CN201378173Y - Aerovane - Google Patents
Aerovane Download PDFInfo
- Publication number
- CN201378173Y CN201378173Y CN 200920068815 CN200920068815U CN201378173Y CN 201378173 Y CN201378173 Y CN 201378173Y CN 200920068815 CN200920068815 CN 200920068815 CN 200920068815 U CN200920068815 U CN 200920068815U CN 201378173 Y CN201378173 Y CN 201378173Y
- Authority
- CN
- China
- Prior art keywords
- axis
- horizontal
- telescopic link
- automatic telescopic
- vertical shaft
- 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 - Lifetime
Links
Images
Landscapes
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
Abstract
The utility model discloses an aerovane, which comprises a wind speed induction cup, a wind vane and a line interface that are fixed on a second vertical shaft, wherein the lower end of the second vertical shaft is connected with a horizontal self-expanding rod; a plurality of signal acquisition ports are arranged on the horizontal self-expanding rod, and the other end of the horizontal self-expanding rod is connected with a vertical shaft; the lower part of the vertical shaft is connected with a variable speed motor; the line interface and the signal acquisition ports are connected with a data acquisition device by a lead; a horizontal length adjusting valve is arranged on the horizontal self-expanding rod; and a height adjusting valve is arranged on the vertical shaft. By adjusting the height of the vertical shaft and the length of the horizontal self-expanding rod, the horizontal planes with different heights in a selecting point area and the value of each point in different measuring radiuses can be measured, so as to obtain more effective data and achieve the aim that the wind field change regularity is effectively analyzed.
Description
Technical field
The utility model relates to a kind of anerovane.
Background technology
At present, when anerovane carries out in-site measurement, the typhoon aerovane value that can only test certain some position at one time normally, and the wind direction and wind velocity value that can not test the interior a plurality of points of each height Different Plane.
Limited number of test points certificate can not fully reflect the Changing Pattern of wind field, and measurement falls flat.If want to test the more data point, just need more anerovane.So, seek out more field measurement point data, must need to expend more man power and material, cause bigger difficulty and inconvenient to actual measurement undoubtedly.
Therefore, be necessary existing anemoclinograph is made improvement, make it to measure simultaneously the wind speed of same surface level multiple spot under the certain height.
The utility model content
The utility model aims to provide a kind of anerovane, can survey the wind direction and wind velocity value of certain height place each point of diverse location simultaneously.
Technical scheme is, a kind of anerovane, and its structure comprises wind speed induction cup, weathervane, line interface and data collector, also comprises Z-axis, second Z-axis, horizontal automatic telescopic link;
Wind speed induction cup, weathervane and line interface are fixed on second Z-axis;
A plurality of signals collecting ports are installed on the horizontal automatic telescopic link;
The bottom of Z-axis is connected with variable speed machine;
One end of horizontal automatic telescopic link is connected with Z-axis top, and the other end is connected to the bottom of second Z-axis;
Horizontal automatic telescopic link is respectively perpendicular to the Z-axis and second Z-axis, and horizontal automatic telescopic link, Z-axis and second Z-axis are at grade;
Line interface is connected with data collector by lead with the signals collecting port;
The horizontal length variable valve is installed on the horizontal automatic telescopic link;
Height adjusting valve is installed on the Z-axis.
Lead is connected with data collector by cable concentrator.
Variable speed machine is connected with automaton.
Automaton is connected to the horizontal length variable valve.
Based on the variable speed machine effect, drive Z-axis and rotate, thereby second Z-axis is moved along track circumference, weathervane, wind speed induction cup and line interface work, the wind direction and wind velocity of diverse location point on the test circumference.
Regulate Z-axis height and horizontal automatic telescopic link length, can measure the surface level of a reconnaissance zone differing heights, the numerical value of interior each point of different measuring radius, thereby can access more valid data, reach the purpose of effective analysis wind field Changing Pattern.
The beneficial effects of the utility model are, can measure the wind direction and wind velocity numerical value of each point in the said three-dimensional body space easily and effectively when wind direction and wind velocity is measured, and are simple in structure, the testing efficiency height.
