CN219635507U - Convenient site selection mapping device - Google Patents
Convenient site selection mapping device Download PDFInfo
- Publication number
- CN219635507U CN219635507U CN202320920582.XU CN202320920582U CN219635507U CN 219635507 U CN219635507 U CN 219635507U CN 202320920582 U CN202320920582 U CN 202320920582U CN 219635507 U CN219635507 U CN 219635507U
- Authority
- CN
- China
- Prior art keywords
- aircraft
- groove
- mapping
- reset
- clamping
- 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.)
- Active
Links
- 238000013507 mapping Methods 0.000 title claims abstract description 42
- 230000002457 bidirectional effect Effects 0.000 claims description 11
- 230000001681 protective effect Effects 0.000 claims description 9
- 230000002093 peripheral effect Effects 0.000 claims description 3
- 230000000694 effects Effects 0.000 claims 2
- 238000010248 power generation Methods 0.000 claims 1
- 241000256626 Pterygota <winged insects> Species 0.000 abstract description 2
- 230000007246 mechanism Effects 0.000 description 10
- 238000000034 method Methods 0.000 description 5
- 230000009471 action Effects 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 241000238631 Hexapoda Species 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000007726 management method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Landscapes
- Stereoscopic And Panoramic Photography (AREA)
Abstract
The utility model relates to the technical field of mapping, and discloses a convenient site selection mapper which comprises an aircraft and mapping equipment. Set up the handle on the aircraft, conveniently carry the body of aircraft, carry out the centre gripping with mapping equipment and aircraft and assemble, carry mapping equipment by the aircraft and carry high altitude survey and drawing operation, need not personnel's in person, when pulling buffer gear, make buffer gear drive the draw-down of card pole that resets, thereby make the protection casing can insert between mounting and the splint one, loosen buffer gear afterwards, reset card pole and rebound under the support of supporting the pressure spring, thereby fix the protection casing, and the setting of protection casing can avoid the winged insect to strike the camera lens on the mapping equipment, the mapping that causes is taken fuzzily or has the problem of foreign matter, and buffer gear is when the aircraft descends, contact with ground at first, thereby reduce the aircraft and the hard straightness that takes place with ground contact when descending, the mapping equipment that the impact force caused when having reduced to descend receives vibration damage.
Description
Technical Field
The utility model relates to the technical field of mapping, in particular to a convenient site selection mapper.
Background
The surveying and mapping literal is understood as measuring and drawing, which is based on computer technology, photoelectric technology, network communication technology, space science and information science, and uses global navigation satellite positioning system, remote sensing and geographic information system as technical cores, and selects the existing characteristic points and boundary lines of the ground and obtains the graph and position information reflecting the ground current situation through measuring means for engineering construction, planning design and administrative management.
When the prior surveying instrument is used, a surveying staff usually brings the device to a place where surveying work needs to be performed, and surveying work is performed, but under the actual condition, the situation of many places is dangerous, the device is not easy to climb, certain danger exists, and the operation is very inconvenient. Accordingly, one skilled in the art would provide a convenient site-selection mapper to address the problems set forth in the background above.
Disclosure of Invention
(one) solving the technical problems
Aiming at the defects of the prior art, the utility model provides a convenient site selection mapper for solving the problems in the background art.
(II) technical scheme
In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides a convenient site selection plotter, includes aircraft, mapping equipment, carries out the centre gripping with mapping equipment and aircraft and assembles, carries mapping equipment by the aircraft and carries out high altitude survey and drawing operation, the elasticity backplate is installed to aircraft upper portion wing week side, the handle is installed to aircraft week side, the I-shaped mount is installed to the aircraft bottom side, the movable groove has been seted up to I-shaped mount bottom inboard, be provided with bi-directional screw in the movable groove, splint two have been cup jointed on the bi-directional screw, I-shaped mount week side is provided with the mounting, mounting one side is provided with splint one, set up spacing logical groove in the mounting, be provided with reset clip in the spacing logical groove, buffer gear is installed to reset clip bottom.
