CN116443287A - Surveying instrument mounting structure of unmanned aerial vehicle survey and drawing - Google Patents
Surveying instrument mounting structure of unmanned aerial vehicle survey and drawing Download PDFInfo
- Publication number
- CN116443287A CN116443287A CN202310414102.7A CN202310414102A CN116443287A CN 116443287 A CN116443287 A CN 116443287A CN 202310414102 A CN202310414102 A CN 202310414102A CN 116443287 A CN116443287 A CN 116443287A
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- aerial vehicle
- unmanned aerial
- surveying instrument
- sliding
- surveying
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- 238000009434 installation Methods 0.000 claims abstract description 28
- 230000007246 mechanism Effects 0.000 claims abstract description 18
- 238000013507 mapping Methods 0.000 claims description 33
- 238000003780 insertion Methods 0.000 claims description 17
- 230000037431 insertion Effects 0.000 claims description 17
- 230000001681 protective effect Effects 0.000 claims description 10
- 230000009471 action Effects 0.000 abstract description 11
- 238000010586 diagram Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000007726 management method Methods 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/80—Arrangement of on-board electronics, e.g. avionics systems or wiring
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
- B64U10/16—Flying platforms with five or more distinct rotor axes, e.g. octocopters
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/80—Arrangement of on-board electronics, e.g. avionics systems or wiring
- B64U20/87—Mounting of imaging devices, e.g. mounting of gimbals
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
- B64U2101/32—UAVs specially adapted for particular uses or applications for imaging, photography or videography for cartography or topography
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
The invention discloses a surveying instrument mounting structure for unmanned aerial vehicle surveying, which comprises an unmanned aerial vehicle body, a surveying instrument body and a surveying instrument head, and further comprises the following components: the plug-in mounting mechanism and the rotating mechanism; the splicing installation mechanism comprises an installation transverse plate and two fixed plugboards, wherein one side of each fixed plugboard is connected with a first triangular block, and two sides of the installation transverse plate are connected with sliding plugboards in a sliding manner. According to the invention, through the action of the plugging installation mechanism, according to the plugging installation modes, the surveying instrument body can be directly subjected to sliding plugging installation according to the action of the fixed plugboard, and compared with the screw installation mode, the screw installation mode does not need a worker to screw the screw by means of a tool, and the installation of the worker is correspondingly facilitated, so that the working efficiency of the worker for installing the surveying instrument body and the unmanned aerial vehicle body is improved, and the working efficiency of the worker for surveying by using the surveying instrument body is improved.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicle surveying and mapping, in particular to a surveying instrument mounting structure for unmanned aerial vehicle surveying and mapping.
Background
The surveying and mapping literal is understood as measurement and drawing, which is based on computer technology, photoelectric technology, network communication technology, space science and information science, and uses Global Navigation Satellite System (GNSS), remote Sensing (RS) and Geographic Information System (GIS) 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 a measuring means for engineering construction, planning design and administrative management.
At present widely used unmanned aerial vehicle carries on the surveying instrument and surveys, utilize unmanned aerial vehicle's flight, do not need the staff to run the survey and drawing, corresponding staff of being convenient for surveys and draws required place, but at present the mounting means of surveying instrument and unmanned aerial vehicle installs through the screw generally, corresponding needs are with the help of screwing up the instrument and carry out fixed mounting to the two, be inconvenient for the staff to reduce the staff and to carry out the work efficiency of installing surveying instrument and unmanned aerial vehicle, corresponding reduction staff uses the work efficiency that the surveying instrument surveyed, for this reason, propose the surveying instrument mounting structure of unmanned aerial vehicle survey and drawing.
Disclosure of Invention
The invention aims to solve the problems that the two are fixed and installed by means of a screw, a worker cannot conveniently install the two by means of a tightening tool, and the working efficiency of installing a surveying instrument and an unmanned aerial vehicle by the worker is reduced.
