Ducted Fans with Flow Control Synthetic Jet Actuators and Methods for Ducted Fan Force and Moment Control

• US 20100140416A1
• Filed: 11/03/2009
• Published: 06/10/2010
• Est. Priority Date: 11/03/2008
• Status: Abandoned Application

• Current Assignee: Adam Lee Entsminger, Etan Karni, Osgar John Iii Ohanian, Paul A. Gelhausen, William Kelly Londenberg
• Original Assignee: Adam Lee Entsminger, Etan Karni, Osgar John Iii Ohanian, Paul A. Gelhausen, William Kelly Londenberg
• Inventors: Karni, Etan, Entsminger, Adam Lee, Ohanian, Osgar John III, Gelhausen, Paul A., Londenberg, William Kelly
• Application Number:
  US12/611,463
• Publication Number:
  US 20100140416A1
• Time in Patent Office: Days
• US Class Current: 244/23.A
• CPC Class Codes: B64C 21/04 for blowing
• CPC Class Codes: B64C 29/02 having its flight directional axis vertical when grounded
• 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
• CPC Class Codes: B64U 50/14 ducted or shrouded
• CPC Class Codes: Y02T 50/10 Drag reduction

Abstract

The present invention relates to the field of aerodynamics. More particularly, the present invention relates to manipulating air flow over a surface, such as the surface of a duct of a ducted fan vehicle. By controlling air flow over, at, or around the surface of a duct, the flight of the vehicle can be controlled. One embodiment of the invention provides a vertical take-off and landing (VTOL) ducted-fan vehicle comprising means for producing steady or unsteady blowing at a surface of a duct for producing control forces and moments for controlling flight. The means for unsteady blowing can be provided by synthetic jets and the means for steady blowing can be provided by a pressurized air supply. The synthetic jets can be integrated into the ducted-fan vehicles in numerous ways, including at the surface of the leading and/or trailing edge of the ducts. The synthetic jets can be independently operated to control the flight of the vehicle. A novel use of these inventive flow control concepts is to apply the control asymmetrically to the duct in order to produce an imbalance in forces, thus resulting in a moment or torque, which can be used to control flight.

Claims

1. An apparatus for causing separation between a surface of a ducted fan and a fluid flow comprising:

a ducted fan having a duct with a leading edge surface;

one or more slots in the leading edge surface disposed around a circumference of the leading edge surface, wherein each slot is an opening for an orifice;

an orifice associated with each slot and operably connected thereto;

a cavity associated with each orifice and operably connected thereto;

at least one steady or synthetic jet operably associated with each cavity and capable of being individually actuated to blow a flow out of the cavity, through the orifice, and through the slot;

such that during operation the flow from each slot is capable of causing a separation between the leading edge surface and a flow entering the duct;

and such that during operation the jets are capable of being actuated asymmetrically around the leading edge surface to produce control forces and moments.

2. The apparatus of claim 1, wherein the slots comprise about 75% of the circumference around which the slots are arranged.

3. The apparatus of claim 1, further comprising a synthetic jet geometry:

wherein the duct has an inside diameter and the slots are rectangular, have a width ranging from about 0.2% to about 0.5% of the duct inside diameter, and have a length ranging from about 5% to about 8% of the duct inside diameter;

wherein the cavities have a diameter ranging from about 8% to about 10% of the duct inside diameter, and a width ranging from about 5% to about 8% of the cavity diameter; and

wherein the orifices have a depth of about 10% of the cavity diameter, a width ranging from about 0.2% to about 0.5% of the duct inside diameter, and a length ranging from about 5% to about 8% of the duct inside diameter.

4. The apparatus of claim 1, wherein the orifices are oriented at about 45°

relative to the leading edge surface, such that during operation the flow from the slots is capable of opposing, at about 45°

, the flow entering the duct.

5. The apparatus of claim 1, wherein the ducted fan is capable of providing propulsion to a vehicle.

6. The apparatus of claim 1, wherein the jets are synthetic jets capable of providing unsteady blowing.

7. The apparatus of claim 6, wherein each synthetic jet comprises a piezoelectric diaphragm with an active surface forming a wall of the cavity.

