CN220298783U - Video equipment clamping shock-absorbing structure for surveying and mapping unmanned aerial vehicle - Google Patents
Video equipment clamping shock-absorbing structure for surveying and mapping unmanned aerial vehicle Download PDFInfo
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- CN220298783U CN220298783U CN202322077140.6U CN202322077140U CN220298783U CN 220298783 U CN220298783 U CN 220298783U CN 202322077140 U CN202322077140 U CN 202322077140U CN 220298783 U CN220298783 U CN 220298783U
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- 238000013507 mapping Methods 0.000 title claims abstract description 23
- 230000007246 mechanism Effects 0.000 claims abstract description 84
- 238000013016 damping Methods 0.000 claims abstract description 39
- 230000000007 visual effect Effects 0.000 claims description 12
- 230000005540 biological transmission Effects 0.000 claims description 3
- 238000000034 method Methods 0.000 abstract description 8
- 230000008569 process Effects 0.000 abstract description 8
- 238000009434 installation Methods 0.000 description 6
- 230000035939 shock Effects 0.000 description 6
- 238000013459 approach Methods 0.000 description 2
- 230000003139 buffering effect Effects 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000002457 bidirectional effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000011900 installation process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
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- 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
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Abstract
The utility model relates to the technical field of unmanned aerial vehicle for surveying and mapping, and discloses a video equipment clamping damping structure for unmanned aerial vehicle for surveying and mapping, which comprises an unmanned aerial vehicle mechanism and further comprises: the unmanned aerial vehicle comprises a damping mechanism, a fixing mechanism and a video mechanism, wherein the top end of the unmanned aerial vehicle mechanism is fixedly connected with the bottom end of the fixing mechanism, the side surface of the fixing mechanism is fixedly connected with the side surface of the damping mechanism, and the side surface of the video mechanism is movably connected with the side surface of the damping mechanism; when vibration occurs in the flying process, the pressure springs on two sides shrink or stretch and absorb impact force through the second damper, the video mechanism is buffered, the lower limit spring and the upper limit spring shrink or stretch, and the fourth damper and the third damper absorb the impact force, so that the connecting block moves up and down along the inner wall of the side face of the clamping plate, the influence of vibration on the video mechanism is reduced, the vibration of the video mechanism is reduced, the shooting picture of the video main body is ensured to be clear, and the accuracy of mapping is improved.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles for surveying and mapping, in particular to a clamping and damping structure of video equipment for an unmanned aerial vehicle for surveying and mapping.
Background
The mapping is to measure, collect and draw the shape, size, spatial position and attribute of natural geographic elements or surface artificial facilities into a graph, in the mapping process, the field is required to be visualized by using a visual device for detail understanding, the photographed picture is transmitted to a computer terminal for processing, the photographing range required in the mapping process is large, the accuracy of photographing information is ensured for reducing the workload of staff, and the photographing is usually performed by installing the visual device for a mapping unmanned aerial vehicle.
The prior art is not enough: the existing surveying and mapping unmanned aerial vehicle is rigidly connected through bolts in the installation process of video equipment, and has no corresponding damping structure, and the unmanned aerial vehicle vibrates in the flight process, so that the video equipment vibrates, and a shot picture is unclear, and the surveying and mapping accuracy is affected; the bolt fastening is fixed through screw thread frictional force, wastes time and energy during the operation, reduces work efficiency.
Disclosure of Invention
In order to overcome the defects in the prior art, the utility model provides a clamping and damping structure for a video device of a surveying and mapping unmanned aerial vehicle, which aims to solve the problems in the prior art.