In order to achieve the above purpose, the present invention adopts the following technical scheme:
the utility model provides a surveying instrument mounting structure of unmanned aerial vehicle survey, includes unmanned aerial vehicle body, surveying instrument body and surveying instrument head, still including: the plug-in mounting mechanism and the rotating mechanism;
the plug-in mounting mechanism comprises a mounting transverse plate and two fixing plug plates, one side of each fixing plug plate is connected with a first triangular block, two sides of each mounting transverse plate are connected with sliding plug plates in a sliding mode, one end of each sliding plug plate is connected with a second triangular block, two sides of each sliding plug plate are fixedly connected with extension springs, one end, far away from the second triangular block, of each sliding plug plate is connected with a protective shell, and one side of each protective shell is connected with an L-shaped sleeve and an L-shaped sliding rod respectively.
Preferably, the rotating mechanism comprises a rotating shaft, the outer side wall of the rotating shaft is fixedly connected with a fixed disc, a connecting rope is connected to the fixed disc, and one end, far away from the fixed disc, of the connecting rope is connected with a fixing bolt.
Preferably, the mounting cross plate is fixedly mounted at the bottom end of the rotating shaft, and the fixing plugboard is fixedly mounted at the top of the surveying instrument body.
Preferably, one sides of the first triangular block and the second triangular block are obliquely arranged, and one sides of the first triangular block and the second triangular block are in sliding fit.
Preferably, the installation diaphragm is provided with a slot, the sliding plugboard slides and extends to the inside of the slot, the second triangular block is located in the slot, and the outer side wall of the fixed plugboard and the inner side wall of the slot are in sliding fit.
Preferably, one end of the extension spring, which is far away from the sliding plugboard, is connected to the outer wall of the mounting transverse plate, and the extension spring and the sliding plugboard are both located in the protective shell.
Preferably, a sliding groove is formed in one end of the L-shaped sleeve, the L-shaped sliding rod extends to the inside of the L-shaped sleeve through the sliding groove, and the L-shaped sliding rod is in sliding connection with the L-shaped sleeve through the sliding groove.
Preferably, a plurality of screw holes have all been seted up to the bottom of fixed disk and unmanned aerial vehicle body, and a plurality of the screw hole is for corresponding the setting, fixing bolt passes through the screw hole and fixes fixed disk and unmanned aerial vehicle body.
Compared with the prior art, the invention has the beneficial effects that:
according to the mapping instrument mounting structure for unmanned aerial vehicle mapping, according to the matching action between the plugging mounting mechanism and the rotating mechanism, according to the plugging mounting modes, the mapping instrument body can be directly subjected to sliding plugging mounting according to the action of the fixed plug board, compared with the screw mounting mode, the screw mounting mode does not need to be screwed down by workers by means of tools, the mounting of the workers is correspondingly facilitated, and therefore the working efficiency of the workers for mounting the mapping instrument body and the unmanned aerial vehicle body is improved, the working efficiency of the workers for mapping by using the mapping instrument body is improved, meanwhile, according to the action of the rotating shaft, the angle of the mapping instrument head on one side of the mapping instrument body can be adjusted at will, corresponding mapping places required in different directions can be adjusted without the workers for adjusting the direction of the unmanned aerial vehicle body when the unmanned aerial vehicle body is in flight, the angle can be adjusted directly when the unmanned aerial vehicle body is mounted, the operation steps of the workers are correspondingly reduced, the unmanned aerial vehicle body is avoided, and the direction of the workers is not convenient to adjust due to higher flying heights.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings that are needed in the embodiments will be briefly described below, it being understood that the following drawings only illustrate some examples of the present invention and therefore should not be considered as limiting the scope, and other related drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.
Fig. 1 is a schematic structural diagram of a mapping instrument mounting structure for unmanned aerial vehicle mapping;
fig. 2 is a schematic structural diagram of a surveying instrument body separated from an unmanned aerial vehicle body according to a surveying instrument installation structure for unmanned aerial vehicle surveying;
fig. 3 is a schematic bottom structural view of a mapping instrument mounting structure for unmanned aerial vehicle mapping according to the present invention;
fig. 4 is an enlarged view of a position a of a mapping instrument installation structure diagram 3 for unmanned aerial vehicle mapping;
fig. 5 is a schematic view of a plane-down cut structure of a mapping instrument mounting structure for unmanned aerial vehicle mapping;
fig. 6 is a schematic cross-sectional view of a mounting cross plate of a mapping instrument mounting structure for unmanned aerial vehicle mapping.
