阅读说明：本技术 风传感器壳体和包括这种壳体的风传感器 (Wind sensor housing and wind sensor comprising such a housing ) 是由 罗宾·斯特罗恩 于 2016-09-09 设计创作，主要内容包括：提供了一种用于风传感器2的壳体6。传感元件4安装在壳体6中用于测量通过的流体流的速度,并且壳体6包括至少一个表面40、42,该至少一个表面具有诸如从表面40、42的突起的突出部和/或凹入表面40、42中的凹入部的成形表面元件38,用于在跨过表面40、42流动的流体中引起湍流。由成形表面元件38所引起的湍流使得通过风传感器2测量的速度较少地受到层流和湍流气流之间的不受控制的转变的影响,并因此实现风传感器2的更精确的校准。(A housing 6 for a wind sensor 2 is provided. The sensing element 4 is mounted in a housing 6 for measuring the velocity of the passing fluid flow, and the housing 6 comprises at least one surface 40, 42 having shaped surface elements 38 such as protrusions from the surface 40, 42 and/or recesses into the surface 40, 42 for inducing turbulence in the fluid flowing across the surface 40, 42. The turbulence caused by the shaped surface elements 38 makes the velocity measured by the wind sensor 2 less affected by uncontrolled transitions between laminar and turbulent air flows and thus enables a more accurate calibration of the wind sensor 2.)

1. A housing for a wind sensor, the housing comprising:

a first housing body having a cylindrical cross-section;

a second housing body having a cylindrical cross-section;

a first reflector in the first housing body; and

a second reflector mounted in the second housing body and coaxially with the first reflector, thereby defining a resonant cavity between the first and second reflectors;

the housing has at least one surface comprising one or more shaped surface elements for inducing turbulence in a fluid flowing across the surface, wherein the one or more shaped surface elements are arranged on a surface extending around a periphery of the first housing body and/or the second housing body.

2. The housing of claim 1, wherein at least one shaped surface element comprises a protrusion from the surface.

3. The housing of claim 1, wherein at least one shaped surface element comprises a recess into the surface.

4. The housing of claim 1, wherein at least one shaped surface element is integral with the surface.

5. The housing according to any one of claims 1 to 4, comprising a plurality of shaped surface elements, wherein the shaped surface elements are evenly arranged on the surface.

6. The housing according to any one of claims 1 to 4, comprising a plurality of shaped surface elements, wherein the shaped surface elements are of uniform size.

7. The housing according to any one of claims 1 to 4, wherein the shaped surface elements induce turbulence in a fluid flowing across the surface at a velocity of more than 3 m/s.

8. The housing of any of claims 1-4, wherein the surface elements are disposed on at least one surface over which a fluid flows as it passes through the housing.

9. A housing according to any one of claims 1 to 4, wherein the housing is arranged to house a sensing element therein to measure fluid flow therethrough.

10. The housing according to any one of claims 1 to 4, wherein the surface elements are arranged on at least one surface of the housing adjoining the resonant cavity.

11. A wind sensor comprising a housing as claimed in any one of claims 1 to 4.

Technical Field

The present invention relates to a housing for a wind sensor, and a wind sensor incorporating the housing.

Background

Wind sensors can be used to measure the flow velocity of air or fluid in a free field. In many applications, it is desirable or necessary to accurately measure fluid velocity.

Wind speed measurements made by the wind sensor can be affected by changes in the orientation of the wind sensor relative to the airflow and the transition from laminar to turbulent flow in the vicinity of the wind sensor, resulting in errors in the measured wind speed.

The present invention seeks to provide a novel housing for a wind sensor.

Drawings

FIG. 1 is a schematic block diagram of the main elements of a wind sensor according to one embodiment of the present invention.

FIG. 2 is a side view of a portion of a wind sensor according to one embodiment.

FIG. 3 is a side view of a central portion of the housing of the wind sensor shown in FIG. 2.

Fig. 4 is a horizontal cross-sectional view through the AA section in fig. 2.

Fig. 5 is a diagram showing a plan view of a separated laminar flow around a cylindrical object.

Fig. 6 is a diagram illustrating a plan view of the separation turbulence around a cylindrical object.

Fig. 7 shows the relationship of reynolds number between resistance and surface property.

Fig. 8 illustrates fluid flow over a fluid flow sensor.

