Actuators for flow control at surfaces of aerodynamic profiles

Abstract

An assembly for arrangement to the surface of an aerodynamic profile comprises an array of actuators, which are designed as piezo actuators and plasma actuators.

Claims

1. An assembly for arrangement in or at a surface of an aerodynamic profile, wherein the assembly comprises: an array of piezo actuators; an array of plasma actuators; and an arrangement of surface elements on a surface of the assembly; wherein the arrangement of surface elements forms a brush-like structure from first surface elements having a first resonant frequency and second surface elements having a second resonant frequency different from the first resonant frequency; or wherein the arrangement of surface elements includes first surface elements having a first module of elasticity and second surface elements having a second module of elasticity different from the first module of elasticity, and wherein the arrangement of surface elements is provided to create shear forces by a varying vibration dampening.

2. The assembly according to claim 1, wherein the plasma actuators are miniaturized.

3. The assembly according to claim 2, wherein the plasma actuators are SDBD or MEE actuators.

4. The assembly according to claim 1, wherein the arrays of piezo and plasma actuators comprise at least 10000 actuators per square meter.

5. The assembly according to claim 1, wherein the arrangement of surface elements forms the brush-like structure further comprises third surface elements having a third resonant frequency different from the first and second resonant frequencies.

6. The assembly according to claim 1, wherein the arrangement of surface elements includes third surface elements having a third module of elasticity different from the first and second modules of elasticity.

7. The assembly according to claim 1, wherein the array of plasma actuators includes at least a pair of two piezo actuators mechanically coupled with each other for creating a piezo transformer.

8. The assembly according to claim 1, wherein individual plasma actuators from the array of plasma actuators are arranged alternatingly with individual piezo actuators from the array of piezo actuators.

9. A foil comprising one or more assemblies according to claim 1 embedded within the foil.

10. The assembly according to claim 1, wherein sets of at least two individual plasma actuators from the array of plasma actuators are arranged alternatingly with sets of at least two individual piezo actuators from the array of piezo actuators.

11. The assembly according to claim 1, wherein at least one plasma actuator in the array of plasma actuators includes a first electrode and a second electrode, and wherein the first electrode forms one of the piezo actuators in the array of piezo actuators.

12. The assembly according to claim 1, wherein each plasma actuator in the array of plasma actuators includes a first electrode and a second electrode, and wherein the electrodes in each plasma actuator in the array of plasma actuators are co-planar with the array of piezo actuators.

13. The assembly according to claim 12 wherein each first electrode and each second electrode is directly adjacent to a piezo actuator in the array of piezo actuators.

14. The assembly according to claim 1 wherein the assembly has a top side and a bottom side, wherein each plasma actuator in the array of plasma actuators is located on the top side of the assembly, and wherein each piezo actuator in the array of piezo actuators is located on the bottom side of the assembly.

15. The assembly according to claim 14 wherein the arrangement of surface elements is on the surface of the top side of the assembly.

16. The assembly according to claim 1, wherein the arrangement of surface elements forms a brush-like structure configured to create a longitudinal force in a direction parallel to a plane defined by the surface of the assembly.

17. A method for measuring an operating parameter, the method comprising: arranging an assembly on a surface of an aerodynamic profile, the assembly comprising: an array of piezo actuators; an array of plasma actuators; and an arrangement of surface elements on a surface of the assembly; and using a selected actuator to measure a local aerodynamic parameter; wherein the arrangement of surface elements forms a brush-like structure from first surface elements having a first resonant frequency and second surface elements having a second resonant frequency different from the first resonant frequency; or wherein the arrangement of surface elements includes first surface elements having a first module of elasticity and second surface elements having a second module of elasticity different from the first module of elasticity, and wherein the arrangement of surface elements is provided to create shear forces by a varying vibration dampening.

18. The method of claim 17, wherein using the selected actuator to measure the local aerodynamic parameter comprises measuring compressive or shear forces.

19. The method of claim 17, wherein using the selected actuator to measure the local aerodynamic parameter comprises measuring temperatures.

