CN201662580U - Ultrasonic wind sensor with tetrahedral structure - Google Patents
Ultrasonic wind sensor with tetrahedral structure Download PDFInfo
- Publication number
- CN201662580U CN201662580U CN2010201288193U CN201020128819U CN201662580U CN 201662580 U CN201662580 U CN 201662580U CN 2010201288193 U CN2010201288193 U CN 2010201288193U CN 201020128819 U CN201020128819 U CN 201020128819U CN 201662580 U CN201662580 U CN 201662580U
- Authority
- CN
- China
- Prior art keywords
- ultrasonic
- base
- tetrahedron
- probes
- bearing
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Images
Abstract
The utility model relates to an ultrasonic wind sensor with a tetrahedral structure, which comprises ultrasonic probes arranged on both a bracket and a base, a support positioned between the bracket and the base, and a control cabinet positioned below the base; the ultrasonic wind sensor is characterized in that one probe is vertically arranged on the bracket or the base, three probes are arranged on the base or the bracket, and the four center points of the top end surfaces of the four ultrasonic probes are taken as four apexes of a spatial tetrahedron; or one ultrasonic probe is vertically arranged on the base, and three ultrasonic probes are arranged on the bracket; and the plane determined by the center points of the top end surface of the three ultrasonic probes installed on the bracket or the base is parallel to the horizontal plane, and the tetrahedron can be a regular tetrahedron, a rectangular tetrahedron or other tetrahedrons. The number of the probes is reduced to four from six, so that not only can the structure of the sensor be simplified, but also the cost and the failure rate are reduced; and the number of the measuring paths is increased to six from three, so that the complexity of calculation of the wind speed is greatly reduced.
Description
Technical field
The utility model relates to the measurement mechanism of natural wind field, is specifically related to a kind of tetrahedral ultrasonic wind sensor.
Background technology
Utilize the advantage of ultrasonic wind sensor measuring wind to be not contain moving component, good environmental adaptability, measurement range is wide, and does not have the restriction of minimum measuring wind.The three-D ultrasonic wind sensor of existing classical architecture all is by three (six) ultrasonic probe to be made up the three-dimensional measurement wind field.Above-mentioned ultrasonic probe is the fundamental measurement unit, its inside includes piezoelectric chip, be used to transmit and receive the ultrasound wave of fixed frequency, piezoelectric chip converts electrical energy into mechanical vibration and produces ultrasound wave during emission, and piezoelectric chip is converted to electric energy with the mechanical vibration that ultrasound wave produces during reception.The scattering cover of its ultrasonic probe front end is a planar rondure, each to the probe the scattering cover each other over against, make ultrasonic probe can receive and dispatch ultrasound wave mutually, constitute a measuring route, and three paths constitute three-dimensional orthogonal coordinate system (three-dimensional cartesian coordinate system).Return the mistiming of broadcasting on every paths by measuring ultrasound wave, the component of compute vectors wind on three paths through the synthetic computing of vector, obtains the three-dimensional wind speed under the conventional coordinates again.
There are several shortcomings in ultrasonic wind sensor based on this structure, at first is that it must use six ultrasonic probes, has increased the complexity of cost and structure on the one hand.Failure rate is higher on the other hand.As long as any probe breaks down, measurement result is invalid, and sensor damages and can't use.
In addition, because three measuring route are not in the horizontal direction, also in the vertical direction not, therefore to obtain the X under the conventional coordinates (the XY-plane parallel is in the three-dimensional cartesian coordinate system of surface level), Y, three components of Z must increase the difficulty of calculating through complicated space geometry computing.
Summary of the invention
The purpose of this utility model is to provide a kind of tetrahedral ultrasonic wind sensor, to remedy the deficiencies in the prior art.
The technical solution of the utility model comprises the ultrasonic probe on bearing and the base, and the support between bearing and base, control cabinet with being positioned at the base below is characterized in that vertically being provided with a ultrasonic probe on bearing, is provided with three ultrasonic probes on base; And four central points of the top end face of above-mentioned four ultrasonic probes are tetrahedral four summits, space.
Perhaps above-mentioned tetrahedral ultrasonic wind sensor is vertically to be provided with a ultrasonic probe on base, is provided with three ultrasonic probes on bearing.
The determined plane parallel of central point of the above-mentioned top end face that is installed in three ultrasonic probes on bearing or the base is in surface level.
Above-mentioned top end face central point with four ultrasonic probes is the tetrahedron on four summits, can be positive tetrahedron, right-angle tetrahedron, or other tetrahedron.
In order to disperse the piezoelectric chip of ultrasound wave and protection ultrasonic probe better, be provided with the scattering cover of ceramic material on the ultrasonic probe top, its surface configuration is a spherical crown surface, and the bottom surface of scattering cover overlaps with the top end face of ultrasonic probe.
