CN201748917U - Wireless optical pilot balloon theodolite - Google Patents
Wireless optical pilot balloon theodolite Download PDFInfo
- Publication number
- CN201748917U CN201748917U CN2010202236707U CN201020223670U CN201748917U CN 201748917 U CN201748917 U CN 201748917U CN 2010202236707 U CN2010202236707 U CN 2010202236707U CN 201020223670 U CN201020223670 U CN 201020223670U CN 201748917 U CN201748917 U CN 201748917U
- Authority
- CN
- China
- Prior art keywords
- theodolite
- interface
- communication module
- wireless communication
- lens body
- 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
Landscapes
- Arrangements For Transmission Of Measured Signals (AREA)
Abstract
The utility model discloses a wireless optical pilot balloon theodolite which comprises an upper lens body provided with a primary telescope, an auxiliary telescope, a zoom mechanism setting wheel and a pitching rotating wheel, and a lower lens body provided with an orientation rotating setting rotating wheel, a zeroing mechanism setting rotating wheel, a data acquisition and storage system setting interface, and a data acquisition key. The theodolite is characterized in that a dovetail groove mechanism is installed on the right side of the upper lens body; a micropower wireless communication module is installed on the upper lens body through the dovetail groove mechanism; the micropower wireless communication module is connected with an interface on the lower lens body of the theodolite through a communication cable; the interface is connected with a main board of the theodolite; and 80 mm spiral SMA antennas are connected on the micropower wireless communication module. The theodolite retains the optical part of an original pilot balloon theodolite, adopts the combination of optical technology, mechanical technology and electric technology, can be used for manual observation and balloon capture, collect data automatically, and transmit data through the wireless module. The design of a sensor adopts the technologies of optical circle and photoelectric encoder, and the synchronous acquisition of optical signals and electrical signals is realized. Data can be simultaneously transmitted to a PC and a hand-held calculator.
Description
Technical field
The utility model relates to a kind of Optical Wind Transit, particularly a kind of wireless optical pilot balloon theodolite.
Background technology
At present, digital Optical Wind Transit has been equipped with army for many years, along with the continuous progress of society, the fast development of science, the artilleryman of army, air force or local meteorological station are a kind of additional detection means of atmospheric exploration using digital Optical Wind Transit to carry out upper air wind measuring.But need the dedicated telephone line cable when this anemometer and external equipment communication, client cables might hinder the anemometer observation data.The real-time image data of digital pilot balloon theodolite step-length interval time was fixed as 60 seconds, must increase operator's labour by artificial timing or not timing image data when needs are encrypted observation.Thereby this transit comes with some shortcomings.
The utility model content
The purpose of this utility model provides a kind of wireless optical pilot balloon theodolite, light harvesting, mechanical, electrical in the portable instrument of one, and stable performance, easy to use, satisfy high precision, high-level efficiency, high-tech needs.Newly designed wireless communication module, increased many grades and gathered the step-length selection function.Break away from the constraint of data communication cable, and alleviated operator's labour intensity.
The purpose of this utility model is achieved by the following technical solution: comprise being provided with the body on show that primary telescope, auxiliary telescope, change times mechanism are provided with wheel, pitch rotation wheel, be provided with that azimuth rotation is provided with runner, the mechanism of making zero is provided with runner, the data acquisition storage system is provided with interface, the following mirror body of data acquisition key, it is characterized in that: a dovetail groove mechanism is installed on body on show right side, and the micro-power wireless communication module is assembled on the body on show by dovetail groove mechanism; The micro-power wireless communication module connects the interface on the mirror body under the transit by communication cable, and interface is connected with the transit mainboard; Connect 80mm spiral SMA antenna on the micro-power wireless communication module.
The advantage that the utlity model has is: kept former pilot balloon theodolite opticator, adopted light, mechanical, electrical three technology to combine, can manually observe, catch balloon, the transit automatic data collection is by wireless module transmission data.On sensor design, adopt optical circle and the same disk technology of photoelectric code disk, realize optics and electrical signal synchronous acquisition.Can be simultaneously to PC and hand-held calculator transmission data.
Description of drawings
Fig. 1 is a structural representation of the present utility model.
Fig. 2 is the left view of Fig. 1.
Fig. 3 is an oat tail groove structure.
Embodiment
Fig. 1-3, concrete structure is as follows: the utility model has primary structure now: primary telescope 15, auxiliary telescope 14 are set on the body 4 on show, become a times mechanism wheel 5, pitch rotation wheel 3 are set; Be provided with on the following mirror body 2 that azimuth rotation is provided with runner 10, the mechanism of making zero is provided with runner 1, the data acquisition storage system is provided with interface 12, data acquisition key 17.Main improved technical essential is: a dovetail groove mechanism 18 is installed on its body on show 4 right sides, and micro-power wireless communication module 7 is assembled on the body 4 on show by dovetail groove mechanism 18.Micro-power wireless communication module 7 is connected with FQ14 aviation plug 11 by plug connector 8, communication cable 9, and FQ14 aviation plug 11 connects the FQ14 aviation interface 12 that mirror body 2 is installed under the transit, is connected with the transit mainboard by the RS232 interface in it.Connect 80mm spiral SMA antenna 6 on the micro-power wireless communication module 7, receive and dispatch the data that transits are gathered by 80mm spiral SMA antenna 6.Set up regularly options button 16 above transit is gathered key 17, the real-time acquisition time step-length is 15s, 20s, 30s, 60s.
