IP Library › Granted Patent US 12,337,954
Granted Patent B1
US 12,337,954 · App. 18/431,181 · Granted Jun 24, 2025

Convertible drive system

Inventors: Scott R. Kempshall (St. Petersburg, FL); Nicholas Pfeifer (Bradenton, FL)
Assignee: Hyalta Aeronautics, Inc.
B64C25/66B60F5/02B64C11/001B64C25/36B64C25/405B64C37/00F04D29/526B60F2301/04F01D15/00F04D29/326
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Quick Facts
Patent No.
US 12,337,954
App. No.
18/431,181
Granted
Jun 24, 2025
Kind
B1
Abstract

A convertible ducted fan engine and mounting system. The convertible ducted fan engine has a shroud encircling a mechanical fan. The convertible ducted fan engine includes a fluid-propulsion configuration in which the mechanical fan rotates freely with respect to the shroud to produce thrust through fluid flow, and a drive-wheel configuration in which the shroud rotates about the rotational axis.

Claims (45)

1. A convertible drive system, comprising:

a motor;

a mechanical fan configured to be rotated by the motor about a rotational axis;

a shroud that at least partially surrounds the mechanical fan or motor;

a fluid-propulsion configuration in which the mechanical fan independently rotates with respect to the shroud to produce thrust through fluid flow;

a drive-wheel configuration in which the mechanical fan and/or a rotational component of the motor is configured to cause at least a portion of the shroud to rotate about the rotational axis in response to rotation of the mechanical fan and/or the rotational component of the motor.

2. The system of claim 1 , further including:

an aft collar in non-rotational mechanical communication with the shroud, the aft collar having a first interlocking component;

the mechanical fan having a second interlocking component;

the fluid-propulsion configuration including the first interlocking component and the second interlocking component operably disengaged; and

the drive-wheel configuration including the first interlocking component and the second interlocking component operably engaged.

3. The system of claim 2 , further including a spring applying a biasing force that causes the second interlocking component to move towards the first interlocking component or the first interlocking component to move towards the second interlocking component.

4. The system of claim 2 , wherein the second interlocking component is disposed on a hub of the mechanical fan, the hub being radially closer to the rotational axis than a plurality of blades.

5. The system of claim 1 , further including:

a fore translation collar in non-rotational mechanical communication with the shroud, the fore translation collar having a first interlocking component;

the mechanical fan having a second interlocking component;

the fluid-propulsion configuration including the first interlocking component and the second interlocking component operably disengaged; and

the drive-wheel configuration including the first interlocking component and the second interlocking component operably engaged.

6. The system of claim 5 , further including a spring applying a biasing force that causes the second interlocking component to move towards the first interlocking component or the first interlocking component to move towards the second interlocking component.

7. The system of claim 5 , wherein the second interlocking component is disposed on a hub of the mechanical fan, the hub being radially closer to the rotational axis than a plurality of blades.

8. The system of claim 1 , further including a tread disposed on an outer surface of the shroud, thereby providing traction between a shroud-contacting surface and the shroud when the ducted fan engine operates in the drive-wheel configuration.

9. A convertible drive system, comprising: a motor; a mechanical fan configured to be rotated by the motor about a rotational axis; a shroud concentrically aligned with the mechanical fan about the rotational axis; a fluid-propulsion configuration in which the mechanical fan rotates independently with respect to the shroud to produce thrust through fluid flow; and a drive-wheel configuration in which the mechanical fan and/or a rotational component of the motor operably interacts with at least a portion the shroud, such that at least the portion of the shroud rotates about the rotational axis in response to rotation of the mechanical fan and/or the rotational component of the motor.

10. The system of claim 9 , further including:

an aft collar in non-rotational mechanical communication with the shroud, the aft collar having a first interlocking component;

the mechanical fan having a second interlocking component;

the fluid-propulsion configuration including the first interlocking component and the second interlocking component operably disengaged; and

the drive-wheel configuration including the first interlocking component and the second interlocking component operably engaged.

11. The system of claim 10 , further including a spring applying a biasing force that forces the second interlocking component towards the first interlocking component or the first interlocking component towards the second interlocking component.

12. The system of claim 10 , wherein the second interlocking component is disposed on a hub of the mechanical fan, the hub being radially closer to the rotational axis than a plurality of blades.

13. The system of claim 9 , further including:

a fore translation collar in non-rotational mechanical communication with the shroud, the fore translation collar having a first interlocking component;

the mechanical fan having a second interlocking component;

the fluid-propulsion configuration including the first interlocking component and the second interlocking component operably disengaged; and

the drive-wheel configuration including the first interlocking component and the second interlocking component operably engaged.

14. The system of claim 13 , further including a spring applying a biasing force that forces the second interlocking component towards the first interlocking component or the first interlocking component towards the second interlocking component.

15. The system of claim 13 , wherein the second interlocking component is disposed on a hub of the mechanical fan, the hub being radially closer to the rotational axis than a plurality of blades.

16. The system of claim 9 , further including a tread disposed on an outer surface of the shroud, thereby providing traction between a shroud-contacting surface and the shroud when the ducted fan engine operates in the drive-wheel configuration.

17. A convertible drive system, comprising: a motor; a mechanical fan configured to be rotated by the motor about a rotational axis; a shroud concentrically aligned with the mechanical fan about the rotational axis; a fluid-propulsion configuration in which the mechanical fan rotates independently with respect to the shroud to produce thrust through fluid flow; and a drive-wheel configuration in which the mechanical fan and/or a rotational component of the motor operably engages a collar that is in mechanical communication with at least a portion of the shroud, such that at least the portion of the shroud rotates about the rotational axis in response to rotation of the mechanical fan and/or the rotational component of the motor.

18. The system of claim 17 , further including:

a collar in non-rotational mechanical communication with the shroud, wherein the collar is concentrically aligned with the shroud and has a first interlocking component;

the mechanical fan having a second interlocking component;

the fluid-propulsion configuration including the first interlocking component and the second interlocking component operably disengaged; and

the drive-wheel configuration including the first interlocking component and the second interlocking component operably engaged.

19. The system of claim 17 , further including a spring applying a biasing force that forces the second interlocking component towards the first interlocking component or the first interlocking component towards the second interlocking component.

20. The system of claim 17 , wherein the second interlocking component is disposed on a hub of the mechanical fan, the hub being radially closer to the rotational axis than a plurality of blades.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 26, 2024
From: KEMPSHALL, SCOTT R., MR.; PFEIFER, NICHOLAS, MR.
To: HYALTA AERONAUTICS, INC.
Reel/Frame 066904/0337 →
Continuity (7)
Continuation 18196288 · May 11, 2023
Continuation 16898583 · Jun 11, 2020
Continuation In Part 16517242 · Jul 19, 2019
Continuation In Part 16414448 · May 16, 2019
Continuation In Part 16225951 · Dec 19, 2018
Continuation In Part 15209383 · Jul 13, 2016
Provisional Application 62854938 · May 30, 2019
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