BOUNDARY LAYER PROBE, MEASURING ASSEMBLY, AND METHOD FOR DETERMINING A FLUID FLOW

Abstract

The invention relates to a boundary layer probe for determining a fluid flow, comprising a measuring surface which is formed on a probe wall and with which a fluid flow to be determined is in contact during a measuring operation. The boundary layer probe also comprises an assembly of measuring obstacles that are formed in the region of the measuring surface as obstacles which disrupt the fluid flow in a flow region adjacent to the measuring surface, each of which has an elongated obstacle course extending over a particular obstacle length, and which are arranged at substantially equidistant angular distances in the circumferential direction. The boundary layer probe additionally has pressure measuring points, each of which is radially adjacent to an associated obstacle in order to detect a local pressure in the region of the measuring surface. The invention additionally relates to a measuring assembly and to a method for determining a fluid flow. (FIG. 1)

Claims

1. A boundary layer probe for determining a fluid flow, comprising: a measuring surface which is formed on a probe wall and with which a fluid flow to be determined is in contact during a measuring operation; an assembly of measuring obstacles which are formed in the region of the measuring surface as obstacles which disrupt the fluid flow in a flow region adjacent to the measuring surface, each has an elongated obstacle course extending over a particular obstacle length, and are arranged at substantially equidistant angular distances in the circumferential direction; and pressure measuring points, each of which is radially adjacent to an associated obstacle in order to detect a local pressure in the region of the measuring surface.

2. The boundary layer probe according to claim 1, wherein the obstacles are arranged rotationally symmetrically in the region of the measuring surface.

3. The boundary layer probe according to claim 1 wherein the elongated obstacle course extends at least in portions along a curved line.

4. The boundary layer probe according to claim 3, wherein the elongated obstacle course is curved in a concave or convex manner in relation to the center of the assembly of measuring obstacles.

5. The boundary layer probe according to claim 1, wherein distal end portions of adjacent measuring obstacles are arranged adjacent to one another.

6. The boundary layer probe according to claim 5, wherein the distal end portions of the adjacent measuring obstacles are connected to one another.

7. The boundary layer probe according to claim 1, wherein the pressure measuring points are each arranged in a central portion of the associated obstacle.

8. The boundary layer probe according to claim 1, wherein the obstacles are each formed having at least one obstacle shape from the following group: web protruding on the measuring surface and recess arranged on the measuring surface.

9. The boundary layer probe according to claim 1, wherein the assembly of measuring obstacles has at least three obstacles.

10. The boundary layer probe according to claim 1, wherein one or all of the pressure measuring points are each formed having a pressure measuring opening to which a pressure measuring device can be coupled.

11. The boundary layer probe according to measuring point is associated with each of the measuring obstacles.

12. A measuring assembly for determining a fluid flow, comprising a boundary layer probe according to claim 1; a measuring chamber which is configured to receive a flow of a fluid flow to be determined, wherein the flow can flow along a probe wall of the boundary layer probe having a measuring surface formed thereon; and a pressure measuring device which is configured to detect a local pressure at each pressure measuring point in the region of the measuring surface of the boundary layer probe.

13. A method for determining a fluid flow, comprising providing a boundary layer probe according to claim 1; forming a flow of a fluid flow to be determined in a measuring chamber, wherein the flow here flows along a probe wall of the boundary layer probe having a measuring surface formed thereon; recording measured pressure values for a local pressure at pressure measuring points in the region of the measuring surface of the boundary layer probe, wherein here differential pressures are recorded for adjacent pressure measuring points; and determining at least one physical measured variable for a boundary layer of the fluid flow on the measuring surface of the boundary layer probe by evaluating the measured pressure values, wherein the at least one physical measured variable is selected from the following group: flow velocity and wall shear stress.

14. The method according to claim 13, wherein the measured pressure values are recorded in a time-resolved manner.

15. The method according to claim 13, wherein the at least one physical measured variable is determined free of any rotation of the measuring surface having the assembly of measuring obstacles.

Description

DESCRIPTION OF EMBODIMENTS

[0032] Further embodiments are explained in detail below with reference to the drawings, in which:

[0033] FIG. 1 is a schematic representation of measuring surfaces of a boundary layer probe having different assemblies of measuring obstacles;

[0034] FIG. 2 is a schematic representation of one of the measuring surfaces from FIG. 1 and a sectional view thereof;

[0035] FIG. 3 is a schematic representation of further measuring surfaces of a boundary layer probe having different assemblies of measuring obstacles and pressure measuring points;

[0036] FIG. 4 is a schematic representation of differential pressure curves as a function of the angle of rotation; and

[0037] FIG. 5 is a schematic representation for a 4D calibration curve.