Description of drawings
Fig. 1 is the utility model anerovane structural representation
Wherein, 1-weathervane, 2-wind speed induction cup, 3-second Z-axis, 4-Z-axis, 5-height adjusting valve, 6-horizontal length variable valve, the horizontal automatic telescopic link of 7-, 8-signals collecting port, the 9-variable speed machine, the 10-line interface, 11-lead, 12-cable concentrator, the 13-data collector, the 14-automaton
Embodiment
Below in conjunction with the drawings and specific embodiments the utility model is further specified.
As shown in Figure 1, a kind of anerovane, its structure comprises: weathervane 1, wind speed induction cup 2 and line interface 10, weathervane, wind speed induction cup and line interface are fixed on second Z-axis 3;
The lower end of second Z-axis 3 is connected with horizontal automatic telescopic link 7, and a plurality of signals collecting ports 8 are installed on the horizontal automatic telescopic link, and the signals collecting port is connected lead 11 respectively with line interface, and lead is connected with data collector 13 by cable concentrator 12;
The other end of horizontal automatic telescopic link is connected to the upper end of Z-axis 4, and the lower end of Z-axis is connected to variable speed machine 9, and variable speed machine is connected with automaton 14;
Horizontal automatic telescopic link 7 is respectively perpendicular to the Z-axis 4 and second Z-axis 3, and horizontal automatic telescopic link, Z-axis and second Z-axis are at grade;
On the horizontal automatic telescopic link 7 horizontal length variable valve 6 is installed, height adjusting valve 5 is installed on the Z-axis 4.Automaton is also connected to the horizontal length variable valve.
By the height of height adjusting valve 5 adjusting Z-axises 4, horizontal automatic telescopic link 7 is regulated the height that needs measurement; The measured zone radius is set, adjusts horizontal automatic telescopic link length by the horizontal adjustment valve; Horizontal automatic telescopic link moves on the track of specifying radius.
Start variable speed machine 9, Z-axis 4 is rotated; Z-axis drives horizontal automatic telescopic link, is that the horizontal direction rotation is done in the axle center with the Z-axis; Second Z-axis is along being that the circular orbit that the center of circle, horizontal automatic telescopic link length are radius moves with the Z-axis; Be fixed on weathervane, wind speed induction cup and line interface work on second Z-axis, measure the wind direction and wind velocity value of difference on this circumference; Arrange a plurality of wind direction and wind velocity signal output ports on the horizontal automatic telescopic link, the data transmission of measuring immediately can have been arrived data collector.
Utilize automaton, the selected separately radius that needs measured zone, automaton is adjusted horizontal automatic telescopic link length by the horizontal adjustment valve, and second Z-axis is moved on another circular orbit that need measure; Start variable speed machine, by same quadrat method, the wind direction and wind velocity value of difference on the new circular orbit of mensuration sustained height, different radii, and pass through the signals collecting port data transmission is arrived data collector.Like this, can measure sustained height, the wind direction and wind velocity value in the varying level distance range.
Change the height of Z-axis by height adjusting valve; Start variable speed machine, in the same way, the wind direction and wind velocity value of difference on the new circular orbit of mensuration same radius, differing heights, and pass through the signals collecting port data transmission is arrived data collector.Like this, can measure differing heights, the interior wind direction and wind velocity value of same horizontal range scope.
Therefore, this anerovane can be measured the numerical value of each difference position in selection area, thereby can access more valid data, reaches the purpose of effective analysis wind field Changing Pattern; And convenience simple in structure, the testing efficiency height.
Claims (4)
1, a kind of anerovane comprises weathervane, wind speed induction cup, line interface and data collector, it is characterized in that, also comprises Z-axis, second Z-axis, horizontal automatic telescopic link;
Wind speed induction cup, weathervane and line interface are fixed on second Z-axis, and the second Z-axis lower end connects horizontal automatic telescopic link;
A plurality of signals collecting ports are installed on the horizontal automatic telescopic link;
The bottom of Z-axis is connected with variable speed machine;
One end of horizontal automatic telescopic link is connected with Z-axis top, and the other end is connected to the bottom of second Z-axis;
Horizontal automatic telescopic link is respectively perpendicular to the Z-axis and second Z-axis, and horizontal automatic telescopic link, Z-axis and second Z-axis are at grade;
Line interface is connected with data collector by lead with the signals collecting port;
The horizontal length variable valve is installed on the horizontal automatic telescopic link;
Height adjusting valve is installed on the Z-axis.
