CN218806634U - Geotechnical engineering reconnaissance is with high altitude measurement unmanned aerial vehicle - Google Patents
Geotechnical engineering reconnaissance is with high altitude measurement unmanned aerial vehicle Download PDFInfo
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- CN218806634U CN218806634U CN202222308595.XU CN202222308595U CN218806634U CN 218806634 U CN218806634 U CN 218806634U CN 202222308595 U CN202222308595 U CN 202222308595U CN 218806634 U CN218806634 U CN 218806634U
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- 238000005259 measurement Methods 0.000 title claims abstract description 10
- 238000013016 damping Methods 0.000 claims abstract description 17
- 238000011835 investigation Methods 0.000 claims abstract description 8
- 230000035939 shock Effects 0.000 abstract description 11
- 238000009434 installation Methods 0.000 description 3
- 238000006243 chemical reaction Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012544 monitoring process 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 discloses an unmanned aerial vehicle is measured with high altitude to geotechnical engineering reconnaissance, including the unmanned aerial vehicle body, the spacing box of the equal fixedly connected with in both sides of unmanned aerial vehicle body bottom, the bottom of unmanned aerial vehicle body is provided with super clear camera, the bottom fixedly connected with sleeve pipe of spacing box, the top fixedly connected with slide bar of cover intraductal chamber, the bottom fixedly connected with stopper of slide bar. The utility model discloses an unmanned aerial vehicle body, spacing box, super clear camera, the sleeve pipe, the slide bar, the stopper, the movable plate, the montant, the sliding plate, the bracing piece, a supporting plate, damping spring, the carousel, the protruding axle, the connecting rod, the connecting seat, the cooperation of riser and gag lever post is used, possess the shock attenuation protection and easy to assemble video recording equipment's advantage, can effectually solve present geotechnical engineering investigation high altitude measurement unmanned aerial vehicle, do not possess the function of shock attenuation protection, be not convenient for install video recording equipment simultaneously, consequently can't satisfy user demand's problem.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is an aerial surveying unmanned aerial vehicle is used in geotechnical engineering reconnaissance.
Background
The unmanned aerial vehicle is an unmanned aerial vehicle operated by using a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by a vehicle-mounted computer, and can be divided into military and civil aspects according to the application field, the unmanned aerial vehicle is divided into a reconnaissance plane and a target plane, the civil aspect is applied to the unmanned aerial vehicle and the industry, and the unmanned aerial vehicle is really just needed; at present, in the application in fields such as aerial photography, agriculture, plant protection, miniature autodyne, express delivery transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news report, electric power inspection, disaster relief, movie & TV shooting, romantic manufacturing and the like, the use of the unmanned aerial vehicle is greatly expanded, the existing high-altitude measurement unmanned aerial vehicle for geotechnical engineering investigation does not have the function of shock absorption and protection, and is inconvenient for installing video equipment, so that the use requirement cannot be met.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle is measured with high altitude to geotechnical engineering reconnaissance possesses shock attenuation protection and the advantage of easy to assemble videography equipment, has solved present unmanned aerial vehicle is measured with high altitude to geotechnical engineering reconnaissance, does not possess the function of shock attenuation protection, and the videography equipment is not convenient for install simultaneously, consequently can't satisfy user demand's problem.
In order to achieve the above purpose, the utility model provides a following technical scheme: the utility model provides an aerial surveying unmanned aerial vehicle for geotechnical engineering reconnaissance, includes the unmanned aerial vehicle body, the equal fixedly connected with in both sides of unmanned aerial vehicle body bottom is spacing box, the bottom of unmanned aerial vehicle body is provided with super clear camera, the bottom fixedly connected with sleeve pipe of spacing box, the top fixedly connected with slide bar of sleeve pipe inner chamber, the bottom fixedly connected with stopper of slide bar, the bottom sliding connection on slide bar surface has the movable plate, the equal fixedly connected with montant in both sides of movable plate bottom, the bottom fixedly connected with sliding plate of montant, the bottom fixedly connected with bracing piece of sliding plate, the bottom of bracing piece extends to sheathed tube outside and fixedly connected with backup pad, the surface cover of slide bar is equipped with damping spring, one side of spacing box inner chamber is provided with the carousel, the positive one side fixedly connected with protruding axle of carousel, the surface sliding connection of protruding axle has the connecting rod, the one end swing joint that protruding axle was kept away from to the connecting rod has the connecting seat, one side fixedly connected with riser that the connecting rod is kept away from the connecting rod, one side fixedly connected with gag lever far away from the connecting rod, the one end that the riser kept away from the riser extends to the inner chamber of super clear camera.
