Aircraft or spacecraft fluidic oscillator device

Patent metadata

Field	Value
Publication number	US-10647416-B2
Application number	US-201615386866-A
Country	US
Kind code	B2
Filing date	Dec 21, 2016
Priority date	Dec 22, 2015
Publication date	May 12, 2020
Grant date	May 12, 2020

Abstract

A fluidic oscillator device, in particular for a or in a flow control system for an aircraft or spacecraft, has a first and a second fluidic actuator, wherein each of the actuators has an inlet for supplying pressure and a first and a second outlet, from which an actuator flow can be discharged. The device further has a fluidic control for controlling an oscillating discharge of the actuator flow from the first and second outlet of the actuators, wherein the control has a connection portion which is arranged between the first actuator and the second actuator.

First claim

The invention claimed is:

1. An aircraft or Spacecraft fluidic oscillator device for or in a flow control system, the device comprising: a first fluidic actuator and an adjacent second fluidic actuator, wherein each of the actuators has an inlet for supplying pressure and a first and a second outlet, from which an actuator flow is discharged; and a fluidic control for controlling an oscillating discharge of the actuator flow from the first and second outlet of the actuators, wherein the control has a connection portion configured as a flat part which is arranged between the first actuator and the second actuator, wherein the control is devoid of a feedback line external to the connection portion.

2. The fluidic oscillator device of claim 1 , wherein the control comprises a control channel in each actuator, wherein a control flow, which is guided through the control channel, determines a respectively active outlet of the actuator, wherein the control channels at the actuators respectively have first and second junctions and wherein the connection portion has a first and a second connection channel which fluidically interconnect the junctions of the control channels.

3. The fluidic oscillator device of claim 2 , wherein the connection portion also has a bypass channel which provides a fluidic connection between the first and the second connection channel and is configured such that the actuators and the control are operated at a common oscillation frequency.

4. The fluidic oscillator device of claim 2 , wherein one or both of the actuators are configured as flat parts with opposing planar faces.

5. The fluidic oscillator device of claim 4 , wherein the flat parts are stacked in a direction perpendicular to the planar faces in a force-locking manner.

6. The fluidic oscillator device of claim 4 , wherein the bypass channel is configured as a groove which is introduced into the connection portion.

7. The fluidic oscillator device of claim 6 , wherein the groove runs in a first planar side and in a second planar side of the connection portion, a passage being provided through the connection portion.

8. The fluidic oscillator device of claim 2 , wherein the bypass channel comprises at least one curve.

9. The fluidic oscillator device of claim 8 , wherein the bypass channel comprises a plurality of curves which are arranged in a serpentine-like manner.

10. The fluidic oscillator device of claim 4 , wherein the first junction of the control channel is arranged on a first planar face of the respective actuator and the second junction of the control channel is arranged on a second planar face of the respective actuator.

11. The fluidic oscillator device of claim 2 , wherein the first junction of the control channel of the first actuator is connected by the first connection channel of the connection portion to the first junction of the control channel of the second actuator.

12. The fluidic oscillator device of claim 11 , wherein the second junction of the control channel of the first actuator is connected by the second connection channel of the connection portion to the second junction of the control channel of the second actuator.

13. The fluidic oscillator device of claim 11 , wherein the first connection channel leads through the connection portion in a first planar side of the connection portion.

14. The fluidic oscillator device of claim 12 , wherein the second connection channel leads through the connection portion in a second planar side of the connection portion.

15. The fluidic oscillator device of claim 2 , wherein the first junction of the control channel of the first actuator is connected by the first connection channel of the connection portion to the second junction of the control channel of the second actuator.

16. The fluidic oscillator device of claim 15 , wherein the second junction of the control channel of the first actuator is connected by the second connection channel of the connection portion to the first junction of the control channel of the second actuator.

17. The fluidic oscillator device of claim 15 , wherein the first connection channel leads through the connection portion from a first planar side of the connection portion to a second planar side.

18. The fluidic oscillator device of claim 16 , wherein the second connection channel leads through the connection portion from the second flat side of the connection portion to the first flat side.

19. The fluidic oscillator device of claim 1 , wherein at least a third fluidic actuator and at least a second connection portion are provided, wherein the second connection portion is arranged between the second actuator and the third actuator and fluidically interconnects them.

20. The fluidic oscillator device of claim 19 , comprising a plurality of further fluidic actuators and a plurality of further connection portions, wherein a respectively one of the further connection portions is arranged between respectively two of the further actuators and fluidically interconnects them.

21. The fluidic oscillator device of claim 1 , wherein, for at least one of the actuators, one of the first or the second outlet has a start outlet configuration which allows the actuator flow to discharge at least mainly through the one outlet at a beginning of a pressurization of the actuator.

22. The fluidic oscillator device of claim 21 , wherein the start outlet configuration comprises a lower fluidic resistance than the configuration of the other outlet of the actuator.

23. The fluidic oscillator device of claim 22 , wherein the start outlet configuration comprises a larger passable cross section than the configuration of another outlet of the actuator.

Assignees

• Airbus Defence & Space Gmbh

Inventors

• Bauer Karin
• Blechschmidt Markus
• Schwarz Sebastian
• Langenbacher Peter

Classifications

• B64C21/02

  by use of slot, ducts, porous areas or the like · CPC title

• F05B2210/30

  Flow characteristics · CPC title

• B64C21/06

  for sucking (BLI propulsion B64C21/01) · CPC title

• B64C21/08 Primary

  adjustable · CPC title

• Y02T50/166

  Cross-Sectional Technologies · mapped topic