Vortex generator apparatus for an aircraft

Patent metadata

Field	Value
Publication number	US-11643190-B2
Application number	US-202117159829-A
Country	US
Kind code	B2
Filing date	Jan 27, 2021
Priority date	Jan 30, 2020
Publication date	May 9, 2023
Grant date	May 9, 2023

Abstract

A vortex generator apparatus for an aircraft includes a surface section having a receiving recess, a vortex generator having a first edge, an opposite second edge and a vortex generator surface component extending from the first edge to the second edge, wherein the first edge is fixedly arranged in or adjacent to the receiving recess. The vortex generator surface component includes at least one electroactive polymer assembly, wherein the at least one electroactive polymer is switchable into an extended state by applying an electrical voltage and into a neutral state by removing the electrical voltage. The electroactive polymer assembly and the vortex generator surface component are configured to retract the vortex generator surface component completely into the receiving recess in the neutral state of the electroactive polymer assembly and to extend the vortex generator surface component from the receiving recess in the extended state.

First claim

The invention claimed is:

1. A vortex generator apparatus for an aircraft, comprising:
a surface section having a receiving recess,
a vortex generator having a first edge, second edge and a vortex generator surface component extending from the first edge to the second edge,
wherein the first edge is fixedly arranged in or adjacent to the receiving recess,
wherein the vortex generator surface component comprises at least one electroactive polymer assembly comprising an electroactive polymer,
wherein the at least one electroactive polymer assembly is switchable into an extended state by applying an electrical voltage and into a neutral state by removing the electrical voltage, and
wherein the at least one electroactive polymer assembly and the vortex generator surface component are configured to retract the vortex generator surface component completely into the receiving recess in the neutral state of the at least one electroactive polymer assembly and to extend the vortex generator surface component from the receiving recess in the extended state, and
wherein the electroactive polymer extends from the receiving recess in the extended state and retracts into the receiving recess in the neutral state.

2. The vortex generator apparatus of claim 1 , wherein the receiving recess is dimensioned to flushly receive the vortex generator surface component.

3. The vortex generator apparatus of claim 1 , wherein the vortex generator surface component comprises a predetermined bending region which is positioned to cause the vortex generator surface component to flushly fit into the recess in a retracted state.

4. The vortex generator apparatus of claim 1 , wherein the vortex generator surface component is configured to move about an angle of at least 45° from a retracted state to the extended state.

5. The vortex generator apparatus of claim 1 , further comprising a vortex generator actuator comprising a voltage source and a controller, wherein the controller is configured to selectively provide the electrical voltage from the voltage source to the at least one electroactive polymer assembly.

6. The vortex generator apparatus of claim 5 , wherein the controller is configured to generate an AC voltage with a variable waveform as the electrical voltage.

7. The vortex generator apparatus of claim 1 ,
further comprising a bending sensor arranged in the vortex generator surface component, and
wherein the bending sensor is configured to provide an electric signal that depends on an actual bending of the vortex generator surface component.

8. The vortex generator apparatus of claim 7 , wherein the bending sensor comprises a separate electroactive polymer sensor, a strain gauge sensor or is provided by the at least one electroactive polymer assembly.

9. The vortex generator apparatus of claim 5 ,
further comprising a bending sensor arranged in the vortex generator surface component,
wherein the bending sensor is configured to provide an electric signal that depends on an actual bending of the vortex generator surface component,
wherein the controller is configured to receive the electric signal, and
wherein the controller is configured to determine a bending degree of the at least one electroactive polymer assembly from the received electric signal.

10. The vortex generator apparatus of claim 9 , wherein the controller is configured to influence the electrical voltage depending on the bending degree and an external vortex generator deployment command.

11. An aircraft, comprising:
a fuselage,
at least one flow body, and
at least one vortex generator apparatus arranged according to claim 1 upstream of the at least one flow body.

12. The aircraft according to claim 11 , wherein the at least one flow body comprises a vertical tail plane.

13. The aircraft according to claim 11 , wherein the at least one flow body comprises a movable flow body attached to the wing.

Assignees

• Airbus Operations Gmbh

Inventors

• Linde Peter
• Hegenbart Matthias
• Benthien Hermann

Classifications

• B64C23/06 Primary

  by generating vortices · CPC title

• B64C23/076 Primary

  the wing tip airfoil devices comprising one or more separate moveable members thereon affecting the vortices, e.g. flaps · CPC title

• Y02T50/10

  Drag reduction · CPC title