Preferably, the top of the supporting plate is fixedly connected with a damper, a bearing plate is fixedly connected between the bottoms of the opposite sides of the two sleeves, and the top of the damper is fixedly connected with the bottom of the bearing plate.
Preferably, the back fixedly connected with servo motor of carousel, servo motor's the back and the inner wall fixed connection of spacing box.
Preferably, both sides of the sliding plate are in sliding connection with the inner wall of the sleeve, and the top and the bottom of the vertical plate are in sliding connection with the inner wall of the limiting box.
Preferably, the top of the damping spring is fixedly connected with the inner wall of the sleeve, and the bottom of the damping spring is fixedly connected with the top of the moving plate.
Preferably, the equal fixedly connected with landing leg in both sides of unmanned aerial vehicle body bottom, the bottom fixedly connected with support of landing leg.
Compared with the prior art, the beneficial effects of the utility model are as follows:
1. the utility model discloses an unmanned aerial vehicle body, spacing box, super clear camera, the sleeve pipe, the slide bar, the stopper, the movable plate, the montant, the sliding plate, the bracing piece, a supporting plate, damping spring, the carousel, the protruding axle, the connecting rod, the connecting seat, the cooperation of riser and gag lever post is used, possess the advantage of shock attenuation protection and easy to assemble video recording equipment, can effectually solve present geotechnical engineering reconnaissance and use high altitude measurement unmanned aerial vehicle, do not possess the function of shock attenuation protection, be not convenient for install video recording equipment simultaneously, consequently, can't satisfy user demand's problem.
2. The utility model discloses a set up the attenuator, can further improve the shock attenuation effect of backup pad when using, through setting up servo motor, can be convenient for drive the carousel and rotate to in driving the protruding axle and rotating, through setting up landing leg and support, can improve the stability of unmanned aerial vehicle body when using.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a front view of the structure of the present invention;
fig. 3 is an enlarged view of a in fig. 1 according to the present invention.
In the figure: 1. an unmanned aerial vehicle body; 2. a limiting box; 3. an ultra-clear camera; 4. a sleeve; 5. a slide bar; 6. a limiting block; 7. moving the plate; 8. a vertical rod; 9. a sliding plate; 10. a support bar; 11. a support plate; 12. a damping spring; 13. a turntable; 14. a protruding shaft; 15. a connecting rod; 16. a connecting seat; 17. a vertical plate; 18. a limiting rod; 19. a damper.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts all belong to the protection scope of the present invention.