Preferably, the protection casing has been centre gripping between mounting and the splint one, reset the draw-in lever and through spacing logical groove and mounting slip joint, reset draw-in lever week side cover is equipped with and supports the pressure spring, support the top lug fixed connection of pressure spring upper portion and reset draw-in lever, support the pressure spring bottom and support the pressure contact with spacing logical tank bottom inner wall, downward pulling buffer gear for buffer gear drives the draw-in lever pull-down that resets, thereby makes the protection casing can insert between mounting and the splint one, unclamps buffer gear afterwards, resets the draw-in lever and kick-backs the location under the pressure of supporting the pressure spring, thereby fixes the protection casing.
Preferably, a sliding clamping groove is formed in the top of the second clamping plate, and the second clamping plate is in sliding clamping connection with the I-shaped fixing frame through the sliding clamping groove.
Preferably, a thread sleeve is arranged in the sliding clamping groove, the bidirectional screw rod is in threaded connection with the two clamping plates through the thread sleeve, and the bidirectional screw rod is rotated to drive the two clamping plates to open and close, so that the surveying and mapping equipment body is clamped and fixed.
(III) beneficial effects
Compared with the prior art, the utility model provides a convenient site selection plotter, which comprises the following components
The beneficial effects are that:
through the design, the aircraft week side is provided with the handle, conveniently carry the body of aircraft, carry out the centre gripping with mapping equipment and aircraft and assemble, carry mapping equipment by the aircraft and carry high altitude survey and drawing operation, need not personnel's personally, when pulling buffer gear, make buffer gear drive the return clip pull, thereby make the protection casing can insert between mounting and the splint one, loosen buffer gear afterwards, the return clip is kick-backed under the support of supporting the pressure spring, thereby fix the protection casing, and the setting of protection casing can avoid the winged insect to strike the camera lens on the mapping equipment, the mapping that causes is shot fuzzily or has the problem of foreign matter, and buffer gear is in the time of the aircraft descends, contact with ground at first, thereby reduce the aircraft and the rigidity that takes place with ground contact when descending, the mapping equipment that the impact force caused when having reduced descends receives vibration damage.
Drawings
Fig. 1 is a schematic perspective view of a convenient site selection plotter according to an embodiment of the present utility model.
Fig. 2 is a schematic structural view of a handle in a convenient site-selection plotter according to an embodiment of the present utility model.
Fig. 3 is a schematic structural diagram of a protective cover in a convenient site selection plotter according to an embodiment of the utility model.
Fig. 4 is a schematic structural diagram of a bidirectional screw in a convenient site selection plotter according to an embodiment of the present utility model.
In the figure: 1. an aircraft; 2. an elastic guard plate; 3. a handle; 4. a fixing member; 401. a clamping plate I; 402. limiting through grooves; 403. a buffer mechanism; 404. resetting the clamping rod; 405. pressing the spring; 5. a protective cover; 6. i-shaped fixing frame; 601. a movable groove; 7. a bidirectional screw; 8. a clamping plate II; 801. a sliding clamping groove; 802. a thread sleeve; 9. a mapping device.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
The utility model provides a technical scheme, a convenient site selection mapper, please refer to fig. 1 and 3, which comprises an aircraft 1 and mapping equipment 9, wherein the mapping equipment 9 and the aircraft 1 are clamped and assembled, the aircraft 1 carries the mapping equipment 9 for high-altitude mapping operation, an elastic guard plate 2 is arranged on the peripheral side of an upper wing of the aircraft 1, and a handle 3 is arranged on the peripheral side of the aircraft 1;
referring to fig. 2, 3 and 4, an i-shaped fixing frame 6 is mounted at the bottom side of the aircraft 1, a movable groove 601 is formed at the inner side of the bottom end of the i-shaped fixing frame 6, a bidirectional screw 7 is arranged in the movable groove 601, a clamping plate II 8 is sleeved on the bidirectional screw 7, a fixing piece 4 is arranged at the periphery side of the i-shaped fixing frame 6, a clamping plate I401 is arranged at one side of the fixing piece 4, a limit through groove 402 is formed in the fixing piece 4, a reset clamping rod 404 is arranged in the limit through groove 402, a buffer mechanism 403 is mounted at the bottom of the reset clamping rod 404, a protective cover 5 is clamped between the fixing piece 4 and the clamping plate I401, the reset clamping rod 404 is in sliding clamping connection with the fixing piece 4 through the limiting through groove 402, a pressing spring 405 is sleeved on the periphery of the reset clamping rod 404, the upper portion of the pressing spring 405 is fixedly connected with a top protruding block of the reset clamping rod 404, the bottom of the pressing spring 405 is in pressing contact with the inner wall of the bottom of the limiting through groove 402, the buffer mechanism 403 is pulled downwards, the buffer mechanism 403 drives the reset clamping rod 404 to pull downwards, the protective cover 5 can be inserted between the fixing piece 4 and the clamping plate one 401, then the buffer mechanism 403 is loosened, and the reset clamping rod 404 is subjected to rebound positioning under the pressing of the pressing spring 405, so that the protective cover 5 is fixed;
referring to fig. 3 and 4, a sliding clamping groove 801 is formed in the top of the second clamping plate 8, the second clamping plate 8 is slidably clamped with the i-shaped fixing frame 6 through the sliding clamping groove 801, a threaded sleeve 802 is installed in the sliding clamping groove 801, the bidirectional screw 7 is in threaded connection with the second clamping plate 8 through the threaded sleeve 802, and the bidirectional screw 7 is rotated to drive the second clamping plates 8 to open and close, so that the body of the mapping equipment 9 is clamped and fixed.