In order to achieve the above purpose, the present utility model provides the following technical solutions: survey and drawing visual equipment centre gripping shock-absorbing structure for unmanned aerial vehicle, including unmanned aerial vehicle mechanism, still include: the device comprises a damping mechanism, a fixing mechanism and a video mechanism, wherein the top end of the unmanned aerial vehicle mechanism is fixedly connected with the bottom end of the fixing mechanism, the side surface of the fixing mechanism is fixedly connected with the side surface of the damping mechanism, the side surface of the video mechanism is movably connected with the side surface of the damping mechanism, the unmanned aerial vehicle mechanism comprises an unmanned aerial vehicle main body, the bottom end of the unmanned aerial vehicle main body is fixedly connected with a supporting rod, the fixing mechanism comprises a top plate, the top end of the top plate is fixedly connected with the bottom end of the unmanned aerial vehicle main body, the bottom end of the top plate is movably connected with a mounting plate, the damping mechanism comprises a clamping plate, the side surface of the clamping plate is fixedly connected with a pressure spring, the side surface of the pressure spring is fixedly connected with a second damper, the side surface of the second damper is fixedly connected with the side surface of the mounting plate, and the video mechanism comprises a video main body, the top end of the video main body is fixedly connected with a connecting block, and the side surface of the connecting block is movably connected with the side surface inner wall of the clamping plate.
Further, the top fixedly connected with of connecting block, the limit plate is gone up to the side fixedly connected with of connecting block, limit spring is gone down to the bottom fixedly connected with of splint, limit spring's bottom fixedly connected with lower backup pad down, the bottom of lower backup pad and the top swing joint of last limit plate, the bottom fixedly connected with fourth attenuator of splint, the bottom of fourth attenuator and the top fixed connection of lower backup pad, limit spring is gone up to the top fixedly connected with of splint, limit spring's top fixedly connected with goes up the backup pad, limit spring's position fixedly connected with third attenuator is gone up on the top of splint, the top of third attenuator and the bottom fixed connection of last backup pad, the top and the bottom swing joint of last backup pad.
Further, a second arc angle is formed in the side face of the connecting block, and a first arc angle is formed in the position, corresponding to the second arc angle, of the side face of the clamping plate.
Further, the side inner wall of the clamping plate is movably connected with a roller through a pin, and the roller is in transmission connection with the side face of the connecting block.
Further, a first inclined plane is formed on the side surface of the upper supporting plate, a third inclined plane is formed at the position, corresponding to the first inclined plane, of the side surface of the upper limiting plate, a fourth inclined plane is formed on the side surface of the upper limiting plate, and a second inclined plane is formed at the position, corresponding to the second arc angle, of the side surface of the lower supporting plate.
Further, the bottom of roof has been seted up logical groove, the side of mounting panel and the side swing joint of logical groove, the side inner wall fixedly connected with motor of roof, the output shaft fixedly connected with two-way threaded rod of motor, the side and the top threaded connection of mounting panel of two-way threaded rod.
Further, the bottom fixedly connected with installation pole of bracing piece, the top inner wall fixedly connected with damping spring of installation pole, damping spring's bottom fixedly connected with base, the top inner wall fixedly connected with first attenuator of installation pole, the bottom of first attenuator and the bottom inner wall fixed connection of base.
The utility model has the technical effects and advantages that:
1. when vibration occurs in the flying process, the pressure springs on two sides shrink or stretch and absorb impact force through the second damper, the video mechanism is buffered, the lower limit spring and the upper limit spring shrink or stretch, and the fourth damper and the third damper absorb the impact force, so that the connecting block moves up and down along the inner wall of the side face of the clamping plate, the influence of vibration on the video mechanism is reduced, the vibration of the video mechanism is reduced, the shooting picture of the video main body is ensured to be clear, and the accuracy of mapping is improved.
2. According to the utility model, the motor drives the bidirectional threaded rod to rotate, the mounting plate is driven to move along the side surface of the through groove through threads, so that the clamping plates on two sides are close to the connecting block, the second circular arc angle is contacted with the first circular arc angle, the connecting block is enabled to rapidly move into the center positions of the two clamping plates, the upper limiting spring pushes the upper supporting plate to upwards enable the top end of the upper supporting plate to be clung to the bottom end of the upper limiting plate, the lower limiting spring pushes the lower supporting plate to downwards enable the bottom end of the lower supporting plate to be clung to the top end of the upper limiting plate, the video mechanism is limited, meanwhile, the inner wall of the side surface of the clamping plate is clung to the side surface of the connecting block to fix the video mechanism, the video mechanism is conveniently installed and fixed, and the improvement of the working efficiency is facilitated.