Referring to fig. 1-3, an aerial surveying unmanned aerial vehicle for geotechnical engineering investigation comprises an unmanned aerial vehicle body 1, wherein both sides of the bottom of the unmanned aerial vehicle body 1 are fixedly connected with limiting boxes 2, the bottom of the unmanned aerial vehicle body 1 is provided with an ultra-clear camera 3, the bottom of the limiting box 2 is fixedly connected with a sleeve 4, the top of the inner cavity of the sleeve 4 is fixedly connected with a slide bar 5, the bottom of the slide bar 5 is fixedly connected with a limiting block 6, the bottom of the surface of the slide bar 5 is slidably connected with a movable plate 7, both sides of the bottom of the movable plate 7 are fixedly connected with a vertical bar 8, the bottom of the vertical bar 8 is fixedly connected with a sliding plate 9, the bottom of the sliding plate 9 is fixedly connected with a support bar 10, the bottom of the support bar 10 extends to the outside of the sleeve 4 and is fixedly connected with a support plate 11, the surface of the slide bar 5 is sleeved with a damping spring 12, one side of the inner cavity of the limiting box 2 is provided with a turntable 13, one side of the front of the turntable 13 is fixedly connected with a convex shaft 14, the surface of the protruding shaft 14 is connected with a connecting rod 15 in a sliding manner, one end of the connecting rod 15, which is far away from the protruding shaft 14, is movably connected with a connecting seat 16, one side of the connecting seat 16, which is far away from the connecting rod 15, is fixedly connected with a vertical plate 17, one side of the vertical plate 17, which is far away from the connecting seat 16, is fixedly connected with a limiting rod 18, one end of the limiting rod 18, which is far away from the vertical plate 17, extends to an inner cavity of the ultra-clear camera 3, the top of the supporting plate 11 is fixedly connected with a damper 19, the damping effect of the supporting plate 11 in use can be further improved by arranging the damper 19, a bearing plate is fixedly connected between the bottoms of the opposite sides of the two sleeves 4, the top of the damper 19 is fixedly connected with the bottom of the bearing plate, the back of the rotary plate 13 is fixedly connected with a servo motor, by arranging the servo motor, the rotary plate 13 can be conveniently driven to rotate, so as to drive the protruding shaft 14 to rotate, the back of the servo motor is fixedly connected with the inner wall of the limiting box 2, the both sides of sliding plate 9 all with sleeve pipe 4's inner wall sliding connection, the top of riser 17 and the equal and spacing box 2's of bottom inner wall sliding connection, damping spring 12's top and sleeve pipe 4's inner wall fixed connection, damping spring 12's bottom and the top fixed connection of movable plate 7, the equal fixedly connected with landing leg in both sides of unmanned aerial vehicle body 1 bottom, the bottom fixedly connected with support of landing leg, through setting up landing leg and support, can improve the stability of unmanned aerial vehicle body 1 when using, through unmanned aerial vehicle body 1, spacing box 2, super clear camera 3, sleeve pipe 4, slide bar 5, stopper 6, movable plate 7, montant 8, sliding plate 9, bracing piece 10, backup pad 11, damping spring 12, carousel 13, protruding axle 14, connecting rod 15, connecting seat 16, riser 17 and stopper 18's cooperation is used, possess the geotechnical advantage of shock attenuation protection and easy to install video recording equipment, can effectually solve present reconnaissance and measure unmanned aerial vehicle with high altitude, do not possess the function of shock attenuation protection, be not convenient for installation video recording equipment simultaneously, consequently, can's problem that can's user demand can's unable satisfied.
During the use, unmanned aerial vehicle body 1 can produce reaction force when falling to the ground, reaction force drives backup pad 11 and removes, backup pad 11 drives bracing piece 10 and removes, bracing piece 10 drives sliding plate 9 and removes, sliding plate 9 drives montant 8 and removes, montant 8 drives movable plate 7 and removes, movable plate 7 extrudees damping spring 12, make damping spring 12 produce deformation, because damping spring 12 has elasticity, so can carry out the shock attenuation protection to unmanned aerial vehicle body 1, when needs installation super clear camera 3, start servo motor through operating external controller, servo motor drives carousel 13 and rotates, carousel 13 drives protruding axle 14 and rotates, protruding axle 14 drives connecting rod 15 and removes, connecting rod 15 drives connecting seat 16 and removes, connecting seat 16 drives riser 17 and removes, riser 17 drives gag lever post 18 and removes, gag lever post 18 carries out spacing fixed to super clear camera 3, with this purpose that reaches quick installation.