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:
Jul. 08, 2025

Filed:

Dec. 22, 2022
Applicant:

Israel Aerospace Industries Ltd., Lod, IL;

Inventors:

Danny Abramov, Lod, IL;

Shai Alexandroni, Lod, IL;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/26 (2006.01); B64C 29/00 (2006.01); B64U 10/25 (2023.01);
U.S. Cl.
CPC ...
B64C 29/0025 (2013.01); B64C 27/26 (2013.01); B64U 10/25 (2023.01);
Abstract

A VTOL-type air vehicle is transitioned from forward speed mode to hover mode via a transient path in transition mode. The air vehicle includes first and second propulsion systems, and high lift, mild stall fixed wings. The first propulsion system can provide a first thrust (sufficient for enabling powered aerodynamic flight) at a first thrust vector. The second propulsion system can provide a second thrust (sufficient for enabling vectored thrust flight) at a second thrust vector, which is spatially fixed with respect to the air vehicle at least during transitioning. The transient path includes, during transitioning, manipulating a first magnitude of angle of attack and a second magnitude of forward speed to provide a corresponding aerodynamic lift component, and concurrently manipulating a third magnitude of the second thrust to provide a vertical vectored thrust component corresponding to the first magnitude of angle of attack. A summation of the aerodynamic lift component and vertical vectored thrust component is sufficient for enabling the air vehicle to remain in controlled flight in transition mode.


Find Patent Forward Citations

Loading…