Fluid Boundary Layer Control

• US 20160009364A1
• Filed: 02/22/2014
• Published: 01/14/2016
• Est. Priority Date: 02/23/2013
• Status: Abandoned Application

• Current Assignee: VIRES Aeronautics, Inc.
• Original Assignee: VIRES Aeronautics, Inc.
• Inventors: Goel, Harshil
• Application Number:
  US14/187,260
• Publication Number:
  US 20160009364A1
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: B64C 1/38 Constructions adapted to reduce effects of aerodynamic or other external heating
• CPC Class Codes: B64C 23/08 using Magnus effect
• CPC Class Codes: B64C 3/141 Circulation Control Airfoils
• CPC Class Codes: Y02T 50/10 Drag reduction

Abstract

The lift and drag performance of all vehicles is strongly influenced by viscous effects, and in turn, laminar separation bubbles. This application employs an effective fluid boundary layer control strategy that reduces parasitic drag, allows for more usable angles of attack, and delays or stops separation. In the approach of this application, the control surface effectively uses the Magnus effect to delay or stop a separation bubble from forming, which can increase lift, reduce drag, and delay degrees of stall by directly manipulating the velocity gradient in the fluid boundary layer.

Claims

1. An apparatus adapted to control flow of a fluid boundary layer, comprising:

an aircraft wing housing, having a chord length, a leading edge and a trailing edge;

at least one bearing element, disposed on an interior portion of the aircraft wing housing, disposed between a first endplate and a second endplate, substantially parallel to the chord length of the aircraft wing housing;

at least one rod member, adapted to fit into the at least one bearing element, extending substantially perpendicular to the chord length of the aircraft wing housing, and;

a rotational belt, disposed on an outer surface of the aircraft wing housing, having an inner surface comprising a first coefficient of friction and an outer surface comprising a second coefficient of friction, wherein the inner surface is operationally coupled to the at least one rod member and the outer surface of the rotational belt is in mechanical contact with the fluid boundary layer.

2. The apparatus of claim 1, further comprising a power source, wherein the power source is adapted to deliver a rotational force to the at least one rod member.

3. The apparatus of claim 1, wherein the rotational belt is actuated when a tangential velocity of an airstream at the fluid boundary layer exceeds a predetermined velocity operating on the outer surface of the rotational belt, wherein the predetermined velocity is determined at least in part by the second coefficient of friction, such that a rotational inertia of the rotational belt is overcome, thereby actuating the rotational belt.

4. The apparatus of claim 2, wherein the rotational belt is actuated when the power source operates to provide rotational force to the at least one rod member.

5. The apparatus of claim 4, further comprising:

a velocity gradient sensor element operatively coupled to the aircraft wing housing; and

a microprocessor element,

wherein the velocity gradient sensor element detects a velocity gradient at the fluid boundary layer and transmits a detected velocity gradient to the microprocessor element.

6. The apparatus of claim 5, wherein the microprocessor element is operatively coupled to the power source and operates to control the delivered rotational force from the power source to the at least one rod member.

7. The apparatus of claim 5, further comprising an accelerometer operatively coupled to the microprocessor.

8. A method of controlling a fluid velocity at a fluid boundary layer of a plane on a surface of a housing, comprising the steps of:

determining an initial fluid velocity at the fluid boundary layer of the plane;

providing at least one bearing element, operatively coupled to at least one rod member, disposed on an interior portion of the housing;

providing a rotational belt, operatively coupled to the at least one rod member;

providing a power source, mechanically coupled to the at least one rod member, wherein the power source operates to deliver a rotational force to the at least one rod member; and

rotating the rotational belt at a control velocity.

9. An apparatus for controlling a fluid boundary layer of at least a portion of a vehicle body surface, comprising:

a vehicle body surface housing;

at least one bearing element, disposed on an interior portion of the vehicle body surface housing, disposed between a first endplate and a second endplate;

at least one rod member, adapted to fit into the at least one bearing element; and

a rotational belt, disposed on an outer surface of the vehicle body surface housing, having an inner surface comprising a first coefficient of friction and an outer surface comprising a second coefficient of friction, wherein the inner surface is operationally coupled to the at least one rod member and the outer surface of the rotational belt is in mechanical contact with the fluid boundary layer.

10. The apparatus of claim 9, further comprising a power source, wherein the power source is adapted to deliver rotational force to the at least one rod member thereby rotating the rotational belt.

11. The apparatus of claim 9, wherein the rotational belt is actuated when a tangential velocity of a fluid stream at the fluid boundary layer exceeds a predetermined velocity operating on the outer surface of the rotational belt, wherein the predetermined velocity is determined in part by the second coefficient of friction, such that a rotational inertia of the rotational belt is overcome, thereby actuating the rotational belt circumferentially.

12. The apparatus of claim 10, wherein the rotational belt is actuated when the power source operates to provide rotational force to the at least one rod member.

13. The apparatus of claim 12, further comprising:

a velocity gradient sensor element operatively coupled to the vehicle body surface housing; and

a microprocessor element,

wherein the velocity gradient sensor element detects a velocity gradient at the fluid boundary layer and transmits a detected velocity gradient to the microprocessor element.

14. The apparatus of claim 13, wherein the microprocessor element is operatively coupled to the power source and operates to variably control the delivered rotational force from the power source to the at least one rod member.

15. An apparatus for controlling at least one of a thermal property or an acoustic property at a fluid boundary layer of at least a portion of a vehicle body surface, comprising:

a vehicle body surface housing;

at least one bearing element, disposed on an interior portion of the vehicle body surface housing, disposed between a first endplate and a second endplate;

at least one rod member, adapted to fit into the at least one bearing element;

a rotational belt, disposed on an outer surface of the vehicle body surface housing, having an inner surface comprising a first coefficient of friction and an outer surface comprising a second coefficient of friction, wherein the inner surface is operationally coupled to the at least one rod member and the outer surface of the rotational belt is in mechanical contact with the fluid boundary layer; and

at least one of;

a thermal sensor, operatively coupled to the vehicle body surface housing, adapted to detect at least one thermal property of the vehicle body surface housing, or

an acoustic sensor, operatively coupled to the vehicle body surface housing, adapted to detect at least one acoustic property of the vehicle body surface housing.

16. The apparatus of claim 15, further comprising a power source, wherein the power source is adapted to deliver rotational force to the at least one rod member thereby rotating the rotational belt.

17. The apparatus of claim 15, wherein the rotational belt is actuated when a tangential velocity of a fluid stream at the fluid boundary layer exceeds a predetermined velocity operating on the outer surface of the rotational belt, wherein the predetermined velocity is determined in part by the second coefficient of friction, such that a rotational inertia of the rotational belt is overcome, thereby actuating the rotational belt circumferentially.

18. The apparatus of claim 16, wherein the rotational belt is actuated when the power source operates to provide rotational force to the at least one rod member.

19. The apparatus of claim 18, further comprising a microprocessor element, wherein the at least one thermal sensor or the at least one acoustic sensor transmits the detected at least one thermal property or at least one acoustic property, respectively, of the vehicle body surface housing to the microprocessor element.

20. The apparatus of claim 19, wherein the microprocessor element is operatively coupled to the power source and operates to variably control the delivered rotational force from the power source to the at least one rod member, thereby controlling the at least one thermal property or the at least one acoustic property of the vehicle body surface housing.