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The utility model provides a geotechnical engineering reconnaissance is with high altitude measurement unmanned aerial vehicle, includes unmanned aerial vehicle body (1), its characterized in that: the unmanned aerial vehicle comprises an unmanned aerial vehicle body (1), limiting boxes (2) are fixedly connected to two sides of the bottom of the unmanned aerial vehicle body (1), a super-clear camera (3) is arranged at the bottom of the unmanned aerial vehicle body (1), sleeves (4) are fixedly connected to the bottom of the limiting boxes (2), slide rods (5) are fixedly connected to the tops of inner cavities of the sleeves (4), limiting blocks (6) are fixedly connected to the bottoms of the slide rods (5), movable plates (7) are slidably connected to the bottoms of the surfaces of the slide rods (5), vertical rods (8) are fixedly connected to two sides of the bottom of the movable plates (7), sliding plates (9) are fixedly connected to the bottoms of the vertical rods (8), supporting rods (10) are fixedly connected to the bottoms of the supporting rods (10), supporting plates (11) are fixedly connected to the bottoms of the surfaces of the slide rods (10), damping springs (12) are sleeved on the surfaces of the slide rods (5), a rotary table (13) is arranged on one side of the inner cavity of the limiting boxes (2), a convex shaft (14) is fixedly connected to one side of the front of the rotary table (13), a connecting rod (15) is slidably connected to a connecting rod (16), and a connecting rod (16) is connected to one side of the connecting seat (16) far away from the connecting seat (16), one side that connecting seat (16) were kept away from in riser (17) is fixedly connected with gag lever post (18), the one end that riser (17) were kept away from in gag lever post (18) extends to the inner chamber of super clear camera (3).
2. The high altitude measurement unmanned aerial vehicle for geotechnical engineering investigation of claim 1, characterized in that: the top fixedly connected with attenuator (19) of backup pad (11), fixedly connected with loading board between the bottom of the relative one side of two sleeve pipes (4), the top of attenuator (19) and the bottom fixed connection of loading board.
3. The high altitude measurement unmanned aerial vehicle for geotechnical engineering investigation of claim 1, characterized in that: the back fixedly connected with servo motor of carousel (13), servo motor's the back and the inner wall fixed connection of spacing box (2).
4. The high altitude measurement unmanned aerial vehicle for geotechnical engineering investigation of claim 1, characterized in that: the two sides of the sliding plate (9) are in sliding connection with the inner wall of the casing (4), and the top and the bottom of the vertical plate (17) are in sliding connection with the inner wall of the limiting box (2).
5. The high altitude measurement unmanned aerial vehicle for geotechnical engineering investigation of claim 1, characterized in that: the top of the damping spring (12) is fixedly connected with the inner wall of the sleeve (4), and the bottom of the damping spring (12) is fixedly connected with the top of the moving plate (7).
6. The high altitude measurement unmanned aerial vehicle for geotechnical engineering investigation of claim 1, characterized in that: the equal fixedly connected with landing leg in both sides of unmanned aerial vehicle body (1) bottom, the bottom fixedly connected with support of landing leg.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222308595.XU CN218806634U (en) | 2022-08-31 | 2022-08-31 | Geotechnical engineering reconnaissance is with high altitude measurement unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222308595.XU CN218806634U (en) | 2022-08-31 | 2022-08-31 | Geotechnical engineering reconnaissance is with high altitude measurement unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218806634U true CN218806634U (en) | 2023-04-07 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222308595.XU Active CN218806634U (en) | 2022-08-31 | 2022-08-31 | Geotechnical engineering reconnaissance is with high altitude measurement unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218806634U (en) |
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2022
- 2022-08-31 CN CN202222308595.XU patent/CN218806634U/en active Active
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20240913 Address after: 510000 302, No. 2, Longxing North 4th Street, Nancun, Taihe Town, Baiyun District, Guangzhou City, Guangdong Province (self declaration) Patentee after: Guangdong Jian'an Testing Co.,Ltd. Country or region after: China Address before: No. 38, Luyuan, Jianye District, Nanjing City, Jiangsu Province, 210000 Patentee before: Zhang Wendong Country or region before: China |