In the figure 1, an unmanned aerial vehicle body; 2. a rotating shaft; 201. a fixed plate; 202. a connecting rope; 203. a fixing bolt; 3. a mapper body; 301. a mapping instrument head; 4. mounting a transverse plate; 401. fixing the plugboard; 402. a first triangular block; 403. sliding plugboards; 404. a second triangular block; 405. a tension spring; 406. a protective shell; 407. an L-shaped sleeve; 408. an L-shaped slide bar.
Detailed Description
For the purpose of making the objects, technical solutions and advantages of the embodiments of the present invention more apparent, the technical solutions of the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention, and it is apparent that the described embodiments are some embodiments of the present invention, but not all embodiments. All other embodiments, based on the embodiments of the invention, which are apparent to those of ordinary skill in the art without inventive faculty, are intended to be within the scope of the invention.
As shown in fig. 1, fig. 2, fig. 3, fig. 5, and fig. 6, a mapping instrument mounting structure for mapping by using an unmanned aerial vehicle, which comprises an unmanned aerial vehicle body 1, a mapping instrument body 3, and a mapping instrument head 301, and further comprises: the plug-in mounting mechanism and the rotating mechanism; the splicing installation mechanism comprises an installation transverse plate 4 and two fixed insertion plates 401, wherein one side of each fixed insertion plate 401 is connected with a first triangular block 402, two sides of each installation transverse plate 4 are connected with a sliding insertion plate 403 in a sliding manner, one end of each sliding insertion plate 403 is connected with a second triangular block 404, two sides of each sliding insertion plate 403 are fixedly connected with extension springs 405, one end, far away from each second triangular block 404, of each sliding insertion plate 403 is connected with a protective shell 406, and one side of each protective shell 406 is respectively connected with an L-shaped sleeve 407 and an L-shaped sliding rod 408;
the invention is further specifically detailed, one side of the first triangular block 402 and one side of the second triangular block 404 are obliquely arranged, the oblique side of the first triangular block 402 and the oblique side of the second triangular block 404 are in sliding fit, a slot is formed in the mounting transverse plate 4, the sliding insertion plate 403 extends into the slot in a sliding manner, the second triangular block 404 is positioned in the slot, the outer side wall of the fixed insertion plate 401 and the inner side wall of the slot are in sliding fit, one end of the extension spring 405, which is far away from the sliding insertion plate 403, is connected to the outer wall of the mounting transverse plate 4, the extension spring 405 and the sliding insertion plate 403 are both positioned in the protective shell 406, one end of the L-shaped sleeve 407 is provided with a sliding groove, the L-shaped sliding rod 408 extends into the L-shaped sleeve 407 through the sliding groove, and the L-shaped sliding rod 408 is in sliding connection with the L-shaped sleeve 407 through the sliding groove;
through the arrangement of the technical scheme, according to the plugging installation modes, the surveying instrument body 3 can be directly subjected to sliding plugging installation according to the action of the fixing plugboard 401, and compared with the screw installation mode, a worker does not need to screw the screws by means of tools, and the installation is correspondingly convenient for the worker, so that the working efficiency of the worker for installing the surveying instrument body 3 and the unmanned aerial vehicle body 1 is improved, and the working efficiency of the worker for surveying by using the surveying instrument body 3 is improved;
as shown in fig. 1, 3 and 4, the rotating mechanism comprises a rotating shaft 2, the outer side wall of the rotating shaft 2 is fixedly connected with a fixed disc 201, a connecting rope 202 is connected to the fixed disc 201, and one end, far away from the fixed disc 201, of the connecting rope 202 is connected with a fixing bolt 203;
the invention is further specifically detailed, the mounting transverse plate 4 is fixedly arranged at the bottom end of the rotating shaft 2, the fixing plugboard 401 is fixedly arranged at the top of the surveying instrument body 3, a plurality of threaded holes are formed in the bottoms of the fixing disc 201 and the unmanned aerial vehicle body 1, the threaded holes are correspondingly arranged, and the fixing bolt 203 is used for fixing the fixing disc 201 and the unmanned aerial vehicle body 1 through the threaded holes;
through the setting of above-mentioned technical scheme, according to axis of rotation 2's effect, can carry out angle of adjustment at will to the surveying instrument head 301 of surveying instrument body 3 one side, corresponding when unmanned aerial vehicle body 1 flies, to the place of the required survey of different directions, need not the staff and adjust unmanned aerial vehicle body 1's direction, directly can angle of adjustment when installing it, corresponding operation steps that have reduced the numerous staff, avoid unmanned aerial vehicle body 1 because of fly height is higher, inconvenient staff carries out direction of adjustment.