20. The method of claim 17, wherein using the selected actuator to measure the local aerodynamic parameter comprises measuring flow conditions.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) In the following, the invention is further explained on the basis of graphically presented embodiments, from which further advantages and features are apparent. It is shown:

(2) FIG. 1 shows an aerodynamic profile with an assembly embedded into a foil arranged on its surface;

(3) FIG. 2 a piezo actuator with a brush-like structure for achieving a resonance effect;

(4) FIG. 3 a piezo actuator with an arrangement of materials having different modules of elasticity to create shear forces by a varying vibration dampening;

(5) FIG. 4 a piezo actuator having a brush-like structure for creating longitudinal forces;

(6) FIG. 5 a piezo actuator with an embedded hard material such as ceramics to create shear and torsion forces from the bending vibration of the piezo actuator;

(7) FIG. 6 an assembly having an array of 8×11 actuators on the top side;

(8) FIG. 7 a schematic illustration of a plasma actuator having two electrodes;

(9) FIG. 8 an assembly having two plasma actuators and a piezo actuator (piezo element) arranged on the top side;

(10) FIG. 9 an assembly having an array of surface elements from three different materials;

(11) FIG. 10 an assembly having two plasma actuators and a piezo actuator;

(12) FIG. 11 a schematic illustration of a plasma actuator, wherein the upper electrode represents a piezo element at the same time;

(13) FIG. 12 an assembly having a plasma actuator and a piezo actuator as well as an array of surface elements from three different materials;

(14) FIG. 13 a sectional view of an assembly having MEMS plasma actuators (DBD elements) in a coplanar arrangement, wherein the DBD elements alternate with piezo actuators;

(15) FIG. 14 a sectional view of an assembly having coplanar (microscopic, i.e. MEMS) DBD elements and macroscopic piezo actuators at the bottom side; and

(16) FIG. 15 a sectional view of an assembly having miniaturized (microscopic) coplanar DBD elements and macroscopic piezo actuators at the bottom side, wherein at the top side of the assembly an arrangement of materials with different acoustic characteristics is provided.

DETAILED DESCRIPTION

(17) In FIG. 1 an aerodynamic profile P having a foil F is shown, into which an assembly having plasma actuators and piezo actuators is embedded. The flow of a surrounding air flow is illustrated by arrows.

(18) FIG. 2 shows an assembly having a piezo actuator. In the surface of a substrate surface elements are provided, which comprise different resonance frequencies A, B and C.

(19) In the assembly illustrated in FIG. 3 a piezo actuator is provided underneath a substrate, wherein surface elements from different materials are provided at the substrate surface, the surface elements accordingly comprising different vibration amplitudes, when they are excited by the actuator.

(20) A similar assembly is illustrated in FIG. 4, wherein, however, groups of surface elements are provided for achieving a force action in a longitudinal direction (direction of the arrow).

(21) In the assembly of FIG. 5, six bar-shaped ceramics components are embedded into the surface.

(22) FIG. 6 shows an assembly having a regular array of 6×8 actuators (piezo and plasma actuators);

(23) FIG. 7 schematically shows a plasma actuator (DBD actuator) having a dielectric and two electrodes, wherein electrode 1 is provided at the top side and electrode 2 at the bottom side.

(24) In the assembly shown in FIG. 8 two plasma actuators (with electrodes 1a, 2a and 1b, 2b respectively) are provided. Furthermore, a piezo actuator is provided on the top side of the dielectric.

(25) FIG. 9 shows an assembly having a piezo actuator at the bottom side of a substrate, wherein on the surface of the substrate a regular array from three different materials A, B and C is created with different vibration characteristics or acoustic characteristics.

(26) FIG. 10 shows an assembly having two plasma actuators (electrodes 1a, 2a and 1b, 2b respectively) as well as a piezo actuator on the bottom side.

(27) FIG. 11 shows a schematical illustration of a plasma actuator having two electrodes 1 and 2, wherein the electrode 1 at the same time constitutes a piezo element (indicated by a thickening of the electrode 1).

(28) The FIGS. 12, 13 and 14 were explained already further above.

(29) FIG. 15 shows an assembly having a plasma actuator (electrodes 1 and 2) and a piezo actuator at the bottom side. A regular array from three different materials A, B and C having different characteristics (e.g. acoustic or vibration characteristics) is provided on the surface.

(30) While at least one exemplary embodiment has been presented in the foregoing detailed description, it should be appreciated that a vast number of variations exist. It should also be appreciated that the exemplary embodiment or embodiments described herein are not intended to limit the scope, applicability, or configuration of the claimed subject matter in any way. Rather, the foregoing detailed description will provide those skilled in the art with a convenient road map for implementing the described embodiment or embodiments. It should be understood that various changes can be made in the function and arrangement of elements without departing from the scope defined by the claims, which includes known equivalents and foreseeable equivalents at the time of filing this patent application.