IP Library Granted Patent US 12,420,922
Granted Patent B2
US 12,420,922 · App. 18/605,447 · Granted Sep 23, 2025

Vertical take-off and landing craft systems and methods

Inventors: William Kyle Heironimus (Dallas, TX); Brian Wang (San Diego, CA); Stephen Chung (Watauga, TX); Luis Gonzalez (Los Angeles, CA); Tony Li Jung Chen (Irvine, CA); Brett Gibson Morham (Manhattan Beach, CA)
Assignee: Supernal, LLC
B64C29/0033B64C39/04B64C9/00
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Quick Facts
Patent No.
US 12,420,922
App. No.
18/605,447
Granted
Sep 23, 2025
Kind
B2
Abstract

A craft capable of a vertical take-off and landing configuration and a horizontal thrust configuration may include, for example, at least a proprotor, an edgewise blade, and a body. The proprotor may be configured to tilt to achieve a horizontal thrust component. A portion of a lift surface may be configured to tilt with the proprotor. In some embodiments, the vertical take-off and/or landing craft may further comprise a tail connected to a first boom and a second boom. In some embodiments, the vertical take-off and/or landing craft may further comprise a tail attached to the body. In some embodiments, the craft includes four rotors positioned on the lift surface and two rotors positioned on a tail connected to the lift surface.

Claims (46)

1. A craft comprising:

a body;

a lift surface attached to the body;

a first proprotor positioned towards a first end of the lift surface;

a second proprotor positioned towards a second end of the lift surface;

a first boom positioned between the body and the first proprotor and attached to the lift surface;

a second boom positioned between the body and the second proprotor and attached to the lift surface;

wherein the first boom and the second boom are connected via a tail aft of the body, wherein the tail includes a connecting surface above the lift surface, and wherein the connecting surface is substantially horizontal;

a third proprotor positioned at a front surface of the first boom;

a fourth proprotor positioned at a front surface of the second boom;

a fifth proprotor positioned on a first end of the connecting surface; and

a sixth proprotor positioned on a second end of the connecting surface.

2. The craft of claim 1 , wherein the first proprotor, second proprotor, third proprotor, and fourth proprotor are rotatable with respect to the lift surface.

3. The craft of claim 1 , wherein the fifth proprotor and sixth proprotor are rotatable with respect to the connecting surface.

4. The craft of claim 1 further comprising a seventh proprotor positioned on the connecting surface.

5. The craft of claim 1 , wherein the body comprises a cabin, the cabin having a front portion and a rear portion, and wherein the tail is disposed behind the rear portion of the cabin.

6. The craft of claim 1 , wherein the fifth proprotor and the sixth proprotor are positioned at a height above a top surface of the body.

7. The craft of claim 1 , wherein at least one of the first proprotor, the second proprotor, the third proprotor, the fourth proprotor, the fifth proprotor, and the sixth proprotor is a tilt rotor.

8. The craft of claim 1 , wherein the lift surface comprises a wing.

9. The craft of claim 1 , wherein the lift surface comprises a plurality of control surfaces.

10. A craft comprising:

a body;

a lift surface attached to the body;

a first proprotor and a first hub, wherein the first hub is attached to a first end of the lift surface and is configured to rotate about an axis substantially parallel to the lift surface;

a second proprotor and a second hub, wherein the second hub is attached to a second end of the lift surface and is configured to rotate about an axis substantially parallel to the lift surface;

a first boom positioned between the body and the first end of the lift surface, the first boom comprising a third proprotor;

a second boom positioned between the body and the second end of the lift surface, the second boom comprising a fourth proprotor; and

a tail extending upwards aft of the body, the tail comprising at least two rotors, wherein the at least two rotors are positioned at a height above a top surface of the body when the at least two rotors are in a horizontal thrust configuration.

11. The craft of claim 10 , wherein the third proprotor and the fourth proprotor are rotatable with respect to the lift surface.

12. The craft of claim 10 , wherein the at least two rotors are positioned on pylons disposed on the connecting surface.

13. A craft comprising:

a body;

a lift surface attached to the body;

a first proprotor positioned towards a first end of the lift surface;

a second proprotor positioned towards a second end of the lift surface;

a first boom positioned between the body and the first proprotor and attached to the lift surface;

a second boom positioned between the body and the second proprotor and attached to the lift surface;

wherein the first boom and the second boom are connected via a tail aft of the body, wherein the tail includes a connecting surface above the lift surface;

a third proprotor positioned at a front surface of the first boom;

a fourth proprotor positioned at a front surface of the second boom;

a fifth proprotor positioned on a pylon disposed on a first end of the connecting surface;

a sixth proprotor positioned on a pylon disposed on a second end of the connecting surface; and

a seventh proprotor positioned between the fifth proprotor and the sixth proprotor.

14. The craft of claim 13 , wherein the first proprotor, second proprotor, third proprotor, and fourth proprotor are rotatable with respect to the lift surface.

15. The craft of claim 13 , wherein the fifth proprotor, sixth proprotor, and seventh proprotor are rotatable with respect to the connecting surface.

16. The craft of claim 13 , wherein the lift surface and the connecting surface each comprise a plurality of control surfaces.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 4, 2024
From: HEIRONIMUS, WILLIAM KYLE; WANG, BRIAN; CHUNG, STEPHEN; GONZALEZ, LUIS; CHEN, TONY LI JUNG; MORHAM, BRETT GIBSON
To: SUPERNAL, LLC
Reel/Frame 068485/0267 →
Continuity (4)
Continuation In Part 18293472
Provisional Application 63333966 · Apr 22, 2022
Provisional Application 63203822 · Jul 31, 2021
Related Publication 20240217656A1 · Jul 4, 2024
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