[0038] FIG. 1 shows a schematic representation of a measuring surface 1 of a boundary layer probe for determining a fluid flow, in particular the direction of the fluid flow, having different assemblies a), b) and c) of measuring obstacles 2a, 2b, 2c, which are formed as forward-protruding microscopic webs or recesses placed in the measuring surface 1 in such a way that a fluid flow to be determined, which flows past the measuring surface 1, is locally disrupted by the measuring obstacles 2a, 2b, 2c, so that local pressure conditions are established which then can be tapped in pressure measuring points 3a, 3b, 3c, each which is associated with one of the measuring obstacles 2a, 2b, 2c.

[0039] In conjunction with the pressure measuring points 3a, 3b, 3c, it can be provided that each of these is formed having a pressure measuring opening in the region of the measuring surface 1 via which the local pressure can be measured. Alternatively, a particular pressure measuring device can be arranged on the measuring surface 1, for example in the form of a pressure-sensitive film, in order to measure the local pressure.

[0040] In the assembly a) of measuring obstacles 2a, 2b, 2c, said measuring obstacles are rounded in the center by a defined radius R1. An increase in R1 (from left to right in FIG. 1) results in different sensor geometries. The extreme, R1=, creates a triangular obstacle (cf. assembly c)). Furthermore, the variation of the number n.sub.s of the measuring obstacles 2a, 2b, 2c can be provided. Infinite radii would then lead to n-cornered obstacles. An infinite number of webs having infinitely large radii in the center ultimately result in a circular shape, wherein the number of pressure measuring points about the circle must be kept finite.

[0041] In this context, FIG. 2 shows a schematic illustration of the assembly a) of measuring obstacles 2a, 2b, 2c, wherein a sectional view is shown on the right-hand side in which behind the pressure measuring opening a channel 4 having a first and a second channel portion 4a, 4b is shown that extends transversely to the measuring surface 1 at the rear of the pressure measuring opening. A pressure measuring device (not shown) can be connected to the end 5 of the channel 4 in order to measure the pressure.

[0042] FIG. 3 shows further embodiments for a boundary layer probe, in which an assembly of measuring obstacles 2a, 2b, 2c is arranged on the measuring surface 1. Here, distal end portions 6a, 6b of adjacent measuring obstacles are connected to one another, so that a continuous course is produced.

[0043] The first four of the embodiments shown in the upper part of FIG. 3 differ from the embodiment shown on the far right in that corner regions are formed where the ends of adjacent obstacles meet, which is not the case with the embodiment shown on the far right (round course of the obstacle). This also applies to the examples of obstacle courses shown in the center in FIG. 3.

[0044] It has been found that the curved obstacle formation (cf. in particular FIGS. 1 and 3) is particularly advantageous at higher fluid speeds at which the compressibility of the fluid to be measured is no longer negligible. Usually this applies to fluid Mach numbers that are larger than 0.3.

[0045] FIGS. 4 and 5 show differential pressure curves and a 4D calibration curve.

[0046] FIG. 4 shows results of measurements. Analogous to the known boundary layer probe with boundary layer fence, the differential pressure curves are used as a basis for evaluation. In each case two pressures are combined to form a measured value in the form of a differential pressure.

[0047] Three phase-shifted, harmonic differential pressure curves 20, 21, 22 can be recognized very well and are very similar to the angle characteristics of the classic boundary layer fence. On the left-hand side in FIG. 4, the reference signs 20, 21, 22 are also schematically associated with the two pressure measuring points, for each of which the course of the pressure difference is shown in the diagram in FIG. 4. In the case of a constant installation position a, there is a combination of three differential pressure values which indicate a clear flow direction.

[0048] One possibility is the direct calibration of the boundary layer probe, in which the three differential pressures are plotted as a function of the flow angle (cf. FIG. 5).

[0049] Other approaches to angular calibration of the probe can also be used. One method is to analytically calculate the flow angle using the three differential pressures:

.sub.flow=f(p(12), p(23), p(31))

[0050] Both the flow angle and the maximum differential pressure that occurs (ideally at 30n 120 n E N) can be determined with only a single installation position. There is therefore no need to turn the probe.

[0051] An alternative evaluation algorithm is based on a linearization of the angle characteristics mentioned above. At least two differential pressures are required for linear interpolation. In the present case there are three. A boundary layer probe having n webs in the simplest case would supply n differential pressure values and further improve the angle determination.

[0052] Potential use cases are numerous. A robust, inexpensive and reliable measuring unit is required in order to measure flows on objects of all kinds. The technology disclosed here can be used for this. These include, for example in any order the turbo machine and automotive industries, manufacturers of wind turbines, and aircraft manufacturers. Because the presented approach promises to also be able to determine the static pressure applied, one unit of the sensor type described would be sufficient to be able to map an extensive range of relevant measurement data. Previously, this required multiple that were unaffordable systems and could only be used in certain applications.

[0053] With the probe technology presented here, flow information is available for the first time which up to now could only be more or less reliably mapped using complex computer models. The validation and further development of existing simulation technology based on the information that is now available is also conceivable.

[0054] The features disclosed in the above description, the claims and the drawings may be relevant to implementing the different embodiments both individually and also in any combination.