Detailed Description

According to an aspect of the invention, a housing for a wind sensor is provided. The housing includes a first housing body having a cylindrical cross-section, a second housing body having a cylindrical cross-section, a first reflector in the first housing body, and a second reflector in the second housing body and mounted coaxially with the first reflector to define a resonant cavity between the first and second reflectors. The housing has at least one surface comprising one or more shaped surface elements for inducing turbulence in a fluid flowing across the surface. One or more shaped surface elements are arranged on a surface extending around the periphery of the first housing body and/or the second housing body.

According to another aspect of the invention there is provided a housing for a wind sensor, the housing having at least one surface comprising one or more shaped surface elements for inducing turbulence in a fluid flowing across the surface.

According to another aspect of the present invention there is provided a wind sensor comprising a housing according to any of the preceding aspects of the present invention.

The housing according to embodiments of the invention mitigates errors associated with the orientation of the wind speed sensor with respect to the airflow and the transition between laminar and turbulent flow.

Specific embodiments will now be described, by way of example only, with reference to the accompanying drawings.

An embodiment of the wind sensor of the present invention will now be described with reference to fig. 1 to 6. In one embodiment, the fluid being measured is air. However, the velocity of other moving fluids may be measured using a wind sensor having the disclosed housing. The terms "wind sensor" and "airflow" should therefore be understood accordingly, and embodiments generally extend to fluid flow sensors.

Referring to the drawings, a wind sensor 2 includes a sensing element 4 for sensing wind speed and generating an electrical signal associated with the wind speed, and a housing 6 for housing the sensing element 4. The wind sensor 2 further has a processing element 8, the processing element 8 being electrically coupled to the sensing element 4 for processing the electrical signal generated by the sensing element 4 in order to determine a wind speed measurement. In the embodiment disclosed, the housing 6 accommodates a processing element 8 in addition to the sensor element 4, but this is not essential.

In the disclosed embodiment, the housing 6 is substantially cylindrical and comprises a first housing body part 12 and a second housing body part 14, the first housing body part 12 and the second housing body part 14 being coaxially arranged as the housing 6. The first housing body portion 12 and the second housing body portion 14 are also both generally cylindrical.

In the disclosed embodiment, the sensing element 4 uses the principle of acoustic resonance in order to sense the velocity of the passing air flow. The first housing body section 12 is provided with a flat surface as a first reflector 16, while the second housing body section 14 is provided with a flat surface as a second reflector 18. The first reflector 16 and the second reflector 18 are circular plates. The first and second reflectors 16, 18 are arranged parallel to each other and spaced apart from each other by a distance D by a plurality of spacers 20 positioned at intervals around the periphery of the first and second reflectors 16, 18. The first reflector 16 and the second reflector 18 define a resonant cavity 24 forming a measurement cavity of the sensing element 4 in the space between the first reflector 16 and the second reflector 18.

In the disclosed embodiment, the first housing body part 12, the second housing body part 14, the first reflector 16, the second reflector 18 and the spacer 20 are integral components of the housing 6 and are formed by machining a cylindrical metal piece. At least one of the first housing body section 12 and the second housing body section 14 may be made hollow to accommodate a converter (described later) and an electronic circuit as necessary. In other embodiments, the first housing body portion 12 may be formed separately from the second housing body portion 14.

The resonant cavity 24 is open to the fluid flow and occupied by the fluid whose velocity is to be measured. In the disclosed embodiment, the resonant cavity 24 contains air that is free to flow through the resonant cavity 24 in any direction.

In the disclosed embodiment, the wind sensor 2 is provided with three electro-acoustic transducers 26, 28, 30 mounted on the second reflector 18 and arranged to emit acoustic signals into the resonant cavity 24 and to receive acoustic signals from the resonant cavity 24.

The acoustic signals received by the transducers 26, 28, 30 are converted to electrical signals and the electrical signals are passed to the processing element 8 for processing to determine the velocity of the airflow. In the disclosed embodiment, the processing element 8 is also operable to generate an electrical excitation signal that is applied to the transducers 26, 28, 30 to cause the transducers 26, 28, 30 to emit an acoustic signal within the resonant cavity 24.

Thus, in the disclosed embodiment, the sensing element 4 includes a first reflector 16 and a second reflector 18 that define a resonant cavity 24, and three transducers 26, 28, 30. In the disclosed embodiment, the sensing element 4 operates as described in european patent publication EP0801311B to determine an airflow measurement. As described in detail in EP0801311B, the wind direction may be determined from wind speed measurements made between different pairs of transducers 26, 28, 30.

