Active flow control systems and methods for aircraft
US-2019248475-A1 · Aug 15, 2019 · US
US10988239B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10988239-B2 |
| Application number | US-201715653557-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jul 19, 2017 |
| Priority date | Oct 27, 2011 |
| Publication date | Apr 27, 2021 |
| Grant date | Apr 27, 2021 |
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An active separation control system, comprising a fluidic oscillatory actuator having an ejector member, an oscillator member, and a joining channel between said oscillator member and said ejector member, all mounted on at least one flexible member, said fluidic oscillatory actuator being mountable on a rotatable door of a vehicle such that said flexible member assumes a different shape when said door is closed than when said door is open, wherein said joining channel is also flexible to assume a shape of said flexible member.
Opening claim text (preview).
What is claimed is: 1. An active separation control system, comprising: a fluidic oscillatory actuator having an ejector member, an oscillator member, and a joining channel between said oscillator member and said ejector member, said fluidic oscillatory actuator, said oscillator member and said joining channel being mounted on at least one flexible member, said fluidic oscillatory actuator being mountable on a rotatable door of a vehicle such that said flexible member assumes a different shape when said door is closed than when said door is open, wherein said joining channel is also flexible to assume a shape of said flexible member. 2. The system of claim 1 , comprising at least two flexible members wherein said ejector member is attached at an inner part of one flexible member and said oscillator member is attached at an inner part of another flexible member. 3. The system of claim 1 , wherein said fluidic oscillatory actuator has a pair of control ports at opposite sides of said joining channel, and a feedback conduit directly connecting said control ports to each other. 4. The system of claim 3 , wherein said feedback conduit is flexible. 5. The system of claim 1 , wherein there is a plurality of fluidic oscillatory actuators, wherein the system comprises a synchronization conduit, and wherein said synchronization conduit is mounted on said flexible member to connect at least two of said actuators such as to effect synchronization between oscillations in said at least two actuators. 6. The system of claim 5 , wherein said synchronization conduit is flexible. 7. The system of claim 5 , wherein said synchronization conduit is effective to provide said synchronization devoid of any moving non-fluidic parts. 8. The system of claim 5 , wherein each oscillatory actuator comprises two opposing control ports, and wherein each control port of each oscillatory actuator is respectively connected to at least two control ports of at least two another oscillatory actuators. 9. The system of claim 5 , wherein each oscillatory actuator comprises two opposing control ports, and wherein each control port of each oscillatory actuator is connected to only one control port of another oscillatory actuator. 10. The system of claim 5 , wherein at least one of said actuator is a suction and oscillatory blowing actuator (SaOB). 11. The system of claim 5 , wherein said synchronization conduit is selected to control phase lag among said actuators. 12. The system of claim 5 , wherein said at least one synchronization conduit is constituted to effect opposite oscillations among at least one pair of oscillatory actuators. 13. The system of claim 5 , wherein a frequency of said oscillatory actuators is X times an expected vortex shedding frequency of fluid at the vicinity of the system, wherein X is from about 1.5 to about 3.5. 14. The system of claim 13 , wherein said X equals 2. 15. The system of claim 5 , wherein a separation between adjacent fluidic oscillatory actuators is about X v St/f, wherein v is an expected velocity of fluid at the vicinity of the system, f is an expected vortex shedding frequency of fluid at the vicinity of the system, St is an expected Strouhal number characterizing fluidic oscillations, and X is from about 0.5 to about 4. 16. The system of claim 5 , wherein said vehicle is a truck trailer. 17. The system of claim 5 , wherein said vehicle is an aeronautical system. 18. A vehicle, comprising: a rotatable door; and an active separation control system comprising: a plurality of fluidic oscillatory actuators, each fluidic oscillatory actuator of said plurality of fluidic oscillatory actuators having an ejector member, an oscillator member, and a joining channel between said oscillator member and said ejector member, wherein said oscillator member, said joining channel and at least one of said plurality of fluidic oscillatory actuators are mounted on at least one flexible member; wherein each fluidic oscillatory actuator is mounted on said rotatable door of the vehicle such that said flexible member assumes a different shape when said door is closed than when said door is open, wherein said joining channel is also flexible to assume a shape of said flexible member, wherein the active separation control system comprises a synchronization conduit, and wherein said synchronization conduit is mounted on said flexible member to connect at least two of said actuators such as to effect synchronization between oscillations in said at least two actuators. 19. A method of controlling air flow at a surface of a vehicle, the method comprising: mounting an active separation control system on a rotatable door of the vehicle, said active separation control system comprising: a fluidic oscillatory actuator having an ejector member, an oscillator member, and a joining channel between said oscillator member and said ejector member, said fluidic oscillatory actuator, said oscillator member and said joining channel being mounted on at least one flexible member, such that said flexible member assumes a different shape when said door is closed than when said door is open, wherein said joining channel is also flexible to assume a shape of said flexible member.
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