CN105783893A - Infrared compass position indicator - Google Patents
Infrared compass position indicator Download PDFInfo
- Publication number
- CN105783893A CN105783893A CN201610354391.6A CN201610354391A CN105783893A CN 105783893 A CN105783893 A CN 105783893A CN 201610354391 A CN201610354391 A CN 201610354391A CN 105783893 A CN105783893 A CN 105783893A
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- CN
- China
- Prior art keywords
- connects
- compass
- infrared
- generator
- location
- 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.)
- Pending
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Classifications
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C17/00—Compasses; Devices for ascertaining true or magnetic north for navigation or surveying purposes
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- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Length Measuring Devices By Optical Means (AREA)
- Photometry And Measurement Of Optical Pulse Characteristics (AREA)
Abstract
The invention discloses an infrared compass position indicator. A compass is flatwise placed on a movable disc frame, the movable disc frame is internally provided with a cross transparent movable disc and a cross position line, a positioning bottom lower base is connected with a positioning bottom upper base, the positioning bottom upper base is connected with a pitching support, the pitching support is connected with a vertical angle fixing rotary knob and a generator fixing table, the generator fixing table is connected with a fixing table rotary handle and a hard light infrared generator, the hard light infrared generator is connected with a hard light infrared switch and a sighting device base, the sighting device base is connected with a sighting telescope outer body, and the sighting telescope outer body is internally provided with a sighting telescope and connected with a low light infrared switch, a light beam vertical fine adjustment rotary knob and a light beam transverse fine adjustment rotary knob; the sighting telescope is viewed through eyes, the vertical angle of an observation target is determined by adjusting the pitching support, the transverse angle is adjusted according to the exact position of the target, and the cross position line can accurately point the week/day degree on the compass with angular variation. The infrared compass position indicator has the advantage that accuracy of the measurement direction angle is improved by ten times or more.
Description
Technical field
The invention belongs to compass and manufacture field, be specifically related to infrared ray compass position finder.
Background technology
Known compass, when measuring orientation angle, is continued to use traditional range estimation and bracing wire localization method always, be there is complex operation, the defect that error is bigger, this drawback there is no good technical scheme so far and solve.
Summary of the invention
The infrared ray compass position finder of the present invention, has invented cross transparent active dish and compass and RF transmitter link has been integrated, improved certainty of measurement dramatically, simplify operation sequence, and its error can control within 0.3 degree.
The present invention has used high light and two kinds of location modes of the low light level, to be suitable for closely and measurement demands different at a distance, can carry out the adjustment of upper and lower observation angle, to adapt to being accurately positioned different target such as massif, river, building and road simultaneously.
In order to achieve the above object, the infrared ray compass position finder of the present invention is achieved in that movable disk framework keeps flat on compass, cross transparent active dish is set in movable disk framework, cross location line, seat under cross transparent active disk center's internal layer connection location, under location, seat connects the seat of honour, the end, location, the seat of honour, the end, location connects tilt mount, tilt mount connects upper lower angle fixed knob, generator fixed station, generator fixed station connects fixed station swing handle, high light infrared generator, high light infrared generator connects high light infrared switch, high light infrared generator connects sight base, sight base connects gun sight ectosome, gun sight is internal outward sets gun sight, gun sight ectosome connects low light level infrared switch, the upper and lower vernier knob of light beam, light beam left and right vernier knob.
nullOperation sequence: first make the centrage in compass Tianchi overlap with magnetic needle，Reserve and sit to Zhou Tiandu，Movable frame is lain on compass，Four limits overlap，Under location, seat is interconnection function with its function of the seat of honour, the end, location，Open infrared switch，High light is made quasi goal or eye to be looked the outer internal gun sight low light level of gun sight to quasi goal，The upper lower angle of observed object is determined by adjusting fixed station tilt mount，Tighten lower angle fixed knob on tilt mount,Strong and weak light can open and use simultaneously，The use of infrared facility is selected also dependent on distance,If closely observing，It is suitable for using high light infrared generator，Open high light infrared switch,Strong beam is allowed directly to be incident upon on measured target，If distant object，It is suitable for using the ultrared gun sight of the low light level，Open low light level infrared switch，The low light level can be incident upon in gun sight scope imageable target，Because being in scope imaging，So not kept clear location by the impact of light beam projection distance and sunlight power,Holding high light infrared generator fixed station swing handle drives the transparent dynamic movable disk of cross and the whole Conjoint packing for wine of RF transmitter circumferentially to move by laterally pulling shank，Left and right angle is adjusted according to concrete orientation, target place，Until fully aligned measured target，Cross location line in cross transparent active dish can with orientation angles change it is thus possible to all skies number of degrees accurately pointed on compass,In gun sight, infrared projection point should be substantially parallel to overlap with cross location line and could correctly observe location，If there being error，Then with the upper and lower vernier knob of light beam、Light beam left and right vernier knob is finely tuned，It is mainly used in arranging adjustment when dispatching from the factory.
The infrared ray compass position finder of the present invention provides the benefit that: greatly simplifie the operation sequence of conventional compass, improves measurement orientation angle degree of accuracy more than ten times.
Below in conjunction with the drawings and specific embodiments, the infrared ray compass position finder of the present invention is described in further detail.
