the right wing (122), and each linear support being provided with at least four lifting propellers (140); and a front wing (141) and a rear wing (142), the front wing being connected to two linear supports among the at least two pairs of linear supports, and the rear wing being connected to two linear supports among the at least two pairs of linear supports, wherein tractor propellers (241) are provided at the front ends of the linear supports, and/or pusher propellers (242) are provided at the rear ends of the linear supports. The aircraft can carry a relatively large number of passengers while improving safety performance.[French]
Est divulgué un aéronef à décollage et atterrissage verticaux (100), comprenant : un fuselage (110) ; une aile gauche (121) et une aile droite (122) reliées au fuselage ; au moins deux paires de supports linéaires (130), les paires de supports linéaires étant respectivement reliées à l'aile gauche (121) et à l'aile droite (122), et chaque support linéaire étant pourvu d'au moins quatre hélices d'élévation (140) ; et une aile avant (141) et une aile arrière (142), l'aile avant étant reliée à deux supports linéaires parmi deux paires de supports linéaires ou plus et l'aile arrière étant reliée à deux supports linéaires parmi deux paires de supports linéaires ou plus, des hélices de traction (241) étant disposées aux extrémités avant des supports linéaires, et/ou des hélices de poussée (242) étant disposées aux extrémités arrière des supports linéaires. L'aéronef peut transporter un nombre relativement important de passagers tout en améliorant les performances de sécurité.[Chinese]
一种垂直起降飞行器（100），包括机身（110）；连接至机身的左机翼（121）和右机翼（122）；至少两对线性支撑件（130），每对线性支撑件分别连接至左机翼（121）和右机翼（122），每个线性支撑件布置至少四个升力螺旋桨（140）；前翼（141）和后翼（142），前翼连接至少两对线性支撑件中两个，后翼连接至少两对线性支撑件中两个；线性支撑件的前端设置拉力螺旋桨（241）；和/或，线性支撑件的后端设置推力螺旋桨（242）。该飞行器可以运载较大数量规模的乘客，且安全性能提升。