The working principle of the device is as follows: the mapping equipment 9 and the aircraft 1 are clamped and assembled, the aircraft 1 carries the mapping equipment 9 to perform high-altitude mapping operation, the personnel do not need to personally and personally take, and the safety of mapping personnel is improved;
the bottom of the aircraft 1 is provided with the I-shaped fixing frame 6, a bidirectional screw rod 7 is arranged in a movable groove 601 in the I-shaped fixing frame 6, the two clamping plates II 8 are driven to open and close by rotating the bidirectional screw rod 7, so that the body of the surveying and mapping equipment 9 is clamped and fixed, then the buffer mechanism 403 is pulled downwards, the buffer mechanism 403 drives the reset clamping rod 404 to pull downwards, so that the protective cover 5 can be inserted between the fixing piece 4 and the clamping plate I401, then the buffer mechanism 403 is loosened, the reset clamping rod 404 is subjected to rebound positioning under the pressing of the pressing spring 405, so that the protective cover 5 is fixed, and the problem of fuzzy mapping shooting or foreign matter can be avoided due to the arrangement of the protective cover 5 when flying insects strike the lens on the surveying and mapping equipment 9;
further, a buffer mechanism 403 is arranged at the bottom of the fixing piece 4, and the buffer mechanism 403 is firstly contacted with the ground when the aircraft 1 descends, so that the rigidity of the aircraft 1, which is caused by the contact with the ground when the aircraft descends, is reduced, and the damage to the mapping equipment 9 caused by impact force during the descending is reduced;
and be provided with handle 3 in aircraft 1 week side to, conveniently carry the body of aircraft 1 to, mapping equipment 9 and aircraft 1 body firm in connection can carry together, need not to separately carry, cause the problem of carrying difficulty, further, be provided with the elasticity backplate 2 at the wing week side of aircraft 1, can protect it in carrying the in-process, avoid the wing to take place to damage, need not to carry out maintenance of careful wing, improved the portability of carrying.
It is noted that relational terms such as first and second, and the like are used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Moreover, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Although embodiments of the present utility model have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. Convenient site selection mapping ware, including aircraft (1), mapping equipment (9), its characterized in that: the utility model provides a low-cost electric power generation device, including aircraft (1), handle (3) are installed to aircraft (1) week side, I shape mount (6) are installed to aircraft (1) bottom side, activity groove (601) have been seted up to I shape mount (6) bottom inboard, be provided with bi-directional screw (7) in activity groove (601), cup joint splint two (8) on bi-directional screw (7), I shape mount (6) week side is provided with mounting (4), mounting (4) one side is provided with splint one (401), spacing logical groove (402) have been seted up in mounting (4), be provided with reset clip (404) in spacing logical groove (402), buffer gear (403) are installed to reset clip (404) bottom.
2. A portable site-directed mapping apparatus as set forth in claim 1, wherein: a protective cover (5) is clamped between the fixing piece (4) and the clamping plate I (401), the reset clamping rod (404) is in sliding clamping connection with the fixing piece (4) through the limiting through groove (402), and a pressing spring (405) is sleeved on the periphery of the reset clamping rod (404).