2, the described a kind of anerovane of claim 1 is characterized in that lead is connected with data collector by cable concentrator.
3, the described a kind of anerovane of claim 1 is characterized in that variable speed machine is connected with automaton.
4, the described a kind of anerovane of claim 1 is characterized in that automaton is connected to the horizontal length variable valve.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 200920068815 CN201378173Y (en) | 2009-03-13 | 2009-03-13 | Aerovane |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 200920068815 CN201378173Y (en) | 2009-03-13 | 2009-03-13 | Aerovane |
Publications (1)
Publication Number | Publication Date |
---|---|
CN201378173Y true CN201378173Y (en) | 2010-01-06 |
Family
ID=41518290
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN 200920068815 Expired - Lifetime CN201378173Y (en) | 2009-03-13 | 2009-03-13 | Aerovane |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN201378173Y (en) |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103018483A (en) * | 2012-11-30 | 2013-04-03 | 中国北车集团大连机车车辆有限公司 | Steering testing device for locomotive fan |
CN104615073A (en) * | 2015-01-30 | 2015-05-13 | 西南交通大学 | Wind observation device capable of being automatically adjusted in azimuth on bridge tower and adjustment method thereof |
CN106639496A (en) * | 2016-12-05 | 2017-05-10 | 北京普华亿能风电技术有限公司 | Wind and shadow resistant anemometer tower |
CN106679928A (en) * | 2016-10-28 | 2017-05-17 | 华南农业大学 | Three-dimensional wind field measurement system applicable to unmanned aerial vehicle and use method of three-dimensional wind field measurement system |
CN106760869A (en) * | 2016-12-05 | 2017-05-31 | 北京普华亿能风电技术有限公司 | A kind of wind resistance shadow anemometer tower |
CN108196085A (en) * | 2017-11-20 | 2018-06-22 | 北京天恒长鹰科技股份有限公司 | A kind of near-earth height wind speed measuring device and method |
CN110987351A (en) * | 2019-12-24 | 2020-04-10 | 西北农林科技大学 | Spatial wind field stereo measurement device and method for orchard sprayer |
CN111855137A (en) * | 2019-11-13 | 2020-10-30 | 东南大学 | Many whirlwind whirlpools wind generating device of core radius adjustable |
CN115143380A (en) * | 2022-05-17 | 2022-10-04 | 上汽通用五菱汽车股份有限公司 | Anemoscope installation mechanism and air volume test system |
CN118088387A (en) * | 2024-02-29 | 2024-05-28 | 江苏斯维尔建筑设计院有限公司 | Height-adjustable wind power tower and adjusting method thereof |
-
2009
- 2009-03-13 CN CN 200920068815 patent/CN201378173Y/en not_active Expired - Lifetime
Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103018483A (en) * | 2012-11-30 | 2013-04-03 | 中国北车集团大连机车车辆有限公司 | Steering testing device for locomotive fan |
CN104615073A (en) * | 2015-01-30 | 2015-05-13 | 西南交通大学 | Wind observation device capable of being automatically adjusted in azimuth on bridge tower and adjustment method thereof |
CN104615073B (en) * | 2015-01-30 | 2017-02-22 | 西南交通大学 | Adjustment method of wind observation device capable of being automatically adjusted in azimuth on bridge tower |
CN106679928B (en) * | 2016-10-28 | 2019-01-08 | 华南农业大学 | A kind of three-dimensional Wind field measurement system and its application method suitable for unmanned plane |
CN106679928A (en) * | 2016-10-28 | 2017-05-17 | 华南农业大学 | Three-dimensional wind field measurement system applicable to unmanned aerial vehicle and use method of three-dimensional wind field measurement system |
CN106760869B (en) * | 2016-12-05 | 2019-07-02 | 北京普华亿能风电技术有限公司 | A kind of wind resistance shadow anemometer tower |