Utilize the method for above-mentioned tetrahedral ultrasonic wind sensor measuring wind to be: at first the surface level with three central point places on bearing or the base is the XY-plane, with a central point in the XY-plane is coordinate origin O, path with mistake initial point O in the XY-plane is an X-axis, crossing the vertical line that initial point O makes X-axis in the XY-plane is Y-axis, cross initial point O do the XY-plane vertical line be the Z axle, a conventional coordinates is set up in X, Y, three sensings according to the right-hand rule of Z; Under conventional coordinates, measure sound wave in wind field along the mistiming of propagating on every positive and negative both direction of measuring route, express wind speed component on every paths with the velocity of sound and time, utilize the two-D wind speed on the synthetic XY-plane of wind speed component on the path in two surface levels then, again with the synthetic three-dimensional wind vector of the wind speed component of crossing initial point O outside this two-D wind speed and the XY-plane, decompose this vector, promptly obtain the X under the conventional coordinates, Y, three wind speed components of Z.
The utility model beneficial effect compared with prior art is: the quantity of ultrasonic probe is reduced to four by six.Because sensor construction had both been simplified in the minimizing of probe quantity, had reduced cost and failure rate again.A kind of ultrasonic probe that has spherical crown surface scattering cover of the utility model design has good curved surface diversity, and measuring route is increased to six by three, wherein there are three measuring route to be positioned on the XY-plane, simplified basis of calculation X widely, Y, the complexity of three wind speed components of Z.
Description of drawings
The sensor synoptic diagram of three ultrasonic probes is installed on Fig. 1 base of the present utility model.
The sensor synoptic diagram of three ultrasonic probes is installed on Fig. 2 bearing of the present utility model.
Central point synoptic diagram on Fig. 3 ultrasonic probe of the present utility model and the top end face thereof.
Fig. 4 measuring method synoptic diagram of the present utility model.
Wherein, 1, ultrasonic probe, 2, support, 3, bearing, 4, base, 5, control cabinet, 6, the scattering cover, 7, central point, 8 tetrahedrons.
Embodiment
As Fig. 1,2 and 4, the utility model comprises the ultrasonic probe 1 on bearing 3 and the base 4, and the support 2 of 4 of bearing 3 and bases, with the control cabinet 5 that is positioned at base 4 belows, it is characterized in that on bearing 3, vertically being provided with a ultrasonic probe 1, and on base 4, be provided with three ultrasonic probes 1, and the central point 7 of the top end face of above-mentioned four ultrasonic probes 1, be four summits of space tetrahedron 8.
Perhaps above-mentioned tetrahedral ultrasonic wind sensor is vertically to be provided with a ultrasonic probe 1 on base 4, is provided with three ultrasonic probes 1 on bearing 3.
The central point 7 determined plane parallel of the above-mentioned top end face that is installed in three ultrasonic probes 1 on base 4 or the bearing 3 are in surface level.
Above-mentioned top end face central point 7 with four ultrasonic probes 1 is the tetrahedron 8 on four summits, can be positive tetrahedron, right-angle tetrahedron or other tetrahedron.
As Fig. 3, above-mentioned ultrasonic probe 1 is fundamental measurement of the present utility model unit, can transmit and receive the ultrasound wave of fixed frequency, is existing commercially available prod.In order to disperse the piezoelectric chip of ultrasound wave and protection ultrasonic probe 1 better, be provided with the scattering cover 6 of ceramic material on ultrasonic probe 1 top, its surface configuration is a spherical crown surface, and the bottom surface of scattering cover 6 overlaps with the top end face of ultrasonic probe 1.
As Fig. 1,2, above-mentioned support 2 is the rigid mount that three angles are mutually 120 degree, is used for fixing bearing 3; The two ends of support 2 are individually fixed on bearing 3 and the base 4, and the inner space is used for electrical traces.This is a kind of existing ripe supporting structure, can weaken the influence of occlusion effect to measuring as far as possible.
Above-mentioned control cabinet 5 adopts existing ripe circuit, is circuit control assembly of the present utility model, is used for generation, emission, received ultrasonic signal, and calculates measurement result by analysis.
As Fig. 4, comprise four ultrasonic probes in the utility model, can receive and dispatch ultrasound wave mutually in twos, thus the total a of sensor described in the utility model, b, c, d, e, six measuring route of f.
As Fig. 4, measuring method of the present utility model: the surface level with three central point 7 places of the ultrasonic probe on the base 41 is the XY-plane, with central point 7 in the XY-plane is coordinate origin O, path with mistake initial point O in the XY-plane is an X-axis, crossing initial point O makes X-axis in the XY-plane vertical line is Y-axis, cross initial point O do the XY-plane vertical line be the Z axle, X, Y, the sensing that Z is three is set up a conventional coordinates according to the right-hand rule; Receive and dispatch ultrasound wave mutually via a pair of probe of control cabinet 5 control then, calculation of wind speed returns the mistiming of broadcasting on every paths, expresses wind speed component on every paths with the time and the velocity of sound.