3. According to the utility model, the second arc angle is contacted with the first arc angle when the clamping plates on two sides are close to the connecting block, so that the connecting block is quickly moved into the center positions of the two clamping plates, the first inclined surface on the side surface of the upper supporting plate is contacted with the third inclined surface on the side surface, the upper supporting plate is smoothly moved to the bottom end, the fourth inclined surface on the side surface of the upper limiting plate is contacted with the second inclined surface on the side surface of the lower supporting plate, and the lower supporting plate is smoothly moved to the top end of the upper limiting plate, thereby being beneficial to quickly positioning and conveniently fixing the position of the video mechanism.
Drawings
FIG. 1 is a schematic diagram of the overall structure of the present utility model;
FIG. 2 is a schematic view of a fixing mechanism according to the present utility model;
FIG. 3 is a schematic view of a vision mechanism according to the present utility model;
FIG. 4 is a schematic view of a shock absorbing mechanism according to the present utility model;
FIG. 5 is a schematic cross-sectional view of the fixing mechanism of the present utility model;
fig. 6 is a schematic cross-sectional structure of the mounting bar of the present utility model.
The reference numerals are: 1. an unmanned aerial vehicle mechanism; 101. an unmanned aerial vehicle main body; 102. a support rod; 103. a mounting rod; 104. a base; 105. a damping spring; 106. a first damper; 2. a damping mechanism; 201. a clamping plate; 202. a pressure spring; 203. a first inclined surface; 204. an upper support plate; 205. a second inclined surface; 206. a second damper; 207. a first arc angle; 208. a roller; 209. an upper limit spring; 210. a third damper; 211. a lower support plate; 212. a lower limit spring; 213. a fourth damper; 3. a fixing mechanism; 301. a top plate; 302. a mounting plate; 303. a through groove; 304. a two-way threaded rod; 305. a motor; 4. a video mechanism; 401. a video camera body; 402. a connecting block; 403. an upper limit plate; 404. a third inclined surface; 405. an upper limit plate; 406. a fourth inclined surface; 407. and a second arc angle.
Detailed Description
The embodiments of the present utility model will be clearly and completely described below with reference to the drawings in the present utility model, and the configurations of the structures described in the following embodiments are merely examples, and the clamping and damping structure for a video device for a surveying and mapping unmanned aerial vehicle according to the present utility model is not limited to the structures described in the following embodiments, and all other embodiments obtained by a person having ordinary skill in the art without making any creative effort are within the scope of the present utility model.
Referring to fig. 1 to 6, the present utility model provides a clamping and damping structure for a video device of a surveying and mapping unmanned aerial vehicle, which comprises an unmanned aerial vehicle mechanism 1 and further comprises: damping mechanism 2, fixed establishment 3 and visual mechanism 4, the top of unmanned aerial vehicle mechanism 1 and the bottom fixed connection of fixed establishment 3, the side of fixed establishment 3 and the side fixed connection of damping mechanism 2, unmanned aerial vehicle mechanism 1 includes unmanned aerial vehicle main part 101, the bottom fixedly connected with bracing piece 102 of unmanned aerial vehicle main part 101, fixed establishment 3 includes roof 301, the top of roof 301 and the bottom fixed connection of unmanned aerial vehicle main part 101, the bottom swing joint of roof 301 has mounting panel 302, damping mechanism 2 includes splint 201, the side fixedly connected with pressure spring 202 of splint 201, the side of pressure spring 202 and the side fixed connection of mounting panel 302, the side of splint 201 corresponds the side fixed connection of pressure spring 202 has second attenuator 206, the side of second attenuator 206 and the side fixed connection of mounting panel 302, visual mechanism 4 includes visual machine main part 401, the top fixedly connected with connecting block 402, the side of connecting block 402 and the side inner wall swing joint of splint 201, place between two splint 201, the side fixedly connected with pressure spring 202 is used to the side of starting mechanism 3 makes the mounting panel 201 to make the side of clamping mechanism carry out the impact mechanism in the time of the compression mechanism 4 when the compression mechanism is used to the side of two sides of damping mechanism 4, the shock absorbing mechanism 4 is guaranteed to the shock absorbing mechanism, the shock 4 in the course is realized.