At least one shaped surface element 38 is arranged on or applied to a surface 40, 42 of the housing 6. Thus, the housing 6 has at least one surface 40, 42 comprising one or more shaped surface elements 38. In the disclosed embodiment, the shaped surface elements 38 are disposed on a surface 40 of the first housing body portion 12 and a surface 42 of the second housing body portion 14. In other embodiments, the shaped surface elements 38 may be provided on only one surface 40, 42 of the housing 6.

The surfaces 40, 42 on which the shaped surface elements 38 are disposed or arranged are the surfaces over which the fluid (in this case air) flows when it passes through the housing 6. The shaped surface elements 38 induce turbulence in the airflow across the surfaces 40, 42 of the housing 6.

The surfaces 40, 42 extend around the periphery of the housing 6. The housing 6 of the disclosed embodiment is generally cylindrical, and thus the surfaces 40, 42 extend around the entire circumference of the housing 6. The presence of the shaped surface elements 38 around the entire circumference results in a uniform performance of the wind sensor 2 regardless of the radial direction of the wind, i.e. regardless of the position of the circumferential periphery on which the wind is incident. However, in some embodiments, the surfaces 40, 42 on which the shaped surface elements 38 are provided may extend over only a portion of the circumference or circumference of the housing 6.

In the disclosed embodiment, the surfaces 40, 42 have a limited longitudinal extent, that is, they extend only over a portion of the height of the housing (which may be the length of the cylinder). The surfaces 40, 42 are adjacent to the sensing element 4 provided by the resonant cavity 24 which serves as a measurement cavity. In some embodiments, the surfaces 40, 42 extend the entire length of the housing 6.

In the disclosed embodiment, the shaped surface element 38 is integral with the surfaces 40, 42 on which it is disposed. In the disclosed embodiment, the shaped surface elements 38 are created by machining the surfaces 40, 42 of the housing 6. In other embodiments, the shaped surface element 38 may be separate from the housing 6 and may be coated or secured to the surfaces 40, 42.

In one embodiment, the shaped surface element 38 includes protrusions protruding from the surfaces 40, 42. The height of the protrusion is generally at least 0.1 millimeter (0.0001 meter), and is generally in the range of 0.1 to 1 millimeter (0.0001 to 0.001 meter).

In one embodiment, the shaped surface element 38 includes a recess or indentation into the surfaces 40, 42. The depth of the recess is typically at least 0.1 mm (0.0001 m) and typically in the range of 0.1 mm to 1 mm (0.0001 m to 0.001 m).

In the disclosed embodiment, the plurality of shaped surface elements 38 are raised to a uniform height from the surfaces 40, 42 or recessed to a uniform depth into the surfaces 40, 42.

In some embodiments, the adjacent shaped surface elements 38 applied to the surfaces 40, 42 are not identical. The variation in the coated forming surface elements 38 may result in a greater degree of turbulence provided by the forming surface elements 38.

In some embodiments, the shaped surface element 38 may include protrusions protruding from the surfaces 40, 42 and recesses recessed into the surfaces 40, 42. In some embodiments, the raised shaped surface elements 38 and the recessed shaped surface elements 38 alternate in a direction around the perimeter or circumference of the housing 6 and/or in a longitudinal direction of the housing 6. The alternation of concave and convex shaped surface elements 38 may provide increased turbulence.

In the disclosed embodiment, the shaped surface elements 38 are evenly spaced on the surfaces 40, 42. The shaped surface elements 38 may produce a uniform performance of the wind sensor 2 regardless of the relative direction of the wind.

The shaped surface elements 38 may be disposed at even angular intervals around the circumference or circumference of the housing 6. The even spacing of the shaped surface elements 38 around the circumference or circumference of the housing 6 results in a uniform performance of the wind sensor 2 regardless of the radial direction of the wind. In the disclosed embodiment, thirty-six shaped surface elements 38 are disposed about the circumference of the housing 6 at 10 degree angular intervals between adjacent surface elements 38.

In the disclosed embodiment, the shaped surface elements 38 have a uniform size. The uniform size of the shaped surface elements 38 may result in a uniform performance of the wind sensor 2 regardless of the radial direction of the wind.

In the disclosed embodiment, the length of the shaped surface element 38, i.e. the length of the shaped surface element 38 in the longitudinal direction of the shell 6, is typically at least 2 mm (0.002 m) and typically in the range of 5 mm to 15 mm (0.005 m to 0.015 m). In some embodiments, the shaped surface elements 38 may extend along the entire height of the first housing body portion 12 and/or along the entire height of the second housing body portion 14.