It is as follows to obtain the wind speed component of three of X, Y, Z as Fig. 4 then: from three measuring route of initial point O, path a, b is positioned within the XY-plane, wherein path a is an X-axis, wind speed component on a is X-axis wind speed component, synthetic a, the wind speed component on the b obtains the two-D wind speed vector on the XY-plane.Terminal point with this vector is the vertical line that intersection point is done the XY-plane.Be positioned at outside the XY-plane from the path c of initial point O, terminal point with the wind speed component vector on the c is an intersection point, make the vertical plane of path c, above-mentioned vertical line and vertical plane must have an intersection point, and the vector that points to this intersection point from initial point O is exactly the three-dimensional wind vector that will measure.Decompose this vector and obtain Y-axis and Z axle wind speed component, can finish the measurement of the three-dimensional wind speed under the conventional coordinates.
Four central points, the 7 determined tetrahedrons 8 that are arranged on four ultrasonic probes 1 on bearing 3 and the base 4 of the present utility model are to be applicable to various tetrahedrons.Especially the easiest when the measurements and calculations with positive tetrahedron and right-angle tetrahedron structure, following embodiment is described further:
The summit that four ultrasonic probes 1 is laid in positive tetrahedron is located, and promptly bottom center's point 7 definite tetrahedrons 8 of the scattering cover 6 of four ultrasonic probes 1 are positive tetrahedron.Positive tetrahedron is meant that tetrahedral four sides are equilateral triangle, and six limits equate that all summit angles are 60 degree.As Fig. 4, keep a side level, be the XY-plane with it, be initial point O with a summit in this plane, be X-axis with a horizontal route from initial point O, set up conventional coordinates according to method described in the utility model.Positive tetrahedron has good spatial symmetry, and its each paths angle equates, therefore two-D wind speed, three-dimensional wind speed and the X in calculating the XY-plane, and Y is during three wind speed components of Z, for the space geometry computing of vector has brought convenience.
Four ultrasonic probes 1 are laid in the summit place of right-angle tetrahedron, and promptly the bottom center point 7 definite tetrahedrons 8 by the scattering cover 6 of four ultrasonic probes 1 are right-angle tetrahedron.Right-angle tetrahedron is meant that tetrahedron has summit, a right angle, and three right-angled side faces that comprise the summit, right angle are vertical in twos.Therefore, be the XY-plane with a right-angled side faces, be initial point O with the summit, right angle, be X-axis with a right-angle side from initial point O, the two other right-angle side is Y-axis and Z axle, sets up conventional coordinates.As Fig. 4, promptly from three measuring route a of initial point, b, c, just with the X of conventional coordinates, Y, the coincidence of Z axle.Obtain wind speed component on this three paths according to measuring method described in the utility model, be standard x, Y, three wind speed components of Z.Synthetic X, Y, three wind speed components of Z promptly obtain the three-dimensional wind speed that will measure.Present embodiment directly obtains X, Y, three wind speed components of Z by the wind speed component on three paths, thereby has saved the computing of resolution of vectors fully.
Claims (5)
1. tetrahedral ultrasonic wind sensor, comprise the ultrasonic probe (1) on bearing (3) and the base (4), and the support (2) between bearing (3) and base (4), with the control cabinet (5) that is positioned at base (4) below, it is characterized in that on bearing (3), vertically being provided with a ultrasonic probe (1), on base (4), be provided with three ultrasonic probes (1); And four central points (7) of four top end faces of above-mentioned four ultrasonic probes (1) are four summits of space tetrahedron (8).
2. tetrahedral ultrasonic wind sensor, comprise the ultrasonic probe (1) on bearing (3) and the base (4), and the support (2) between bearing (3) and base (4), with the control cabinet (5) that is positioned at base (4) below, it is characterized in that on base (4), vertically being provided with a ultrasonic probe (1), on bearing (3), be provided with three ultrasonic probes (1); And four central points (7) of four top end faces of above-mentioned four ultrasonic probes (1) are four summits of space tetrahedron (8).
3. tetrahedral ultrasonic wind sensor as claimed in claim 1 or 2, it is characterized in that bearing (2) go up or base (3) on the determined plane parallel of central point (7) of top end face of three ultrasonic probes (1) in surface level.
4. tetrahedral ultrasonic wind sensor as claimed in claim 1 or 2, it is characterized in that above-mentioned four top end face central points (7) with four ultrasonic probes (1) are the tetrahedron (8) on four summits, be positive tetrahedron, right-angle tetrahedron, or other tetrahedron.