Wherein, the top end of the connecting block 402 is fixedly connected with 403, the side surface of the connecting block 402 is fixedly connected with an upper limit plate 405, the bottom end of the clamping plate 201 is fixedly connected with a lower limit spring 212, the bottom end of the lower limit spring 212 is fixedly connected with a lower support plate 211, the bottom end of the lower support plate 211 is movably connected with the top end of the upper limit plate 405, the bottom end of the clamping plate 201 is fixedly connected with a fourth damper 213, the bottom end of the fourth damper 213 is fixedly connected with the top end of the lower support plate 211, the top end of the clamping plate 201 is fixedly connected with an upper limit spring 209, the top end of the upper limit spring 209 is fixedly connected with an upper support plate 204, the top end of the clamping plate 201 is fixedly connected with a third damper 210 corresponding to the position of the upper limit spring 209, the top end of the third damper 210 is fixedly connected with the bottom end of the upper support plate 204, when the top end of the upper supporting plate 204 is movably connected with the bottom end of the upper supporting plate 403, the clamping plate 201 is clamped on two sides of the connecting block 402 to fix the video mechanism 4, the upper limiting spring 209 pushes the upper supporting plate 204 upwards to enable the top end of the upper supporting plate 204 to be tightly attached to the bottom end of the upper supporting plate 403, the lower limiting spring 212 pushes the lower supporting plate 211 downwards to enable the bottom end of the lower supporting plate 211 to be tightly attached to the top end of the upper limiting plate 405, the video mechanism 4 is limited, when the unmanned aerial vehicle mechanism 1 operates to vibrate, the lower limiting spring 212 and the upper limiting spring 209 shrink or stretch, and impact force is absorbed through the fourth damper 213 and the third damper 210, so that the connecting block 402 moves up and down along the side inner wall of the clamping plate 201, and the influence of vibration on the video mechanism 4 is reduced.
Wherein, the side of the connecting block 402 is provided with a second arc angle 407, the side of the clamping plate 201 is provided with a first arc angle 207 corresponding to the position of the second arc angle 407, and when two clamping plates 201 approach the connecting block 402, the second arc angle 407 contacts with the first arc angle 207, so that the connecting block 402 moves into the center positions of the two clamping plates 201 rapidly.
Wherein, the side inner wall of splint 201 has gyro wheel 208 through round pin swing joint, and gyro wheel 208 and the side transmission of connecting block 402 are connected, and when connecting block 402 moved along splint 201's side inner wall up and down, gyro wheel 208's side contacted with connecting block 402's side, made gyro wheel 208 roll along connecting block 402's side, reduced the frictional force between pressure spring 202 and the connecting block 402.
Wherein, the side surface of the upper support plate 204 is provided with a first inclined surface 203, the side surface of 403 is provided with a third inclined surface 404 corresponding to the position of the first inclined surface 203, the side surface of the upper limit plate 405 is provided with a fourth inclined surface 406, the side surface of the lower support plate 211 is provided with a second inclined surface 205 corresponding to the position of the second arc angle 407, when the clamping plates 201 on two sides approach the connecting block 402, the first inclined surface 203 on the side surface of the upper support plate 204 contacts with the third inclined surface 404 on the side surface of 403, so that the upper support plate 204 smoothly moves to the bottom end of 403, and the fourth inclined surface 406 on the side surface of the upper limit plate 405 contacts with the second inclined surface 205 on the side surface of the lower support plate 211, so that the lower support plate 211 smoothly moves to the top end of the upper limit plate 405.
Wherein, logical groove 303 has been seted up to the bottom of roof 301, the side of mounting panel 302 and logical side swing joint of groove 303, the side inner wall fixedly connected with motor 305 of roof 301, the output shaft fixedly connected with two-way threaded rod 304 of motor 305, the side of two-way threaded rod 304 and the top threaded connection of mounting panel 302, motor 305 drives two-way threaded rod 304 rotation, drive mounting panel 302 through the screw thread and remove along the side of logical groove 303 and make damper 2 press from both sides tight visual mechanism 4 and fix.