3. A portable site-directed mapping apparatus as set forth in claim 2, wherein: the upper part of the pressing spring (405) is fixedly connected with a top protruding block of the reset clamping rod (404), and the bottom of the pressing spring (405) is in pressing contact with the inner wall of the bottom of the limit through groove (402).
4. A portable site-directed mapping apparatus as set forth in claim 1, wherein: the top of the second clamping plate (8) is provided with a sliding clamping groove (801), and the second clamping plate (8) is in sliding clamping connection with the I-shaped fixing frame (6) through the sliding clamping groove (801).
5. A portable site-directed mapping apparatus as set forth in claim 4, wherein: a thread sleeve (802) is arranged in the sliding clamping groove (801), and the bidirectional screw (7) is in threaded connection with the clamping plate II (8) through the thread sleeve (802).
6. A portable site-directed mapping apparatus as set forth in claim 1, wherein: an elastic guard plate (2) is arranged on the peripheral side of the upper wing of the aircraft (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320920582.XU CN219635507U (en) | 2023-04-17 | 2023-04-17 | Convenient site selection mapping device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320920582.XU CN219635507U (en) | 2023-04-17 | 2023-04-17 | Convenient site selection mapping device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219635507U true CN219635507U (en) | 2023-09-05 |
Family
ID=87820252
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202320920582.XU Active CN219635507U (en) | 2023-04-17 | 2023-04-17 | Convenient site selection mapping device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219635507U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117902082A (en) * | 2024-03-19 | 2024-04-19 | 江苏新裕盛电子智能科技有限公司 | Unmanned aerial vehicle is used in survey and drawing with descending shock-absorbing function |
-
2023
- 2023-04-17 CN CN202320920582.XU patent/CN219635507U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117902082A (en) * | 2024-03-19 | 2024-04-19 | 江苏新裕盛电子智能科技有限公司 | Unmanned aerial vehicle is used in survey and drawing with descending shock-absorbing function |
| CN117902082B (en) * | 2024-03-19 | 2024-05-10 | 江苏新裕盛电子智能科技有限公司 | Unmanned aerial vehicle is used in survey and drawing with descending shock-absorbing function |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN219635507U (en) | Convenient site selection mapping device | |
| CN213543569U (en) | Follow-on surveying instrument adjusting device for engineering | |
| CN214372476U (en) | Unmanned aerial vehicle carries on topography mapping device of total powerstation | |
| CN208872305U (en) | A kind of total station | |
| CN108760754B (en) | Sucker type wall surface crack detection device and detection method | |
| CN116443287A (en) | Surveying instrument mounting structure of unmanned aerial vehicle survey and drawing | |
| CN112377376B (en) | Lightning protection system of wind generating set | |
| CN214893291U (en) | Portable topographic surveying and mapping device | |
| CN213462167U (en) | Dustproof construction of outdoor stereo set | |
| CN211977931U (en) | Portable equipment box for surveying instrument | |
| CN209812377U (en) | Shock-proof device for optical lens | |
| CN221024232U (en) | High flight survey and drawing unmanned aerial vehicle of security | |
| CN220472797U (en) | Environmental parameter measuring device under noisy environment | |
| CN213333137U (en) | A on-spot mapping device for real estate survey and drawing | |
| CN220884815U (en) | Automatic inspection equipment for photovoltaic field | |
| CN220489936U (en) | Drill rod with graduation | |
| CN215475754U (en) | Be used for surveying and mapping unmanned aerial vehicle that takes photo by plane | |
| CN211954130U (en) | Inclination angle sensor convenient to install for engineering machinery | |
| CN214138945U (en) | Unmanned aerial vehicle is patrolled and examined to electric power convenient to control | |
| CN220721397U (en) | Unmanned aerial vehicle data acquisition device for geological exploration | |
| CN217730763U (en) | Unmanned aerial vehicle equipment for pipeline inspection | |
| CN217484259U (en) | Concrete compactness detection device | |
| CN220501047U (en) | Mapping unmanned aerial vehicle with buffering protection function | |
| CN219178551U (en) | Inclination measuring device | |
| CN218847758U (en) | Constant-current sampler for environment detection |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |