CN217294920U - Survey and drawing is with exploration unmanned aerial vehicle - Google Patents
Survey and drawing is with exploration unmanned aerial vehicle Download PDFInfo
- Publication number
- CN217294920U CN217294920U CN202220382509.7U CN202220382509U CN217294920U CN 217294920 U CN217294920 U CN 217294920U CN 202220382509 U CN202220382509 U CN 202220382509U CN 217294920 U CN217294920 U CN 217294920U
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- fixedly connected
- plate
- shock absorber
- spring
- inner cavity
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- 238000013016 damping Methods 0.000 claims abstract description 38
- 239000006096 absorbing agent Substances 0.000 claims abstract description 31
- 230000035939 shock Effects 0.000 claims abstract description 31
- 238000013507 mapping Methods 0.000 claims abstract description 15
- 230000007246 mechanism Effects 0.000 abstract description 5
- 230000001681 protective effect Effects 0.000 abstract description 3
- 230000000694 effects Effects 0.000 description 7
- 238000005516 engineering process Methods 0.000 description 4
- 230000002633 protecting effect Effects 0.000 description 3
- 230000003139 buffering effect Effects 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 230000006641 stabilisation Effects 0.000 description 2
- 238000011105 stabilization Methods 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008901 benefit 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
- 238000007726 management method 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
- 230000008569 process Effects 0.000 description 1
- 238000006467 substitution reaction 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
Abstract
The utility model discloses a survey and drawing is with exploration unmanned aerial vehicle, which comprises a bod, the outside fixedly connected with wing of organism, the first spring of outside fixedly connected with of wing, the outside fixedly connected with guard plate of first spring, the bottom fixedly connected with diaphragm of guard plate, there is a damping shock absorber in the front of diaphragm through connecting pin swing joint, one side swing joint of a damping shock absorber has the connecting plate, the four corners of connecting plate inner chamber is all pegged graft and is had the montant. The utility model discloses an organism, wing, first spring, guard plate, diaphragm, first damping bumper shock absorber, connecting plate, montant, fixed plate, second spring, second damping bumper shock absorber, casing, cylinder, support, camera, fixed pin, movable rod, movable block, apron and impact sensor's cooperation has solved current survey and drawing unmanned aerial vehicle and has been poor in protective effect when work and descending, leads to the problem of the easy damage of unmanned aerial vehicle and mapping mechanism.
Description
Technical Field
The utility model relates to a survey and drawing technical field specifically is an exploration unmanned aerial vehicle is used in survey and drawing.
Background
Surveying and mapping refer to measurement and mapping, a computer technology, a photoelectric technology, a network communication technology, space science and information science are taken as a basis, a global navigation satellite positioning system, remote sensing and a geographic information system are taken as a technical core, existing characteristic points and boundary lines on the ground are obtained to reflect the current situation of the ground through a measurement means, planning design and administrative management of engineering construction are provided, due to terrain factors and along with the progress of science and technology, aerial photography and mapping are carried out by an unmanned aerial vehicle, the existing surveying and mapping unmanned aerial vehicle is poor in protection effect during working and landing, so that the unmanned aerial vehicle and a surveying and mapping mechanism are easy to damage, and therefore the unmanned aerial vehicle for surveying and mapping is provided.
SUMMERY OF THE UTILITY MODEL
Not enough to prior art, the utility model provides a survey and drawing is with exploration unmanned aerial vehicle possesses the good advantage of protecting effect, and it is poor to have solved current survey and drawing unmanned aerial vehicle at work when descending protecting effect, leads to the problem of the easy damage of unmanned aerial vehicle and mapping mechanism.
Technical scheme
In order to achieve the above object, the utility model provides a following technical scheme: an exploration unmanned aerial vehicle for surveying and mapping comprises a machine body, wherein the outer side of the machine body is fixedly connected with a wing, the outer side of the wing is fixedly connected with a first spring, the outer side of the first spring is fixedly connected with a protection plate, the bottom of the protection plate is fixedly connected with a transverse plate, the front surface of the transverse plate is movably connected with a first damping shock absorber through a connecting pin, one side of the first damping shock absorber is movably connected with a connecting plate, vertical rods are all inserted in four corners of an inner cavity of the connecting plate, the top and the bottom of each vertical rod are fixedly connected with a fixing plate, one side of each fixing plate is fixedly connected with a second spring, one side of each second spring is fixedly connected with the connecting plate, the top of each connecting plate is fixedly connected with a second damping shock absorber, the top of each second damping shock absorber is fixedly connected with the machine body, and a shell is fixedly connected with the middle shaft at the bottom of the machine body, the utility model discloses a sensor, including casing, casing inner chamber, front side fixedly connected with cylinder, the back fixedly connected with support of cylinder, the top fixedly connected with camera of support, the right side fixedly connected with fixed pin of camera, the surperficial swing joint of fixed pin has the movable rod, the back swing joint of movable rod has the movable block, the back fixedly connected with apron of movable block, hinge and casing swing joint are passed through to the positive bottom of apron, the positive fixedly connected with impact sensor of casing.
Preferably, the bottom of the wing is provided with a sliding groove, an inner cavity of the sliding groove is connected with a sliding block in a sliding mode, and the bottom of the sliding block is fixedly connected with the transverse plate.
Preferably, the inner cavity of the connecting plate is provided with a through hole, and the inner cavity of the through hole is fixedly connected with a damping sleeve.
Preferably, the bottom of the inner cavity of the shell is provided with a movable groove, and the inner cavity of the movable groove is in sliding connection with the support.
Preferably, the number of the wings is four, and the four wings are uniformly distributed on the surface of the machine body.
Advantageous effects
Compared with the prior art, the utility model provides a survey and drawing is with exploration unmanned aerial vehicle possesses following beneficial effect:
1. the utility model discloses when guard plate and foreign object bump in the course of the work, the guard plate can drive first spring and take place the deformation, can drive the diaphragm simultaneously and remove, the diaphragm drives the connecting pin and removes, the connecting pin drives first damping bumper shock absorber and takes place the deformation, simultaneously first damping bumper shock absorber still can drive the connecting plate and remove, the connecting plate drives second damping bumper shock absorber and takes place the deformation, and when bumping, the impact sensor can monitor the signal, then the cylinder can drive the support and remove, the support drives the camera and removes, the camera drives the fixed pin and removes, the fixed pin drives the movable rod and removes, the movable rod drives the movable block and removes, the movable block drives the apron and rotates with the hinge as the centre of a circle, thereby protect the camera, when descending, the fixed plate of bottom can contact with ground, because of the effect of the impact force, the organism can drive the second damping bumper shock absorber and take place the deformation, simultaneously the second damping bumper shock absorber can drive the connecting plate and remove, and the connecting plate drives second spring and first damping bumper shock absorber and takes place deformation, and first damping bumper shock absorber drives the diaphragm and removes, and the diaphragm drives the guard plate and removes, and the guard plate drives first spring and takes place deformation to can play the effect of buffering, it is poor to have solved current survey and drawing unmanned aerial vehicle protective effect when work and descending, leads to the problem of the easy damage of unmanned aerial vehicle and mapping mechanism.
2. The utility model discloses a set up spout and slider, stabilized the work of diaphragm to make guard plate job stabilization, through setting up the damping cover, played damped effect, avoid continuously rocking, through setting up the movable groove, stabilized the work of support, thereby make camera job stabilization.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic view of the side view structure of the shell of the present invention in a sectional view;
fig. 3 is a schematic view of the local top view structure of the present invention.
In the figure: 1. a body; 2. an airfoil; 3. a first spring; 4. a protection plate; 5. a transverse plate; 6. a first damping shock absorber; 7. a connecting plate; 8. a vertical rod; 9. a fixing plate; 10. a second spring; 11. a second damping bumper; 12. a housing; 13. a cylinder; 14. a support; 15. a camera; 16. a fixing pin; 17. a movable rod; 18. a movable block; 19. a cover plate; 20. an impact sensor.
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 work belong to the protection scope of the present invention.
Referring to fig. 1-3, an exploration unmanned aerial vehicle for surveying and mapping comprises a machine body 1, wherein the outer side of the machine body 1 is fixedly connected with four wings 2, the four wings 2 are uniformly distributed on the surface of the machine body 1, the outer side of each wing 2 is fixedly connected with a first spring 3, the outer side of each first spring 3 is fixedly connected with a protection plate 4, the bottom of each protection plate 4 is fixedly connected with a transverse plate 5, the bottom of each wing 2 is provided with a chute, the inner cavity of each chute is slidably connected with a sliding block, the bottom of each sliding block is fixedly connected with the transverse plate 5, the work of the transverse plate 5 is stabilized by arranging the chutes and the sliding blocks, so that the protection plates 4 work stably, the front side of the transverse plate 5 is movably connected with a first damping shock absorber 6 through a connecting pin, one side of each first damping shock absorber 6 is movably connected with a connecting plate 7, the inner cavity of each connecting plate 7 is provided with a through hole, and the inner cavity of each through hole is fixedly connected with a damping sleeve, through the arrangement of the damping sleeve, a damping effect is achieved, continuous shaking is avoided, vertical rods 8 are inserted into four corners of an inner cavity of the connecting plate 7, fixing plates 9 are fixedly connected to the top and the bottom of each vertical rod 8, a second spring 10 is fixedly connected to one side of each fixing plate 9, one side of each second spring 10 is fixedly connected to the connecting plate 7, a second damping shock absorber 11 is fixedly connected to the top of each connecting plate 7, the top of each second damping shock absorber 11 is fixedly connected to the machine body 1, a shell 12 is fixedly connected to a middle shaft at the bottom of the machine body 1, a cylinder 13 is fixedly connected to the front side of the inner cavity of the shell 12, a support 14 is fixedly connected to the back of the cylinder 13, a movable groove is formed in the bottom of the inner cavity of the shell 12, the inner cavity of the movable groove is slidably connected to the support 14, the work of the support 14 is stabilized through the arrangement of the movable groove, so that the camera 15 works stably, the top of the support 14 is fixedly connected to the camera 15, the right side fixedly connected with fixed pin 16 of camera 15, the surperficial swing joint of fixed pin 16 has movable rod 17, and the back swing joint of movable rod 17 has movable block 18, and the back fixedly connected with apron 19 of movable block 18, hinge and casing 12 swing joint are passed through to the positive bottom of apron 19, and the positive fixedly connected with impact sensor 20 of casing 12.
The working principle is as follows: when the protection plate 4 collides with a foreign object in the working process, the protection plate 4 drives the first spring 3 to deform and simultaneously drives the transverse plate 5 to move, the transverse plate 5 drives the connecting pin to move, the connecting pin drives the first damping shock absorber 6 to deform, the first damping shock absorber 6 also drives the connecting plate 7 to move, the connecting plate 7 drives the second damping shock absorber 11 to deform, and when the collision occurs, the impact sensor 20 monitors a signal, the air cylinder 13 drives the bracket 14 to move, the bracket 14 drives the camera 15 to move, the camera 15 drives the fixed pin 16 to move, the fixed pin 16 drives the movable rod 17 to move, the movable rod 17 drives the movable block 18 to move, the movable block 18 drives the cover plate 19 to rotate by taking the hinge as the center of a circle, thereby protecting the camera 15, when the bottom fixing plate 9 contacts with the ground, due to the action of the impact force, organism 1 can drive second damping shock absorber 11 and take place deformation, second damping shock absorber 11 can drive connecting plate 7 and remove simultaneously, connecting plate 7 drives second spring 10 and first damping shock absorber 6 takes place deformation, first damping shock absorber 6 drives diaphragm 5 and removes, diaphragm 5 drives guard plate 4 and removes, guard plate 4 drives first spring 3 and takes place deformation, thereby can play the effect of buffering, it is poor to have solved current survey and drawing unmanned aerial vehicle protective effect when work and descending, lead to the problem of the easy damage of unmanned aerial vehicle and survey and drawing mechanism.
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 (5)
1. The utility model provides a survey and drawing is with exploration unmanned aerial vehicle, includes organism (1), its characterized in that: the aircraft is characterized in that the outer side of the engine body (1) is fixedly connected with an airfoil (2), the outer side of the airfoil (2) is fixedly connected with a first spring (3), the outer side of the first spring (3) is fixedly connected with a protection plate (4), the bottom of the protection plate (4) is fixedly connected with a transverse plate (5), the front of the transverse plate (5) is movably connected with a first damping shock absorber (6) through a connecting pin, one side of the first damping shock absorber (6) is movably connected with a connecting plate (7), four corners of an inner cavity of the connecting plate (7) are respectively spliced with a vertical rod (8), the top and the bottom of the vertical rod (8) are respectively and fixedly connected with a fixed plate (9), one side of the fixed plate (9) is fixedly connected with a second spring (10), one side of the second spring (10) is fixedly connected with the connecting plate (7), and the top of the connecting plate (7) is fixedly connected with a second damping shock absorber (11), the top of the second damping shock absorber (11) is fixedly connected with the machine body (1), a shell (12) is fixedly connected with the middle shaft at the bottom of the machine body (1), the front side of the inner cavity of the shell (12) is fixedly connected with an air cylinder (13), the back of the air cylinder (13) is fixedly connected with a bracket (14), the top of the bracket (14) is fixedly connected with a camera (15), the right side of the camera (15) is fixedly connected with a fixed pin (16), the surface of the fixed pin (16) is movably connected with a movable rod (17), the back of the movable rod (17) is movably connected with a movable block (18), the back of the movable block (18) is fixedly connected with a cover plate (19), the bottom of the front of the cover plate (19) is movably connected with the shell (12) through a hinge, and the front surface of the shell (12) is fixedly connected with an impact sensor (20).
2. The surveying drone for surveying and mapping of claim 1, characterized in that: the bottom of the wing (2) is provided with a sliding groove, the inner cavity of the sliding groove is connected with a sliding block in a sliding mode, and the bottom of the sliding block is fixedly connected with the transverse plate (5).
3. The surveying drone for surveying and mapping of claim 1, characterized in that: the inner cavity of the connecting plate (7) is provided with a through hole, and the inner cavity of the through hole is fixedly connected with a damping sleeve.
4. The surveying drone for surveying and mapping of claim 1, characterized in that: the bottom of the inner cavity of the shell (12) is provided with a movable groove, and the inner cavity of the movable groove is connected with the support (14) in a sliding manner.
5. The surveying drone for surveying and mapping of claim 1, characterized in that: the number of the wings (2) is four, and the four wings (2) are uniformly distributed on the surface of the machine body (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220382509.7U CN217294920U (en) | 2022-02-24 | 2022-02-24 | Survey and drawing is with exploration unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220382509.7U CN217294920U (en) | 2022-02-24 | 2022-02-24 | Survey and drawing is with exploration unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217294920U true CN217294920U (en) | 2022-08-26 |
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ID=82928289
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202220382509.7U Expired - Fee Related CN217294920U (en) | 2022-02-24 | 2022-02-24 | Survey and drawing is with exploration unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217294920U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117184471A (en) * | 2023-11-07 | 2023-12-08 | 山东中宇航空科技发展有限公司 | Unmanned aerial vehicle survey and drawing measuring device |
-
2022
- 2022-02-24 CN CN202220382509.7U patent/CN217294920U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117184471A (en) * | 2023-11-07 | 2023-12-08 | 山东中宇航空科技发展有限公司 | Unmanned aerial vehicle survey and drawing measuring device |
| CN117184471B (en) * | 2023-11-07 | 2024-02-06 | 山东中宇航空科技发展有限公司 | Unmanned aerial vehicle survey and drawing measuring device |
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20220826 |
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| CF01 | Termination of patent right due to non-payment of annual fee |