5. tetrahedral ultrasonic wind sensor as claimed in claim 1 or 2, the top that it is characterized in that above-mentioned ultrasonic probe (1) is provided with scattering cover (6), this scattering cover (6) surface is a spherical crown surface, and the bottom surface of scattering cover (6) overlaps with the top end face of ultrasonic probe (1); Described scattering cover (6) is a ceramic shield.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010201288193U CN201662580U (en) | 2010-03-09 | 2010-03-09 | Ultrasonic wind sensor with tetrahedral structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010201288193U CN201662580U (en) | 2010-03-09 | 2010-03-09 | Ultrasonic wind sensor with tetrahedral structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201662580U true CN201662580U (en) | 2010-12-01 |
Family
ID=43233000
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010201288193U Expired - Fee Related CN201662580U (en) | 2010-03-09 | 2010-03-09 | Ultrasonic wind sensor with tetrahedral structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201662580U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101813709A (en) * | 2010-03-09 | 2010-08-25 | 山东省科学院海洋仪器仪表研究所 | Tetrahedral ultrasonic wind sensor and measuring method thereof |
| CN103558410A (en) * | 2013-10-30 | 2014-02-05 | 苏州斯威高科信息技术有限公司 | Ultrasonic wave anemoscope anti-interference device and method based on non-intrinsic frequency excitation |
| CN107167626A (en) * | 2017-04-28 | 2017-09-15 | 南京信息工程大学 | Three-dimensional ultrasonic wind meter and wind detection method based on nonopiate survey wind formation |
-
2010
- 2010-03-09 CN CN2010201288193U patent/CN201662580U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101813709A (en) * | 2010-03-09 | 2010-08-25 | 山东省科学院海洋仪器仪表研究所 | Tetrahedral ultrasonic wind sensor and measuring method thereof |
| CN103558410A (en) * | 2013-10-30 | 2014-02-05 | 苏州斯威高科信息技术有限公司 | Ultrasonic wave anemoscope anti-interference device and method based on non-intrinsic frequency excitation |
| CN103558410B (en) * | 2013-10-30 | 2015-11-04 | 苏州斯威高科信息技术有限公司 | Based on the jamproof device and method of ultrasonic wind velocity indicator that extrinsic frequency excites |
| CN107167626A (en) * | 2017-04-28 | 2017-09-15 | 南京信息工程大学 | Three-dimensional ultrasonic wind meter and wind detection method based on nonopiate survey wind formation |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN101813709B (en) | Tetrahedral ultrasonic wind sensor and measuring method thereof | |
| CN103163324B (en) | A kind of wind energy turbine set three-dimensional ultrasonic wind speed system for detecting temperature and measuring method thereof | |
| US20180074177A1 (en) | 3d-position determination method and device | |
| CN108169511B (en) | Three-dimensional space carrys out the wind velocity measurement system and method for wind | |
| CN103728463B (en) | Ultrasonic wind meter and measuring method | |
| CN102269769A (en) | Ultrasonic three-dimensional wind measuring method and three-dimensional ultrasonic anemometer | |
| CN102103013A (en) | Three-dimensional vector hydrophone | |
| CN201662580U (en) | Ultrasonic wind sensor with tetrahedral structure | |
| CN104133217B (en) | Method and device for three-dimensional velocity joint determination of underwater moving target and water flow | |
| CN108020815A (en) | A kind of method, equipment and storage device for positioning underwater robot | |
| CN102288779B (en) | High-accuracy anti-interference ultrasonic wind speed and wind direction measuring method | |
| JP2018084537A (en) | Wind measuring device | |
| CN204694730U (en) | Three-dimensional ultrasonic anerovane | |
| CN105509665B (en) | A kind of measuring point space displacement measurement apparatus and method based on ultrasonic wave principle | |
| CN110082431A (en) | A kind of method and device for material surface acoustic impedance measurement | |
| CN203706523U (en) | Sound velocity measuring experiment instrument | |
| RU153990U1 (en) | ACOUSTIC ANEMOMETER | |
| CN103308141B (en) | A kind of two-dimensional quadrupole directivity hydrophone | |
| CN106321370B (en) | By the wind electricity blade flexural measurement device and method for seeking measurement point coordinate | |
| RU2387966C1 (en) | Device for determination of position coordinates of manned space object pressure skin puncture by space particles and method for puncture position coordinates determination | |
| CN108490386A (en) | The detecting system and method for a kind of flexible parallel mechanism moving platform spatial position | |
| CN105738651A (en) | Ultrasonic wave wind speed measurement apparatus with temperature compensation | |
| CN203643467U (en) | Ultrasonic wind meter | |
| CN210075580U (en) | Acoustic vector sensor sensitivity measuring device and system | |
| Ghahramani et al. | An Inexpensive Low-Power Ultrasonic 3-Dimensional Air Velocity Sensor |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20101201 Termination date: 20110309 |