CN213323728U - Survey and drawing unmanned aerial vehicle measuring device installation mechanism - Google Patents
Survey and drawing unmanned aerial vehicle measuring device installation mechanism Download PDFInfo
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- CN213323728U CN213323728U CN202022052699.XU CN202022052699U CN213323728U CN 213323728 U CN213323728 U CN 213323728U CN 202022052699 U CN202022052699 U CN 202022052699U CN 213323728 U CN213323728 U CN 213323728U
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Abstract
The utility model discloses a survey and drawing unmanned aerial vehicle measuring device installation mechanism relates to survey and drawing unmanned aerial vehicle measuring device technical field, and is still stable inadequately for solving current survey and drawing unmanned aerial vehicle measuring device's installation performance, the problem that the stability performance of the installation of part and descending is not perfect enough. The utility model discloses a damping stabilizing frame, including engine mounting bracket, measuring equipment mounting bracket, wing mounting bracket, fixed block, side installation fixed block, shock attenuation stabilizing frame, engine mounting bracket, measuring equipment mounting bracket, wing mounting bracket, fixed block, support mount, shock attenuation stabilizing frame's internally mounted has the fixed stay horizontal pole.
Description
Technical Field
The utility model relates to a survey and drawing unmanned aerial vehicle measuring device technical field specifically is a survey and drawing unmanned aerial vehicle measuring device installation mechanism.
Background
The aerial survey of the unmanned aerial vehicle is a powerful supplement of the traditional aerial photogrammetry means, has the characteristics of flexibility, high efficiency, rapidness, fineness, accuracy, low operation cost, wide application range, short production period and the like, the method has obvious advantages in the aspect of fast obtaining of high-resolution images in small areas and areas with difficult flight, along with the development of unmanned aerial vehicles and digital camera technologies, the digital aerial photography technology based on an unmanned aerial vehicle platform has shown unique advantages, the combination of the unmanned aerial vehicles and aerial photogrammetry enables the 'unmanned aerial vehicle digital low-altitude remote sensing' to become a brand-new development direction in the field of aerial remote sensing, the aerial photography of the unmanned aerial vehicles can be widely applied to the aspects of national major engineering construction, disaster emergency and treatment, territorial supervision, resource development, new rural areas, small town construction and the like, and the method has wide prospects in the aspects of basic surveying and mapping, land resource investigation and monitoring, dynamic monitoring of land utilization, digital city construction, acquisition of emergency disaster relief surveying and mapping data and.
However, the installation and use performance of the existing surveying and mapping unmanned aerial vehicle measuring device is not stable enough, and the installation and landing stability performance of components is not perfect enough; therefore, the existing requirements are not met, and the installation mechanism of the surveying and mapping unmanned aerial vehicle measuring device is provided for the existing requirements.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a survey and drawing unmanned aerial vehicle measuring device installation mechanism to the installation performance of the current survey and drawing unmanned aerial vehicle measuring device who provides in solving above-mentioned background is still stable inadequately, the problem that the stability performance of the installation of part and descending is not perfect enough.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a survey and drawing unmanned aerial vehicle measuring device installation mechanism, is including installation main fixed block, the engine mounting bracket is installed to the below of installation main fixed block, the measuring equipment mounting bracket is installed to the below of engine mounting bracket, the wing mounting bracket is all installed to the both sides of installation main fixed block, the connection fixed block is installed to the one end of installation main fixed block, the wing installation piece is installed in the outside of connecting the fixed block, side installation fixed block is all installed to the outside both sides of engine mounting bracket, the support mount is installed in the outside of side installation fixed block, the shock attenuation steady rest is installed in the outside of support mount below.
Preferably, the main mounting block, the measuring equipment mounting frame and the engine mounting frame are connected through bolts, and the wing mounting frame is fixedly connected with the main mounting block.
Preferably, the anti-collision fixing gasket is arranged outside the wing mounting frame and is connected with the wing mounting frame in a sticking mode.
Preferably, the side edge mounting fixing block is fixedly connected with the engine mounting frame and the supporting fixing frame, and a rotation limiting groove is formed in the lower end of the supporting fixing frame.
Preferably, the internally mounted of shock attenuation stabilizer has the fixed stay horizontal pole, and the fixed stay horizontal pole rotates through the damping pivot with supporting the mount and be connected, the fixed cushion of shock attenuation is all installed to the both sides of fixed stay horizontal pole, the externally mounted of the fixed cushion of shock attenuation has wear-resisting boss, and wear-resisting boss and the fixed cushion fixed connection of shock attenuation.
Preferably, the anti-collision sponge cushion is installed on the inner side of the engine installation frame, a central support frame is installed in the middle of the inside of the engine installation frame, and side fixing plates are arranged on the outer side of the central support frame.
Preferably, the side fixed plate is provided with a plurality of, and a plurality of side fixed plate distributes in proper order, the intermediate position department of central bracing frame is provided with the fixed orifices, all be provided with the installation fixed orifices on central bracing frame and the side fixed plate.
Compared with the prior art, the beneficial effects of the utility model are that:
1. the utility model discloses an install installation main fixed block, engine mounting bracket and measuring equipment mounting bracket, can make the installation stability of part obtain better guarantee, through installing side installation fixed block and shock attenuation steady rest, can be better the support performance of guarantee survey and drawing unmanned aerial vehicle measuring device, stability when descending has also obtained certain guarantee, solved the installation performance of current survey and drawing unmanned aerial vehicle measuring device and still not stable enough, the problem that the stability performance of the installation of part and descending is not perfect enough;
2. the utility model discloses an internally mounted at engine mounting bracket has crashproof foam-rubber cushion, center support frame and side fixed plate, the stability ability of guarantee part installation that can be better, and the support performance is more perfect, and the performance of later stage survey and drawing also can obtain better guarantee.
Drawings
Fig. 1 is a front view of the mounting mechanism of a surveying and mapping unmanned aerial vehicle measuring device of the present invention;
FIG. 2 is a schematic structural view of the side mounting fixing block and the damping stabilizing frame of the present invention;
fig. 3 is a schematic structural diagram of the engine mounting bracket of the present invention.
In the figure: 1. installing a main fixing block; 2. an engine mount; 3. a measuring equipment mounting frame; 4. a wing mount; 5. an anti-collision fixing washer; 6. connecting a fixed block; 7. a wing mounting block; 8. a fixed block is arranged on the side edge; 9. supporting the fixed frame; 10. a damping stabilizing frame; 11. fixing the support cross bar; 12. damping and fixing the cushion block; 13. a wear-resistant reinforcing block; 14. rotating the limiting groove; 15. a damping rotating shaft; 16. an anti-collision sponge cushion; 17. a central support frame; 18. a fixing hole; 19. side fixing plates; 20. and installing a fixing hole.
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.
Referring to fig. 1-3, the present invention provides an embodiment: the utility model provides a survey and drawing unmanned aerial vehicle measuring device installation mechanism, including installation main fixed block 1, engine mounting bracket 2 is installed to the below of installation main fixed block 1, measuring equipment mounting bracket 3 is installed to the below of engine mounting bracket 2, wing mounting bracket 4 is all installed to the both sides of installation main fixed block 1, the connection fixed block 6 is installed to the one end of installation main fixed block 1, wing installation piece 7 is installed in the outside of connection fixed block 6, side installation fixed block 8 is all installed to the outside both sides of engine mounting bracket 2, support mount 9 is installed in the outside of side installation fixed block 8, shock attenuation steady rest 10 is installed in the outside of support mount 9 below, the stability ability of guarantee part installation that can be better, moreover, the steam.
Further, the main mounting block 1 and the measuring equipment mounting frame 3 are connected with the engine mounting frame 2 through bolts, the wing mounting frame 4 is fixedly connected with the main mounting block 1, the connection performance is more stable and perfect, and the practicability is higher.
Further, the outside of wing mounting bracket 4 is equipped with crashproof fixed washer 5, and crashproof fixed washer 5 pastes with wing mounting bracket 4 and is connected, and the stability performance of guarantee connection that can be better can not take place to matter along with the increase of live time and change.
Further, side installation fixed block 8 and engine mounting bracket 2 and the equal fixed connection of support mount 9, the lower extreme of supporting mount 9 is provided with rotates spacing groove 14, and guarantee that can be better rotates spacing performance.
Further, the internally mounted of shock attenuation stabilizer 10 has fixed stay horizontal pole 11, and fixed stay horizontal pole 11 and support mount 9 rotate through damping pivot 15 and connect, and shock attenuation fixed cushion 12 is all installed to the both sides of fixed stay horizontal pole 11, and the externally mounted of shock attenuation fixed cushion 12 has wear-resisting boss 13, and wear-resisting boss 13 and shock attenuation fixed cushion 12 fixed connection, connects more convenient trouble-saving, and the practicality is higher.
Further, crashproof foam-rubber cushion 16 is installed to the inboard of engine mounting bracket 2, and central bracing frame 17 is installed to the inside intermediate position department of engine mounting bracket 2, and the outside of central bracing frame 17 is provided with side fixed plate 19, guarantee structural performance that can be better, and performance and practicality have obtained better promotion.