As shown in fig. 1-6, the functional principle of the present invention can be illustrated by the following operation: when a worker installs the surveying instrument body 3 and the unmanned aerial vehicle body 1, the surveying instrument body 3 is directly inserted into the slot on the installation transverse plate 4 through the fixing insertion plate 401, along with the action of the fixing insertion plate 401 inserted into the slot, the first triangular block 402 is contacted with the inclined side of the second triangular block 404, the first triangular block 402 extrudes the second triangular block 404 according to the action of the sliding fit arrangement of the inclined side of the first triangular block 402 and the inclined side of the second triangular block 404, the second triangular block 404 correspondingly slides to the outer side of the installation transverse plate 4, so that the first triangular block 402 slides to the upper side of the second triangular block 404, at the moment, the second triangular block 404 returns to the initial position according to the action of the sliding insertion plate 403 and the extension spring 405, and is blocked on the first triangular block 402, at the moment, the top of the surveying instrument body 3 is attached to the bottom of the installation transverse plate 4, the surveying instrument body 3 and the unmanned aerial vehicle body 1 can be fixedly installed, by the setting of the technical scheme, the surveying instrument body 3 can be directly installed according to the action of the installation screw 3 of the surveying instrument by the installation method, the corresponding worker can be directly installed by the surveying instrument body 3 according to the installation method of the sliding screw 3, and the operator is not required to install the corresponding screw 3 by the personnel, and the worker is convenient to install the surveying instrument by screwing the worker;
after the installation of the surveying instrument body 3 and the unmanned aerial vehicle body 1 is completed, the rotation shaft 2 is rotated, the surveying instrument head 301 on one side of the surveying instrument body 3 can be adjusted, after the angle adjustment is completed, the fixing bolt 203 is directly screwed into the threaded hole manually, so that the rotation shaft 2 is fixed at an angle, through the arrangement of the technical scheme, the surveying instrument head 301 on one side of the surveying instrument body 3 can be adjusted at will, corresponding positions of the surveying instrument body 1 which need to be surveyed in different directions are correspondingly flown up, the direction of the unmanned aerial vehicle body 1 is not required to be adjusted by a worker, the angle can be adjusted directly when the unmanned aerial vehicle body is installed, the operation steps of the worker are correspondingly reduced, and the unmanned aerial vehicle body 1 is prevented from being adjusted by the worker due to higher flying height, and the direction is inconvenient to the worker;
the fixing action of the fixing plate 201 on the rotating shaft 2 by the fixing bolt 203 is relatively low, and only a worker needs to manually screw the fixing plate.
The foregoing is only a preferred embodiment of the present invention, but the scope of the present invention is not limited thereto, and any person skilled in the art, who is within the scope of the present invention, should make equivalent substitutions or modifications according to the technical scheme of the present invention and the inventive concept thereof, and should be covered by the scope of the present invention.
