MORPHING DUCTED FAN FOR VERTICAL TAKE-OFF AND LANDING VEHICLE

• US 20110147533A1
• Filed: 12/21/2009
• Published: 06/23/2011
• Est. Priority Date: 12/21/2009
• Status: Abandoned Application

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Cox, Paul Alan, O'Brien, Patrick, Goossen, Emray
• Application Number:
  US12/643,839
• Publication Number:
  US 20110147533A1
• Time in Patent Office: Days
• US Class Current: 244/23.A
• CPC Class Codes: B64C 11/001 Shrouded propellers
• CPC Class Codes: B64C 39/024 of the remote controlled vehicle type, i.e. RPV
• CPC Class Codes: B64U 10/13 Flying platforms
• CPC Class Codes: B64U 30/20 Rotors; Rotor supports
• CPC Class Codes: B64U 30/26 Ducted or shrouded rotors

Abstract

A morphing duct of a ducted fan for a vertical take-off and landing (VTOL) vehicle is configured to change shape as function of the flight mode of the vehicle to improve the thrust per unit energy input for the ducted fan. Additionally, the morphing duct may be configured to change shape to change the flight path of the VTOL vehicle.

Claims

1. A ducted fan for a vertical take-off and landing (VTOL) vehicle, the ducted fan comprising:

a rotor fan; and

an annular duct surrounding the fan and comprising an inlet section on a first side of the fan and an outlet section on a second side of the fan opposing the first side,

wherein at least one of the inlet section or the outlet section is configured to actively change shape as a function of a mode of operation of the VTOL vehicle.

2. The ducted fan of claim 1, wherein the at least one of the inlet section or the outlet section is configured to change from a first shape in a first mode of operation of the VTOL vehicle to a second shape in a second mode of operation of the VTOL vehicle.

3. The ducted fan of claim 2, wherein at least one of the first shape or the second shape comprises a converging arcuate, a radius bell mouth, or an elliptical bell mouth shape.

4. The ducted fan of claim 1, further comprising:

a flight control module configured to generate an electric signal indicative of the mode of operation of the VTOL vehicle; and

a duct control module configured determine the mode of operation of the VTOL vehicle based on the electrical signal.

5. The ducted fan of claim 1, wherein the at least one of the inlet section or the outlet section is configured to change to a shape that changes a contraction ratio of the respective section as a function of the mode of operation of the VTOL vehicle, the contraction ratio being at least one of an area defined by a highlight radius of the inlet section divided by an area defined by a throat radius of the annular duct, or an area defined by an exit radius of the outlet section divided by the area defined by the throat radius.

6. The ducted fan of claim 5, wherein the at least one of the inlet section or the outlet section is configured to increase the contraction ratio in a first mode of operation of the VTOL vehicle and decrease the contraction ratio in a second mode of operation of the VTOL vehicle.

7. The ducted fan of claim 1, wherein the inlet section is configured to change to a first shape that increases a contraction ratio of the inlet section in a first mode of operation of the VTOL vehicle, wherein the contraction ratio is defined as an area defined by a highlight radius of the inlet section divided by an area defined by a throat radius of the annular duct, and configured to change to a second shape that decreases the contraction ratio of the inlet section in a second mode of operation of the VTOL vehicle.

8. The ducted fan of claim 7, wherein the outlet section is configured to change to a first shape that decreases a contraction ratio of the outlet section in the first mode of operation of the VTOL vehicle, the contraction ratio comprising an area defined by an exit radius of the outlet section divided by an area defined by the throat radius of the annular duct, and to change to a second shape that increases the contraction ratio of the outlet section in the second mode of operation of the VTOL vehicle.

9. The ducted fan of claim 1, further comprising:

an actuator connected to the at least one of the inlet section or the outlet section; and

a duct control module configured to trigger the actuator to change the shape of the at least one of the inlet section or the outlet section as a function of a mode of operation of the VTOL vehicle.

10. The ducted fan of claim 9, wherein the at least one of the inlet section or the outlet section is biased into a first shape and the actuator comprises at least one of a pneumatic actuator configured to change the at least one of the inlet or outlet sections from the first shape to a second shape or a piezoelectric material operatively connected to the at least one of the inlet or outlet sections and configured to change the at least one of the inlet or outlet sections from the first shape to a second shape in response to electricity.

11. The ducted fan of claim 9, wherein the at least one of the inlet section or the outlet section comprises a smart material and the actuator comprises one of an electrical, thermal, or magnetic actuator.

12. The ducted fan of claim 9, wherein the at least one of the inlet section or the outlet section comprises a plurality of overlapping vanes and the actuator comprises a ring surrounding the vanes, wherein the duct control module displaces the ring to change the section from a first shape to a second shape.

13. The ducted fan of claim 9, wherein the actuator comprises at least one of a pneumatic, an electrical, a thermal, a magnetic, a mechanical, a electromechanical, or a piezoelectric actuator.

14. The ducted fan of claim 1, wherein the at least one of the inlet section or the outlet section is configured to actively change into an asymmetrical shape along a longitudinal axis of the annular duct as a function of a mode of operation of the VTOL vehicle.

15. The ducted fan of claim 1, wherein the outlet section is configured to change shape to change a trajectory of the ducted fan in at least one mode of operation of the VTOL vehicle.

16. A vertical take-off and landing (VTOL) vehicle comprising:

an engine; and

at least one ducted fan comprising;

a rotor fan operatively connected to the engine; and

an annular duct surrounding the fan and comprising an inlet section and an outlet section on opposing sides of the fan,

wherein at least one of the inlet section or the outlet section is configured to change shape as a function of a mode of operation of the VTOL vehicle.

17. The VTOL vehicle of claim 16, further comprising an actuator configured to be triggered to change the shape of at least one of the inlet section or the outlet section as a function of a mode of operation of the VTOL vehicle.

18. A method comprising:

determining a flight mode of a vertical take-off and landing (VTOL) vehicle to which a ducted fan is operatively connected;

determining a shape for at least one of an inlet section or an outlet section of a duct of the ducted fan as a function of the flight mode; and

changing the at least one of the inlet section or the outlet section of the duct of the ducted fan to the shape.

19. The method of claim 18, further comprising changing a shape of the outlet section to change a trajectory of the ducted fan in at least one mode of operation of the VTOL vehicle.

20. The method of claim 18, wherein changing the at least one of the inlet section or the outlet section of the duct of the ducted fan to the shape comprises controlling an actuator connected to the at least one of the inlet section or the outlet section to change the shape of the at least one of the inlet section or the outlet section.