Back to results
US 2024/0262489 A1Published application
Dual engine vertical take off and landing collapsible fixed wing aircraft
AssigneeAnduril Industries, Inc.
InventorsSean Keith-Stewart, Christian William Lopez, Jessica Rader
Life of this patent
Estimating the term…
Abstract
The present application discloses an aircraft. The aircraft comprises a first wing and a second wing, a fuselage to which the first wing and the second wing are mounted, a first engine operatively mounted to the first wing, and a second engine operatively mounted to the second wing. The aircraft is configured to vertically take-off and land. The first engine and the second engine are used for both (i) vertical take-off and landing, and (ii) horizontal flight
Claims20
An aircraft, comprising:
- a first wing and a second wing;
- a fuselage disposed between the first wing and the second wing;
- a first engine operatively mounted to the first wing;
- and
- a second engine operatively mounted to the second wing,
- wherein:
- the aircraft is configured to vertically take-off and land;
- and
- the first engine and the second engine are used for both (i) vertical take-off and landing, and (ii) horizontal flight.
6 more elements
Dependencies are inferred from the claim text.