Accompanying drawing explanation
1. compass in figure, 2. movable disk framework, 3. cross transparent active dish, 4. cross location line, 5. seat under location, the 6. seat of honour, the end, location, 7. tilt mount, 8. goes up lower angle fixed knob, 9. generator fixed station, 10. fixed station swing handle, 11. high light infrared generators, 12. sight bases, 13. gun sight ectosome, 14. high light infrared switch, 15. gun sights, 16. low light level infrared switch, the 17. upper and lower vernier knobs of light beam, 18. light beam left and right vernier knobs.
Fig. 1 is the infrared ray compass position finder perspective view of the present invention；
Fig. 2 is infrared ray compass position finder stereochemical structure compass perspective view of the present invention；
Fig. 3 is infrared ray compass position finder stereochemical structure cross transparent active dish perspective view of the present invention.
Detailed description of the invention
nullAccording to Fig. 1、Fig. 2、The position finder of infrared ray compass shown in Fig. 3，Movable disk framework 2 keeps flat on compass 1，Cross transparent active dish 3 is set in movable disk framework 2、Cross location line 4，Cross transparent active dish 3 center internal layer connects seat 5 under location，Under location, seat 5 connects the seat of honour, the end 6, location，The seat of honour, the end 6, location connects tilt mount 7，Tilt mount 7 connects upper lower angle fixed knob 8、Generator fixed station 9，Generator fixed station 9 connects fixed station swing handle 10、High light infrared generator 11，High light infrared generator 11 connects high light infrared switch 14，High light infrared generator 11 connects sight base 12，Sight base 12 connects gun sight ectosome 13，Gun sight 15 is set in gun sight ectosome 13，Gun sight ectosome 13 connects low light level infrared switch 16、The upper and lower vernier knob 17 of light beam、Light beam left and right vernier knob 18.
Claims (1)
- null1. outside line compass position finder，It is characterized in that: movable disk framework (2) keeps flat on compass (1)，Cross transparent active dish (3) is set in movable disk framework (2)、Cross location line (4)，Cross transparent active dish (3) center internal layer connects seat (5) under location，Under location, seat (5) connects the seat of honour, the end, location (6)，The seat of honour, the end, location (6) connects tilt mount (7)，Tilt mount (7) connects upper and lower fixed knob (8)、Generator fixed station (9)，Generator fixed station (9) connects fixed station swing handle (10)、High light infrared generator (11)，High light infrared generator (11) connects high light infrared switch (14)，High light infrared generator (11) connects sight base (12)，Sight base (12) connects gun sight ectosome (13)，Gun sight (15) is set in gun sight ectosome (13)，Gun sight ectosome (13) connects low light level infrared switch (16)、The upper and lower vernier knob of light beam (17)、Light beam left and right vernier knob (18).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610354391.6A CN105783893A (en) | 2016-05-26 | 2016-05-26 | Infrared compass position indicator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610354391.6A CN105783893A (en) | 2016-05-26 | 2016-05-26 | Infrared compass position indicator |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105783893A true CN105783893A (en) | 2016-07-20 |
Family
ID=56379442
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610354391.6A Pending CN105783893A (en) | 2016-05-26 | 2016-05-26 | Infrared compass position indicator |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105783893A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109202355A (en) * | 2018-11-05 | 2019-01-15 | 无锡华联科技集团有限公司 | A kind of rib of slab weld seam cursor positioning mechanism |
| CN112665611A (en) * | 2020-12-17 | 2021-04-16 | 陕西宝成航空仪表有限责任公司 | Airborne magnetic compass azimuth error calibration device |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20020147565A1 (en) * | 2001-04-05 | 2002-10-10 | Zander Dennis R. | Block signal and train proximity detector |
| TW570187U (en) * | 2003-05-13 | 2004-01-01 | Chau-Sheng Jung | Improved compass structure with an infrared indication device |
| CN203687951U (en) * | 2013-11-11 | 2014-07-02 | 詹顺荣 | Green laser positioning compasser |
| CN205679235U (en) * | 2016-05-26 | 2016-11-09 | 张健 | Infrared ray compass position finder |
-
2016
- 2016-05-26 CN CN201610354391.6A patent/CN105783893A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20020147565A1 (en) * | 2001-04-05 | 2002-10-10 | Zander Dennis R. | Block signal and train proximity detector |
| TW570187U (en) * | 2003-05-13 | 2004-01-01 | Chau-Sheng Jung | Improved compass structure with an infrared indication device |
| CN203687951U (en) * | 2013-11-11 | 2014-07-02 | 詹顺荣 | Green laser positioning compasser |
| CN205679235U (en) * | 2016-05-26 | 2016-11-09 | 张健 | Infrared ray compass position finder |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109202355A (en) * | 2018-11-05 | 2019-01-15 | 无锡华联科技集团有限公司 | A kind of rib of slab weld seam cursor positioning mechanism |
| CN112665611A (en) * | 2020-12-17 | 2021-04-16 | 陕西宝成航空仪表有限责任公司 | Airborne magnetic compass azimuth error calibration device |
| CN112665611B (en) * | 2020-12-17 | 2022-10-25 | 陕西宝成航空仪表有限责任公司 | Airborne magnetic compass azimuth error calibration device |
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| C10 | Entry into substantive examination | ||
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| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20160720 |
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| WD01 | Invention patent application deemed withdrawn after publication |