Wherein, the bottom fixedly connected with installation pole 103 of bracing piece 102, the top inner wall fixedly connected with damping spring 105 of installation pole 103, damping spring 105's bottom fixedly connected with base 104, the first attenuator 106 of top inner wall fixedly connected with of installation pole 103, the bottom of first attenuator 106 and the bottom inner wall fixed connection of base 104, unmanned aerial vehicle mechanism 1 is at descending process base 104 and ground contact, make damping spring 105 shrink and absorb the impact force through first attenuator 106, carry out shock attenuation buffering to unmanned aerial vehicle mechanism 1, the impact force of shock attenuation impact force is to the influence of equipment.
The working principle of the utility model is as follows: when the visual mechanism 4 is installed, the connecting block 402 is placed between the clamping plates 201 at two sides, the starting motor 305 drives the bi-directional threaded rod 304 to rotate, the mounting plate 302 is driven by threads to move along the side surface of the through groove 303, the clamping plates 201 at two sides are close to the connecting block 402, the second circular arc angle 407 is contacted with the first circular arc angle 207, the connecting block 402 is quickly moved into the center positions of the two clamping plates 201, the first inclined surface 203 at the side surface of the upper supporting plate 204 is contacted with the third inclined surface 404 at the side surface of the 403, the upper supporting plate 204 is smoothly moved to the bottom end of the 403, the fourth inclined surface 406 at the side surface of the upper limiting plate 405 is contacted with the second inclined surface 205 at the side surface of the lower supporting plate 211, the lower supporting plate 211 is smoothly moved to the top end of the upper limiting plate 405, the upper limiting spring 209 pushes the upper supporting plate 204 upwards to enable the top end of the upper supporting plate 204 to be clung to the bottom end of the lower supporting plate 211 to be clung to the top end of the upper limiting plate 405, the video mechanism 4 is limited, meanwhile, the inner wall of the side surface of the clamping plate 201 is tightly attached to the side surface of the connecting block 402 to fix the video mechanism 4, the unmanned aerial vehicle mechanism 1 runs and flies to the air, the video main body 401 shoots the ground, when vibration occurs in the flying process, the pressure springs 202 on two sides shrink or stretch and absorb the impact force through the second damper 206, the video mechanism 4 is buffered, meanwhile, the lower limit spring 212 and the upper limit spring 209 shrink or stretch, and absorb the impact force through the fourth damper 213 and the third damper 210, the connecting block 402 moves up and down along the inner wall of the side surface of the clamping plate 201, the influence of the vibration on the video mechanism 4 is reduced, the vibration of the video mechanism 4 is reduced, the shooting picture of the video main body 401 is ensured to be clear, the unmanned aerial vehicle mechanism 1 contacts the ground in the landing process base 104, the damper spring 105 is contracted to absorb the impact force by the first damper 106, thereby damping and buffering the unmanned aerial vehicle mechanism 1.
The foregoing description of the preferred embodiments of the utility model is not intended to limit the utility model to the precise form disclosed, and any such modifications, equivalents, and alternatives falling within the spirit and principles of the utility model are intended to be included within the scope of the utility model.
Claims (7)
1. The utility model provides a survey and drawing visual equipment centre gripping shock-absorbing structure for unmanned aerial vehicle, includes unmanned aerial vehicle mechanism (1), its characterized in that still includes: damping mechanism (2), fixed establishment (3) and visual mechanism (4), the top of unmanned aerial vehicle mechanism (1) and the bottom fixed connection of fixed establishment (3), the side of fixed establishment (3) and the side fixed connection of damping mechanism (2), the side of visual mechanism (4) and the side swing joint of damping mechanism (2), unmanned aerial vehicle mechanism (1) includes unmanned aerial vehicle main part (101), the bottom fixed connection of unmanned aerial vehicle main part (101) has bracing piece (102), fixed establishment (3) include roof (301), the top of roof (301) and the bottom fixed connection of unmanned aerial vehicle main part (101), the bottom fixed connection of roof (301) has mounting panel (302), damping mechanism (2) include splint (201), the side of splint (201) is fixedly connected with pressure spring (202), the side of pressure spring (202) and the side fixed connection of mounting panel (302), the side of splint (201) corresponds the position fixed connection of pressure spring (202) has second ware (206), the side of second ware (206) and the fixed connection of visual side (302) has damping mechanism (401), the top end of the video camera main body (401) is fixedly connected with a connecting block (402), and the side surface of the connecting block (402) is movably connected with the side surface inner wall of the clamping plate (201).
