WO2025081447 - A HOUSEHOLD INTELLIGENT, LIGHTWEIGHT, SAFE, SMALL-FOLDING MANNED AIRCRAFT
National phase entry is expected:
Publication Number
WO/2025/081447
Publication Date
24.04.2025
International Application No.
PCT/CN2023/125553
International Filing Date
20.10.2023
Title **
[English]
A HOUSEHOLD INTELLIGENT, LIGHTWEIGHT, SAFE, SMALL-FOLDING MANNED AIRCRAFT
[French]
AÉRONEF PILOTÉ PLIABLE, PETIT, SÛR, LÉGER, INTELLIGENT ET DOMESTIQUE
Applicants **
SU, Wu
Inventors
SU, Hengzhi
Priority Data
202311356649.2
19.10.2023
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 | * |
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| Number of Office Actions | * |
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International Searching Authority |
EPO
* |
| 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 |
Natural Person
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| * | |
| * | |
| * | |
| * | |
| * | |
| Entry into National Phase under |
Chapter I
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| Patent Delivery |
Send the Letters Patent by Courier
* |
| Translation |
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* 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 | 1893 | |
| EPO | Filing, Examination, Granting | 6643 | |
| Japan | Filing, Examination, Granting | 2023 | |
| South Korea | Filing, Examination, Granting | 1779 | |
| USA | Filing, Examination, Granting | 8340 |
Total:
20,678
The term for entry into the National Phase has expired. This quotation is for informational purposes only
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Abstract[English]
The invention discloses a household intelligent, lightweight, safe, folding small manned aircraft, which comprises a ground driving system, a rotor wing flight system, a cabin (10) and a fixed wing flight system (13, 14). The ground driving system comprises a tire leg (5), a force spring sensor (6) and a driving motor; The rotor wing flight system includes a folding arm (2), a motor (3), a rotor wing (4) and an anti-collision radar. The fixed-wing flight system consists of foldable fixed wings (13, 14), motors and a rotor wing (12). The top of the aircraft adopts an inflatable low cost parachute (9), the bottom adopts an anti-fall airbag, the wing is provided with an anti-collision radar, and the front is provided with a micro laser ranging radar, which is safe and reliable to use. The structure of the invention adopts optionally carbon fiber material, which makes the weight light.[French]
L'invention concerne un aéronef piloté pliable, petit, sûr, léger, intelligent et domestique, qui comprend un système de conduite au sol, un système de vol à aile à rotor, une cabine (10) et un système de vol à ailes fixes (13, 14). Le système de conduite au sol comprend une jambe à pneumatique (5), un capteur à ressort de force (6) et un moteur de conduite. Le système de vol à aile à rotor comprend un bras de pliage (2), un moteur (3), une aile à rotor (4) et un radar anti-collision. Le système de vol à ailes fixes est constitué d'ailes fixes pliables (13, 14), de moteurs et d'une aile à rotor (12). La partie supérieure de l'aéronef comporte un parachute à faible coût gonflable (9), la partie inférieure adopte un coussin de sécurité gonflable anti-chute, l'aile comporte un radar anti-collision, et l'avant comporte un micro-radar de télémétrie laser, qui est sûr et fiable à utiliser. La structure de l'invention adopte éventuellement un matériau à fibres de carbone, ce qui réduit le poids.