8. The apparatus of claim 7, wherein the jets are capable of producing a lateral flow whereby the flow from each slot, while in the cavity, is parallel to the active surface of the piezoelectric diaphragm.

9. An apparatus for causing attachment between a surface of a ducted fan and a fluid flow comprising:

a ducted fan having a trailing edge region comprising an inner duct surface and a Coanda surface;

one or more slots in the trailing edge region disposed around a circumference of the Coanda surface, wherein each slot is an opening for an orifice;

an orifice associated with each slot and operably connected thereto;

a cavity associated with each orifice and operably connected thereto;

at least one steady or synthetic jet operably associated with each cavity and capable of being individually actuated to blow a flow out of the cavity, through the orifice, and through the slot;

such that during operation the flow from each slot is capable of causing a Coanda effect in a flow exiting the duct, whereby the flow exiting the duct has a tendency to attach to the Coanda surface;

and such that during operation the jets are capable of being actuated asymmetrically around the circumference to produce control forces and moments.

10. The apparatus of claim 9, wherein the slots comprise about 85% of the circumference around which the slots are arranged.

11. The apparatus of claim 9, further comprising a synthetic jet geometry:

wherein the duct has an inside diameter and the slots are rectangular or curved to follow the Coanda surface circumference, have a width ranging from about 0.2% to about 0.5% of the duct inside diameter, and have a length ranging from about 5% to about 8% of the duct inside diameter;

wherein the cavities have a diameter ranging from about 8% to about 10% of the duct inside diameter, and a width ranging from about 5% to about 8% of the cavity diameter; and

wherein the orifices have a depth of about 10% of the cavity diameter, a width ranging from about 0.2% to about 0.5% of the duct inside diameter, and a length ranging from about 5% to about 8% of the duct inside diameter.

12. The apparatus of claim 9, wherein the orifices are disposed under and parallel to the inner duct surface to deliver, during operation, the flow from each slot in a direction tangential to the Coanda surface and the flow exiting the duct.

13. The apparatus of claim 9, wherein the jets are synthetic jets capable of providing unsteady blowing.

14. The apparatus of claim 13, wherein each synthetic jet comprises a piezoelectric diaphragm with an active surface forming a wall of the cavity.

15. The apparatus of claim 14, wherein the synthetic jets produce lateral blowing whereby the flow from the slots, while in the cavity, is parallel to the active surface of the piezoelectric diaphragm.

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

a ducted fan with a duct having a leading edge surface and a trailing edge region with an inner duct surface and a Coanda surface;

one or more slots in the leading edge surface, and optionally or alternatively in the trailing edge region, disposed around a circumference of the leading edge surface or Coanda surface, wherein each slot is an opening for an orifice;

an orifice associated with each slot and operably connected thereto;

a cavity associated with each orifice and operably connected thereto;

at least one steady or synthetic jet operably associated with each cavity and capable of being individually actuated to blow a flow out of the cavity, through the orifice, and through the slot;

such that during operation the flow from each slot in the leading edge surface is capable of causing a separation between the leading edge surface and a flow entering the duct, and the flow from each slot in the trailing edge region is capable of causing a Coanda effect in a flow exiting the duct, whereby the flow exiting the duct has a tendency to attach to the Coanda surface;

and such that during operation the jets are capable of being actuated asymmetrically around the leading edge surface or Coanda surface to produce control forces and moments for flight control.

17. The ducted-fan vehicle of claim 16, wherein the ducted fan is capable of providing propulsion.

18. The ducted-fan vehicle of claim 16, wherein the synthetic jets comprise piezo diaphragms.

19. A method of flight control of a ducted-fan vehicle comprising:

deterring a flow entering a duct of a ducted-fan vehicle from attaching to a leading edge surface of the duct; and

optionally or alternatively inducing a flow exiting the duct to attach to a Coanda surface of the duct;

by actuating synthetic jets incorporated into the leading edge surface or Coanda surface to produce unsteady blowing and cause control forces and moments for controlling flight of the ducted-fan vehicle.

20. The method of claim 19, wherein the jets are arranged to produce unsteady blowing at about a 45°

angle relative to the leading edge surface.