Further, side fixed plate 19 is provided with a plurality of, and a plurality of side fixed plate 19 distributes in proper order, and central support frame 17's intermediate position department is provided with fixed orifices 18, all is provided with installation fixed orifices 20 on central support frame 17 and the side fixed plate 19, and the installation fixity can be more stable perfect, and the practicality is higher.
The working principle is as follows: during the use, install the part as required in the inside and the upper end of engine mounting bracket 2 and measuring equipment mounting bracket 3, the support performance of guarantee part that center support frame 17 and side fixed plate 19 can be better, it fixes to use the bolt to pass installation fixed orifices 20, the protective properties of guarantee part that crashproof foam-rubber cushion 16 can be better, fixed stay horizontal pole 11, when the guarantee that shock attenuation fixed cushion 12 and wear-resisting boss 13 can be better descends, fixed stay horizontal pole 11 can be when falling to the ground, the rotation through damping pivot 15 drives fixed stay horizontal pole 11 and rotates, shock attenuation fixed cushion 12 wear-resisting boss 13 can be when the ground is not steady better the stability performance that the guarantee supported, the practicality is higher.
It is obvious to a person skilled in the art that the invention is not restricted to details of the above-described exemplary embodiments, but that it can be implemented in other specific forms without departing from the spirit or essential characteristics of the invention. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Claims (7)
1. The utility model provides a survey and drawing unmanned aerial vehicle measuring device installation mechanism, is including installation main fixed block (1), its characterized in that: engine mounting bracket (2) are installed to the below of installation main fixed block (1), measuring equipment mounting bracket (3) are installed to the below of engine mounting bracket (2), wing mounting bracket (4) are all installed to the both sides of installation main fixed block (1), the one end of installation main fixed block (1) is installed and is connected fixed block (6), wing installation block (7) are installed in the outside of connecting fixed block (6), side installation fixed block (8) are all installed to the outside both sides of engine mounting bracket (2), support mount (9) are installed in the outside of side installation fixed block (8), shock attenuation stabilizing frame (10) are installed in the outside of support mount (9) below.
2. The surveying and mapping drone measuring device mounting mechanism of claim 1, characterized in that: the mounting main fixing block (1), the measuring equipment mounting frame (3) and the engine mounting frame (2) are connected through bolts, and the wing mounting frame (4) is fixedly connected with the mounting main fixing block (1).
3. The surveying and mapping drone measuring device mounting mechanism of claim 1, characterized in that: the anti-collision fixing gasket (5) is arranged outside the wing mounting frame (4), and the anti-collision fixing gasket (5) is connected with the wing mounting frame (4) in a sticking mode.
4. The surveying and mapping drone measuring device mounting mechanism of claim 1, characterized in that: side installation fixed block (8) and engine mounting bracket (2) and the equal fixed connection of support mount (9), the lower extreme of support mount (9) is provided with rotation spacing groove (14).
5. The surveying and mapping drone measuring device mounting mechanism of claim 1, characterized in that: the damping stabilizing frame is characterized in that a fixed supporting cross rod (11) is arranged inside the damping stabilizing frame (10), the fixed supporting cross rod (11) and the supporting fixing frame (9) are rotatably connected through a damping rotating shaft (15), damping fixing cushion blocks (12) are arranged on two sides of the fixed supporting cross rod (11), wear-resistant reinforcing blocks (13) are arranged outside the damping fixing cushion blocks (12), and the wear-resistant reinforcing blocks (13) are fixedly connected with the damping fixing cushion blocks (12).
6. The surveying and mapping drone measuring device mounting mechanism of claim 1, characterized in that: the anti-collision sponge mat (16) is installed to the inboard of engine mounting bracket (2), central support frame (17) is installed to the inside intermediate position department of engine mounting bracket (2), the outside of central support frame (17) is provided with side fixed plate (19).
7. The surveying and mapping drone measuring device mounting mechanism of claim 6, characterized by: side fixed plate (19) are provided with a plurality of, and a plurality of side fixed plate (19) distribute in proper order, the intermediate position department of central bracing frame (17) is provided with fixed orifices (18), all be provided with installation fixed orifices (20) on central bracing frame (17) and side fixed plate (19).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022052699.XU CN213323728U (en) | 2020-09-18 | 2020-09-18 | Survey and drawing unmanned aerial vehicle measuring device installation mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022052699.XU CN213323728U (en) | 2020-09-18 | 2020-09-18 | Survey and drawing unmanned aerial vehicle measuring device installation mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN213323728U true CN213323728U (en) | 2021-06-01 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022052699.XU Active CN213323728U (en) | 2020-09-18 | 2020-09-18 | Survey and drawing unmanned aerial vehicle measuring device installation mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN213323728U (en) |
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2020
- 2020-09-18 CN CN202022052699.XU patent/CN213323728U/en active Active
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