IP Library › Granted Patent US 11,702,194
Granted Patent B1
US 11,702,194 · App. 16/898,583 · Granted Jul 18, 2023

Convertible ducted fan engine

Inventors: Scott R. Kempshall (St. Petersburg, FL); Nicholas Pfeifer (Clearwater, 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 11,702,194
App. No.
16/898,583
Granted
Jul 18, 2023
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 (55)

1. A ducted fan engine, comprising:

a motor;

a mechanical fan configured to be rotated by the motor about a rotational axis, the mechanical fan having a plurality of blades;

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 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 ducted fan engine 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 ducted fan engine 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 ducted fan engine 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 the plurality of blades.

5. The ducted fan engine 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 ducted fan engine 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 ducted fan engine 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 the plurality of blades.

8. The ducted fan engine 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 ducted fan engine, comprising:

a motor;

a mechanical fan configured to be rotated by the motor about a rotational axis, the mechanical fan having a plurality of blades;

a shroud concentrically aligned with the mechanical fan about the rotational axis;

a fluid-propulsion configuration in which the mechanical fan independently rotates 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 the shroud, such that 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 ducted fan engine 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 ducted fan engine 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 ducted fan engine 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 the plurality of blades.

13. The ducted fan engine 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 ducted fan engine 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 ducted fan engine 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 the plurality of blades.

16. The ducted fan engine 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 ducted fan engine, comprising:

a motor;

a mechanical fan configured to be rotated by the motor about a rotational axis, the mechanical fan having a plurality of blades concentrically arranged about the rotational axis;

a shroud concentrically aligned with the mechanical fan about the rotational axis;

a fluid-propulsion configuration in which the mechanical fan independently rotates 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 the shroud, such that 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 ducted fan engine 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 ducted fan engine of claim 18 , 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 ducted fan engine of claim 18 , wherein the second interlocking component is disposed on a hub of the mechanical fan, the hub being radially closer to the rotational axis than the plurality of blades.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 15, 2020
From: KEMPSHALL, SCOTT R.; PFEIFER, NICHOLAS
To: HYALTA AERONAUTICS, INC.
Reel/Frame 052937/0191 →
Continuity (5)
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
Cited By (2)
US 12,296,993 US 12,337,954