Claims (8)
1. The utility model provides a surveying instrument mounting structure of unmanned aerial vehicle survey, includes unmanned aerial vehicle body (1), surveying instrument body (3) and surveying instrument head (301), its characterized in that, still including: the plug-in mounting mechanism and the rotating mechanism;
the utility model provides a socket mounting mechanism is including installation diaphragm (4) and two fixed picture peg (401), one side of fixed picture peg (401) is connected with first triangular block (402), the both sides sliding connection of installation diaphragm (4) has slip picture peg (403), the one end of slip picture peg (403) is connected with second triangular block (404), the both sides fixedly connected with extension spring (405) of slip picture peg (403), the one end that second triangular block (404) was kept away from to slip picture peg (403) is connected with protective housing (406), two one side of protective housing (406) is connected with L type sleeve (407) and L slide bar (408) respectively.
2. The surveying instrument mounting structure for unmanned aerial vehicle surveying and mapping according to claim 1, wherein the rotating mechanism comprises a rotating shaft (2), a fixed disc (201) is fixedly connected to the outer side wall of the rotating shaft (2), a connecting rope (202) is connected to the fixed disc (201), and a fixing bolt (203) is connected to one end, far away from the fixed disc (201), of the connecting rope (202).
3. The surveying instrument mounting structure of unmanned aerial vehicle survey according to claim 2, wherein the mounting cross plate (4) is fixedly mounted at the bottom end of the rotating shaft (2), and the fixing insert plate (401) is fixedly mounted at the top of the surveying instrument body (3).
4. The mapping instrument mounting structure for mapping by using the unmanned aerial vehicle according to claim 1, wherein one side of the first triangular block (402) and one side of the second triangular block (404) are arranged in an inclined manner, and the inclined sides of the first triangular block (402) and the second triangular block (404) are arranged in a sliding fit manner.
5. The surveying instrument mounting structure for unmanned aerial vehicle surveying and mapping according to claim 1, wherein the mounting cross plate (4) is provided with a slot, the sliding insertion plate (403) slides and extends to the inside of the slot, the second triangular block (404) is located in the inside of the slot, and the outer side wall of the fixing insertion plate (401) is in sliding fit with the inner side wall of the slot.
6. The surveying instrument mounting structure according to claim 1, wherein one end of the extension spring (405) away from the sliding insertion plate (403) is connected to the outer wall of the mounting cross plate (4), and both the extension spring (405) and the sliding insertion plate (403) are located in the protective shell (406).
7. The surveying instrument mounting structure for unmanned aerial vehicle surveying and mapping according to claim 1, wherein a sliding groove is formed in one end of the L-shaped sleeve (407), the L-shaped sliding rod (408) extends to the inside of the L-shaped sleeve (407) through the sliding groove, and the L-shaped sliding rod (408) is slidably connected with the L-shaped sleeve (407) through the sliding groove.
8. The surveying instrument mounting structure for unmanned aerial vehicle surveying and mapping according to claim 2, wherein a plurality of threaded holes are formed in the bottoms of the fixing disc (201) and the unmanned aerial vehicle body (1), the threaded holes are correspondingly formed, and the fixing bolts (203) fix the fixing disc (201) and the unmanned aerial vehicle body (1) through the threaded holes.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310414102.7A CN116443287A (en) | 2023-04-18 | 2023-04-18 | Surveying instrument mounting structure of unmanned aerial vehicle survey and drawing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310414102.7A CN116443287A (en) | 2023-04-18 | 2023-04-18 | Surveying instrument mounting structure of unmanned aerial vehicle survey and drawing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN116443287A true CN116443287A (en) | 2023-07-18 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202310414102.7A Pending CN116443287A (en) | 2023-04-18 | 2023-04-18 | Surveying instrument mounting structure of unmanned aerial vehicle survey and drawing |
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| CN (1) | CN116443287A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117232487A (en) * | 2023-11-09 | 2023-12-15 | 惠州市大禹工程质量检测中心有限公司 | Topography measuring equipment for hydraulic engineering |
-
2023
- 2023-04-18 CN CN202310414102.7A patent/CN116443287A/en active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117232487A (en) * | 2023-11-09 | 2023-12-15 | 惠州市大禹工程质量检测中心有限公司 | Topography measuring equipment for hydraulic engineering |
| CN117232487B (en) * | 2023-11-09 | 2024-01-26 | 惠州市大禹工程质量检测中心有限公司 | Topography measuring equipment for hydraulic engineering |
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