The data that the utility model collected are transferred to PC or special-purpose hand-held calculator by wireless module 7.When needs with transit in data all extract, also can by wireless module with data transmission to PC or special-purpose hand-held calculator.When not needing to adopt wireless module transmission data, also can use client cables that transit is connected with PC or special-purpose hand-held calculator, realize the two-way communication function of data.
Claims (1)
1. wireless optical pilot balloon theodolite, comprise and be provided with the body on show that primary telescope, auxiliary telescope, change times mechanism are provided with wheel, pitch rotation wheel, be provided with that azimuth rotation is provided with runner, the mechanism of making zero is provided with runner, the data acquisition storage system is provided with interface, the following mirror body of data acquisition key, it is characterized in that: a dovetail groove mechanism is installed on body on show right side, and the micro-power wireless communication module is assembled on the body on show by dovetail groove mechanism; The micro-power wireless communication module connects the interface on the mirror body under the transit by communication cable, and interface is connected with the transit mainboard; Connect 80mm spiral SMA antenna on the micro-power wireless communication module.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010202236707U CN201748917U (en) | 2010-06-12 | 2010-06-12 | Wireless optical pilot balloon theodolite |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010202236707U CN201748917U (en) | 2010-06-12 | 2010-06-12 | Wireless optical pilot balloon theodolite |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201748917U true CN201748917U (en) | 2011-02-16 |
Family
ID=43583592
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010202236707U Expired - Fee Related CN201748917U (en) | 2010-06-12 | 2010-06-12 | Wireless optical pilot balloon theodolite |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201748917U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104613928A (en) * | 2015-02-09 | 2015-05-13 | 中国人民解放军63863部队 | Automatic tracking and air measurement method for optical pilot balloon theodolite |
| CN112097802A (en) * | 2020-08-05 | 2020-12-18 | 沈阳第三三零一装备制造有限公司 | Composite photoelectric code disc device |
-
2010
- 2010-06-12 CN CN2010202236707U patent/CN201748917U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104613928A (en) * | 2015-02-09 | 2015-05-13 | 中国人民解放军63863部队 | Automatic tracking and air measurement method for optical pilot balloon theodolite |
| CN112097802A (en) * | 2020-08-05 | 2020-12-18 | 沈阳第三三零一装备制造有限公司 | Composite photoelectric code disc device |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN201948153U (en) | Automatic parasol capable of tracking pitch angle and azimuth of the sun | |
| CN203780780U (en) | Solar underwater robot | |
| CN201653423U (en) | Water flow tracking measurement buoy | |
| CN104122117A (en) | Automatic river and lake water sample control acquisition system based on multi-rotor-wing unmanned aerial vehicle | |
| CN201748917U (en) | Wireless optical pilot balloon theodolite | |
| CN201594146U (en) | Automatic snowfall monitoring device | |
| CN201444154U (en) | Intelligent monitoring detecting system capable of realizing over-water positioning or cruising | |
| CN102305621A (en) | Hydrological comprehensive measurement device | |
| CN204347514U (en) | A kind of water conservancy information intelligent telemetry terminal system based on multi-channel data acquisition | |
| CN102923295A (en) | Method for mooring radar by kite high altitude | |
| CN203864985U (en) | Unmanned measurement and control ship and unmanned measurement and control system | |
| CN202256722U (en) | Multi-parameter surface drifting buoy | |
| CN205212941U (en) | Satellite sensing wild animal tracer | |
| CN209486331U (en) | A kind of maritime meteorology and Hydrological observation system | |
| CN201328115Y (en) | Wireless data transmission system for total station | |
| CN208077010U (en) | A kind of novel hydrometeorological observation system | |
| CN206832249U (en) | Portable floating type hydrology current surveying device | |
| CN202650224U (en) | Power image recognition type meter reading instrument | |
| CN207923679U (en) | A kind of wind profile instrument based on LoRa | |
| CN208508614U (en) | A kind of icing monitoring and warning system | |
| CN206638262U (en) | A kind of high efficiency hydrologic monitoring device | |
| CN202092680U (en) | Comprehensive transmission line monitoring device with three-dimensional attitude sensor | |
| CN201878058U (en) | Wind and solar complementary device for marine data buoy | |
| CN202232369U (en) | Movable type weather modification operation commanding device | |
| CN204859418U (en) | Meadow quadrat chart is like automatic acquisition equipment |
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: 20110216 Termination date: 20120612 |