In the disclosed embodiment, the width of the shaped surface elements 38 (i.e., the size of the shaped surface elements 38 in the circumferential direction of the shell 6) is typically at least 2 millimeters (0.002 meters), and typically in the range of 3 millimeters to 15 millimeters (0.003 meters to 0.015 meters). In some embodiments, the shaped surface elements 38 may extend around the perimeter or circumference of the housing 6.

In the disclosed embodiment, the shaped surface element 38 is substantially rectangular in plan view and has a cross-sectional profile that is, for example, substantially rectangular, such as a cuboid. In other embodiments, shaped surface elements 38 having square, oval, triangular, and other shapes in cross-sectional profile when viewed in plan, work effectively and can be more easily manufactured by automated tooling. In one embodiment, all the shaped surface elements 38 are identical. In some embodiments, different planar or contoured shapes may be used for each of the plurality of shaped surface elements 38. The use of a plurality of non-identical shaped surface elements 38 may create a greater degree of turbulence.

The shaped surface elements 38 of the disclosed embodiments induce turbulence in the fluid flowing across the surfaces 40, 42 of the housing 6 at the actual wind speeds encountered by the wind sensor 2, for example for wind speeds greater than 3 m/s.

The fluid flow around the object is laminar or turbulent, depending on factors such as the viscosity of the fluid, the velocity of the fluid flow, and the shape of the object or the direction of the object relative to the fluid flow, and can be analyzed using the reynolds number. Laminar flow of fluid occurs at low reynolds numbers and is characterized by smooth fluid motion. At high reynolds numbers, the fluid exhibits turbulence. In air, the boundary between the laminar flow of air and the turbulent flow following it is generally produced at about 10⁵Reynolds number of (d).

The difference between laminar flow around a cylindrical object and turbulent flow around a cylindrical object can be more clearly understood with reference to fig. 5 to 7.

Figure 5 shows the fluid flowing around the cylinder at a given flow rate. It can be seen that the fluid flow is laminar at the sides of the cylinder, but separates from the cylinder, creating a large low pressure area on the lee side of the cylinder. In this case, the cylinder body may generate a considerable resistance.

Figure 6 shows different forms of fluid flowing around the cylinder at a higher flow rate than that experienced in the configuration shown in figure 5. A turbulent boundary layer is along the sides of the cylinder. Contrary to the flow regime seen in fig. 5, the fluid flow in fig. 6 flows further along the contour of the cylinder to the lee side of the cylinder. In such a flow structure, the low pressure area is smaller, and thus the resistance is reduced.

The graph in fig. 7 illustrates the dependence of the resistance on the reynolds number. The reynolds number is a well-known quantity that is proportional to the relative velocity of the fluid flow over the surface of the object. It can be seen that at low reynolds numbers/slow fluid flow rates, the resistance is high. At these flow rates there is a laminar flow regime as shown in figure 5. However, as the fluid flow velocity/reynolds number increases, turbulent fluid flow conditions are created, resulting in a sharp and abrupt decrease in resistance at a reynolds number that is specific to the object over which the fluid is flowing. It has been recognized that sudden changes between laminar and turbulent fluid flow conditions considerably affect the measurement accuracy of fluid velocity sensors, and it is therefore desirable to cause such changes at low wind speeds as occurs where the effect of drag is minimized.

In the example shown in fig. 7, the operating range begins at zero fluid flow velocity and extends to a maximum fluid flow velocity. At low fluid flow rates, the flow regime shown in fig. 5 is very common and therefore experiences high resistance. At the upper end of the operating range shown in fig. 7, the fluid flow conditions shown in fig. 6 are prevalent and experience a correspondingly small amount of resistance. As can be seen from fig. 7, the transition between these two states is an abrupt transition. Experiments have shown that for a smooth walled version of the fluid flow sensor of the type shown in fig. 2 and 3 (i.e. a fluid sensor that does not include shaped surface elements as comprised in the embodiments shown in these figures) and a constant fluid flow velocity, although the sensor appears symmetrical, switching or alternating switching between laminar and turbulent fluid flow conditions may occur and significantly affect the measurement accuracy. It was found, particularly surprisingly, that even small changes in the direction of entry of the fluid flow on the sensor lead to significant changes in the measured fluid flow velocity. Without wishing to be bound by theory, it is believed that this change in the incoming direction of the fluid flow exposes the plurality of spacers 20 to the fluid flow in the following manner: based on the angle of entry of the fluid flow on the sensor housing, laminar or turbulent flow of the fluid around the sensor is caused. According to fig. 7, this is believed to cause a step change in the amount of resistance experienced by the fluid flow.

