CN201378173Y - Aerovane - Google Patents

Aerovane Download PDF

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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
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CN
China
Prior art keywords
axis
horizontal
telescopic link
automatic telescopic
vertical shaft
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Expired - Lifetime
Application number
CN 200920068815
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Chinese (zh)
Inventor
蒋友娣
朱伟峰
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shanghai Building Science Research Institute Group Co Ltd
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Shanghai Building Science Research Institute Group Co Ltd
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Priority to CN 200920068815 priority Critical patent/CN201378173Y/en
Application granted granted Critical
Publication of CN201378173Y publication Critical patent/CN201378173Y/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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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

A kind of anerovane
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.
CN 200920068815 2009-03-13 2009-03-13 Aerovane Expired - Lifetime CN201378173Y (en)

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

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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)

* Cited by examiner, † Cited by third party
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

Cited By (16)

* Cited by examiner, † Cited by third party
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

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Granted publication date: 20100106

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