WO2024168075 - COMPACT PERSONAL FLIGHT VEHICLE

National phase entry is expected:
Publication Number WO/2024/168075
Publication Date 15.08.2024
International Application No. PCT/US2024/014859
International Filing Date 07.02.2024
Title **
[English] COMPACT PERSONAL FLIGHT VEHICLE
[French] VÉHICULE DE VOL PERSONNEL COMPACT
Applicants **
KOWALD, Hunter William
Inventors
KOWALD, Hunter William
Priority Data
63/443,815   07.02.2023   US
18/494,650   25.10.2023   US
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
*
Recordal of a Change of the Applicant's Name/Address
*
Type of Assignment
*
Applicant's Legal Status
*
*
*
*
*
*
Entry into National Phase under
*
*
*
*
Patent Delivery
*
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 StagesTotal
China Filing, Examination, Granting2751
EPO Filing, Examination, Granting14449
Japan Filing, Examination, Granting2616
South Korea Filing, Examination, Granting2323
USA Filing, Examination, Granting7340
MasterCard Visa
Total: 29,479

The term for entry into the National Phase has expired. This quotation is for informational purposes only

Contact Us
Abstract[English] An apparatus includes a frame and a plurality of propellers coupled to the frame and configured to produce sufficient thrust to allow the apparatus to hover. Each propeller from the plurality of propellers having a horizontally oriented blade and a first propeller from the plurality of propellers overlapping a second propeller from the plurality of propellers in a vertical plane.[French] Un appareil comprend un corps et une pluralité d'hélices couplées au corps et conçues pour produire une poussée suffisante afin de permettre à l'appareil d'effectuer un vol stationnaire. Chaque hélice de la pluralité d'hélices a une pale orientée horizontalement et une première hélice de la pluralité d'hélices chevauchant une seconde hélice de la pluralité d'hélices dans un plan vertical.