As also shown in fig. 7, the transition between high and low resistance fluid flow states occurs at different reynolds numbers for smooth walled objects and for objects with rough surfaces. It will be appreciated that the sensitivity of the sensor to these changing flow conditions is higher for high fluid flow velocities than for lower fluid flow velocities. It will thus be appreciated that the use of shaped surface elements is desirable to incorporate therein. Furthermore, it has also been found that the change in resistance magnitude at transitions between two flow states, as also shown in FIG. 7, transitions less at lower Reynolds numbers than at higher Reynolds numbers.

FIG. 8 illustrates fluid flow incident on a sensor housing of an embodiment. The fluid flow may be considered to include a component 50, a component 60, and a component 70, the component 50 being incident on the first housing portion 12, the component 60 being incident on the first housing portion 14, and the component 70 flowing through the resonant cavity 24. In a smooth wall sensor housing where this effect can be observed, it is only the fluid component 70 that may cause the fluctuations in the velocity measurements described above. It has surprisingly been found, however, that the addition of the above-described shaped surface elements 38 to the surfaces 40 and 42 alleviates this problem, such that fluctuations in flow rate measurements are reduced or eliminated. This is surprising in view of the fact that the shaped surface elements act on the flow components 50 and 60 if they are provided on both surfaces 40 and 42, or on only one of the flow components 50 and 60 if they are provided on only one of the surfaces 40 and 42. Without wishing to be bound by theory, it is believed that the shaped surface elements 38 on surfaces 40 and/or 42 cause turbulence in the leeward side of the first and/or second housing body portions 12/14, as shown in fig. 8, and similar to the flow pattern shown in fig. 6. It is believed that by imposing such a flow pattern on flow components 50 and/or 60, the pressure downstream of first and/or second sensor housing body portions 12/14 changes in a manner that also affects flow component 70 such that the change in the angle of incidence of fluid flow component 70 on support 20 is insufficient for flow component 70 to assume a laminar flow pattern. Thus, the transition from laminar to turbulent fluid flow for the entire sensor occurs at a lower reynolds number/flow rate in the portion of the operating range of the sensor where the transition has a reduced effect on measurement accuracy. Thus, the entire sensor will operate according to the solid lines shown in FIG. 7. The turbulence in the boundary layer of the air flow around the wind sensor 2 caused by the shaped surface elements 38 affects the overall flow pattern around the wind sensor 2. Thus, changes in the measured airflow will always affect changes in the true wind speed, rather than reflect changes between laminar and turbulent fluid flows around the wind sensor 2. Thus, inaccuracies in the calibration of the wind sensor 2 due to unpredictable variations between laminar and turbulent fluid flows around the wind sensor 2 may be avoided.

Embodiments of the present disclosure thus provide a housing 6 for a wind speed sensor 2. The housing 6 causes turbulence in the airflow and the overall flow pattern is substantially insensitive to wind orientation, wind turbulence levels and contamination of the wind sensor surface. Thus, inaccuracies in wind speed caused by unpredictable switching between laminar and turbulent flow may be reduced or eliminated, and calibration of the wind sensor 2 may be achieved more accurately. The measurement of wind direction is also improved since the wind direction can be calculated from a plurality of wind speed measurements.

In the disclosed embodiment, the shaped surface elements 38 are arranged on a surface on which air flows when passing through the wind sensor 2. However, the shaped surface element 38 may additionally or alternatively be disposed within the resonant cavity 24.

Other variations and modifications will be apparent to persons skilled in the art. Such variations and modifications may involve equivalent and other features which are already known and which may be used instead of or in addition to features already described herein. Features which are described in the context of separate embodiments may be provided in combination in a single embodiment. Conversely, features which are described in the context of a single embodiment can also be provided separately or in any suitable subcombination.

It should be noted that the term "comprising" does not exclude other elements, the terms "a" or "an" do not exclude a plurality, a single feature may fulfil the functions of several features recited in the claims and reference signs in the claims shall not be construed as limiting the scope of the claims. It should also be noted that the drawings are not necessarily to scale; emphasis instead generally being placed upon illustrating the principles of the disclosure.