CN106760869A (en) * | 2016-12-05 | 2017-05-31 | 北京普华亿能风电技术有限公司 | A kind of wind resistance shadow anemometer tower |
CN106639496A (en) * | 2016-12-05 | 2017-05-10 | 北京普华亿能风电技术有限公司 | Wind and shadow resistant anemometer tower |
CN106639496B (en) * | 2016-12-05 | 2019-07-02 | 北京普华亿能风电技术有限公司 | A kind of wind resistance shadow anemometer tower |
CN108196085A (en) * | 2017-11-20 | 2018-06-22 | 北京天恒长鹰科技股份有限公司 | A kind of near-earth height wind speed measuring device and method |
CN111855137A (en) * | 2019-11-13 | 2020-10-30 | 东南大学 | Many whirlwind whirlpools wind generating device of core radius adjustable |
CN111855137B (en) * | 2019-11-13 | 2022-04-05 | 东南大学 | Many whirlwind whirlpools wind generating device of core radius adjustable |
CN110987351A (en) * | 2019-12-24 | 2020-04-10 | 西北农林科技大学 | Spatial wind field stereo measurement device and method for orchard sprayer |
CN110987351B (en) * | 2019-12-24 | 2024-06-04 | 西北农林科技大学 | Spatial wind field three-dimensional measurement device and method for orchard sprayer |
CN115143380A (en) * | 2022-05-17 | 2022-10-04 | 上汽通用五菱汽车股份有限公司 | Anemoscope installation mechanism and air volume test system |
CN118088387A (en) * | 2024-02-29 | 2024-05-28 | 江苏斯维尔建筑设计院有限公司 | Height-adjustable wind power tower and adjusting method thereof |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN201378173Y (en) | Aerovane | |
CN104060572B (en) | Flap type wave generator system in a kind of super gravity field | |
CN102073071B (en) | Fully automatic and high-precision dust and sand collector | |
CN201615848U (en) | Full-automatic and high-precision sand-dust collector | |
CN206311975U (en) | A kind of Radar IF simulation device | |
CN202720104U (en) | Portable type high precision automatic sand collector and automatic sand collection system | |
CN209525054U (en) | A kind of small-sized fixed-wing aerial survey unmanned plane centroid measurement instrument | |
CN212364343U (en) | Multi-point displacement dynamic air quantity measuring device | |
CN102207513B (en) | Method for calibrating rotor current meter | |
CN210426467U (en) | Electric power construction foundation ditch detection device | |
CN102494632B (en) | Device and method for detecting heliostat face shape error | |
CN206756870U (en) | A kind of spherical three-dimensional multi-functional air speed measuring apparatus | |
CN206696306U (en) | A kind of current meter calibration equipment | |
CN204613239U (en) | A kind of base construction of wind speed measuring apparatus | |
CN204613238U (en) | A kind of wind speed measuring apparatus | |
CN103123361B (en) | MEMS angular velocity and acceleration transducer automatic calibration method and system thereof | |
CN209656694U (en) | A kind of soil erosion measurement and positioning device | |
CN204881942U (en) | Ball friction torque detector | |
CN108981747B (en) | Wave direction calibrating device for wave buoy | |
CN115560936A (en) | Laser automatic detection device and detection method for looseness of tower bolt | |
CN202453007U (en) | Comprehensive water power parameter test device | |
CN208398892U (en) | The wave direction calibrating installation of wave buoy | |
CN106840924A (en) | A kind of shock resistance tester for simulating the impact of bulky grain bed load | |
CN103575929A (en) | Multi-wind-direction wind-drift-sand-flow flow real-time monitor | |
CN206557016U (en) | A kind of shock resistance tester for simulating the impact of bulky grain bed load |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CX01 | Expiry of patent term |
Granted publication date: 20100106 |
|
CX01 | Expiry of patent term |