2. The video device clamping and damping structure for a surveying and mapping unmanned aerial vehicle according to claim 1, wherein: the top fixedly connected with (403) of connecting block (402), limit plate (405) are gone up to the side fixedly connected with of connecting block (402), limit spring (212) are gone up to the bottom fixedly connected with of splint (201), limit spring (212) are gone up limit spring's bottom fixedly connected with bottom backup pad (211) down, the bottom and the top swing joint of last limit plate (405) of bottom backup pad (211), the bottom fixedly connected with fourth attenuator (213) of splint (201), the bottom and the top fixedly connected with of lower backup pad (211) of fourth attenuator (213), limit spring (209) are gone up to the top fixedly connected with of splint (201), limit spring's (209) are gone up limit spring's top fixedly connected with and are gone up backup pad (204), limit spring's (209) are gone up in the top of splint (201) position fixedly connected with third attenuator (210), the top and the bottom swing joint of last backup pad (204) of third attenuator (210).
3. The video device clamping and damping structure for a surveying and mapping unmanned aerial vehicle according to claim 2, wherein: the side of connecting block (402) has seted up second circular arc angle (407), the side of splint (201) has seted up first circular arc angle (207) corresponding to the position of second circular arc angle (407).
4. The video device clamping and damping structure for a surveying and mapping unmanned aerial vehicle according to claim 2, wherein: the side inner wall of the clamping plate (201) is movably connected with a roller (208) through a pin, and the roller (208) is in transmission connection with the side face of the connecting block (402).
5. The video device clamping and damping structure for a surveying and mapping unmanned aerial vehicle according to claim 2, wherein: the side of last backup pad (204) has seted up first inclined plane (203), third inclined plane (404) are seted up to the position that the side of (403) corresponds first inclined plane (203), fourth inclined plane (406) are seted up to the side of going up limiting plate (405), second inclined plane (205) are seted up to the position that the side of lower backup pad (211) corresponds second circular arc angle (407).
6. The video device clamping and damping structure for a surveying and mapping unmanned aerial vehicle according to claim 1, wherein: the bottom of roof (301) has been seted up logical groove (303), the side of mounting panel (302) and the side swing joint of logical groove (303), the side inner wall fixedly connected with motor (305) of roof (301), the output shaft fixedly connected with two-way threaded rod (304) of motor (305), the side and the top threaded connection of mounting panel (302) of two-way threaded rod (304).
7. The video device clamping and damping structure for a surveying and mapping unmanned aerial vehicle according to claim 1, wherein: the novel damping device comprises a supporting rod (102), wherein a mounting rod (103) is fixedly connected to the bottom end of the supporting rod (102), a damping spring (105) is fixedly connected to the inner wall of the top end of the mounting rod (103), a base (104) is fixedly connected to the bottom end of the damping spring (105), a first damper (106) is fixedly connected to the inner wall of the top end of the mounting rod (103), and the bottom end of the first damper (106) is fixedly connected with the inner wall of the bottom end of the base (104).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322077140.6U CN220298783U (en) | 2023-08-03 | 2023-08-03 | Video equipment clamping shock-absorbing structure for surveying and mapping unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322077140.6U CN220298783U (en) | 2023-08-03 | 2023-08-03 | Video equipment clamping shock-absorbing structure for surveying and mapping unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220298783U true CN220298783U (en) | 2024-01-05 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322077140.6U Active CN220298783U (en) | 2023-08-03 | 2023-08-03 | Video equipment clamping shock-absorbing structure for surveying and mapping unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220298783U (en) |
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2023
- 2023-08-03 CN CN202322077140.6U patent/CN220298783U/en active Active
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