CN212099344U - Environmental monitoring unmanned aerial vehicle with working mechanism easy to disassemble - Google Patents
Environmental monitoring unmanned aerial vehicle with working mechanism easy to disassemble Download PDFInfo
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- CN212099344U CN212099344U CN202020545273.5U CN202020545273U CN212099344U CN 212099344 U CN212099344 U CN 212099344U CN 202020545273 U CN202020545273 U CN 202020545273U CN 212099344 U CN212099344 U CN 212099344U
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Abstract
The utility model discloses an environment monitoring unmanned aerial vehicle with an easily detachable working mechanism, which comprises a flight assembly and a disassembly assembly, wherein the disassembly assembly is fixedly arranged at the bottom of the flight assembly; the flight assembly comprises a bottom plate, a flight motor is fixedly mounted at the top of the bottom plate, a flight rotating shaft is fixedly connected onto an output shaft at the top of the flight motor, flight blades are fixedly mounted at the top end of the flight rotating shaft, an undercarriage is fixedly connected to the bottom of the bottom plate, and a dismounting groove is formed in the bottom of the bottom plate; the dismouting subassembly includes the backup pad of fixed mounting on dismouting inslot wall right side. The utility model discloses a mutually supporting of flight subassembly and dismouting subassembly has realized an environment monitoring unmanned aerial vehicle who easily dismantles operating mechanism for the dismantlement of whole work main part becomes labour saving and time saving, has greatly alleviateed staff's work burden, makes things convenient for the staff to maintain or maintain the work main part, and the practicality is high, is fit for using widely.
Description
Technical Field
The utility model relates to an environmental monitoring unmanned aerial vehicle technical field specifically is an easily dismantle operating device's environmental monitoring unmanned aerial vehicle.
Background
At the in-process that carries out environmental monitoring, often need to use monitoring unmanned aerial vehicle, current environmental monitoring unmanned aerial vehicle is difficult for dismantling operating mechanism, and whole operating mechanism's dismantlement work is wasted time and energy, needs to spend the more time of staff and energy, has increased staff's work burden, and inconvenient staff maintains and maintains operating mechanism, and the practicality is low.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an easily dismantle operating device's environmental monitoring unmanned aerial vehicle to solve the problem that proposes in the background art.
In order to achieve the above object, the utility model provides a following technical scheme: an environment monitoring unmanned aerial vehicle with an easily detachable working mechanism comprises a flight assembly and a disassembling and assembling assembly, wherein the disassembling and assembling assembly is fixedly installed at the bottom of the flight assembly;
the flight assembly comprises a bottom plate, a flight motor is fixedly mounted at the top of the bottom plate, a flight rotating shaft is fixedly connected to an output shaft at the top of the flight motor, flight blades are fixedly mounted at the top end of the flight rotating shaft, an undercarriage is fixedly connected to the bottom of the bottom plate, and a dismounting groove is formed in the bottom of the bottom plate;
the disassembly and assembly component comprises a supporting plate fixedly arranged on the right side of the inner wall of the disassembly and assembly groove, a connecting block is arranged on the left side of the supporting plate, a working main body is fixedly connected to the bottom of the connecting block, the left side of the supporting plate penetrates through the connecting block and extends to the interior of the supporting plate to be movably connected with the supporting plate, a transverse plate is fixedly connected to the right side of the connecting block, a vertical rod is movably connected to the bottom of the transverse plate, a moving plate is fixedly connected to the bottom of the vertical rod, the top end of the vertical rod penetrates through the transverse plate and the supporting plate in sequence and extends to the interior of the supporting plate to be movably connected with the supporting plate, a first spring is sleeved on the surface of the vertical rod and is positioned between the transverse plate and the moving plate, the transverse plate and, the surface of telescopic link has cup jointed the second spring, pass through second spring fixed connection between diaphragm and the cardboard, the left bottom fixedly connected with fixture block of cardboard, the left side of fixture block runs through the movable plate and extends to its inside rather than swing joint.
Preferably, the top of the connecting block is contacted with the top of the inner wall of the dismounting groove.
Preferably, the left end of the second spring is fixedly connected with the transverse plate, and the right end of the second spring is fixedly connected with the left side of the clamping plate.
Preferably, the left side of the clamping plate and the right side of the moving plate are in contact with each other.
Compared with the prior art, the beneficial effects of the utility model are as follows:
the utility model discloses a mutually supporting of flight subassembly and dismouting subassembly has realized an environment monitoring unmanned aerial vehicle who easily dismantles operating mechanism for the dismantlement of whole work main part becomes labour saving and time saving, has greatly alleviateed staff's work burden, makes things convenient for the staff to maintain or maintain the work main part, and the practicality is high, is fit for using widely.
Drawings
FIG. 1 is a structural section view in elevation of the present invention;
fig. 2 is a schematic structural diagram of a top view of the present invention;
fig. 3 is a structural section view of the front view of the dismounting assembly of the present invention.
In the figure: the flying assembly comprises a flying assembly 1, a bottom plate 101, a flying motor 102, a flying rotating shaft 103, flying blades 104, a landing gear 105, a dismounting groove 106, a dismounting assembly 2, a supporting plate 201, a connecting block 202, a working body 203, a transverse plate 204, a vertical rod 205, a moving plate 206, a first spring 207, a telescopic rod 208, a clamping plate 209, a second spring 210 and a clamping block 211.
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 environment monitoring unmanned aerial vehicle with a working mechanism easy to detach comprises a flying assembly 1 and a dismounting assembly 2, wherein the dismounting assembly 2 is fixedly installed at the bottom of the flying assembly 1.
The flight assembly 1 comprises a bottom plate 101, a flight motor 102 is fixedly mounted at the top of the bottom plate 101, a flight rotating shaft 103 is fixedly connected to an output shaft at the top of the flight motor 102, flight blades 104 are fixedly mounted at the top end of the flight rotating shaft 103, an undercarriage 105 is fixedly connected to the bottom of the bottom plate 101, and a detachable groove 106 is formed in the bottom of the bottom plate 101.
The dismounting assembly 2 comprises a supporting plate 201 fixedly arranged on the right side of the inner wall of the dismounting groove 106, a connecting block 202 is arranged on the left side of the supporting plate 201, the top of the connecting block 202 is contacted with the top of the inner wall of the dismounting groove 106, the bottom of the connecting block 202 is fixedly connected with a working body 203, the working body 203 can be a gas detector in the prior art, the left side of the supporting plate 201 penetrates through the connecting block 202 and extends to the inside of the supporting plate 201 to be movably connected with the connecting block, a transverse plate 204 is fixedly connected with the right side of the connecting block 202, a vertical rod 205 is movably connected with the bottom of the transverse plate 204, a moving plate 206 is fixedly connected with the bottom of the vertical rod 205, the top end of the vertical rod 205 penetrates through the transverse plate 204 and the supporting plate 201 in sequence and is movably connected with the supporting plate 201, a first spring 207, an expansion link 208 is fixedly connected in a groove on the right side of the transverse plate 204, the right end of the expansion link 208 penetrates through the transverse plate 204 and extends to the outside of the transverse plate 204 and is fixedly connected with a clamping plate 209, the left side of the clamping plate 209 is contacted with the right side of the transverse plate 204, a second spring 210 is sleeved on the surface of the expansion link 208, the transverse plate 204 is fixedly connected with the clamping plate 209 through the second spring 210, the left end of the second spring 210 is fixedly connected with the transverse plate 204, the right end of the second spring 210 is fixedly connected with the left side of the clamping plate 209, the bottom of the left side of the clamping plate 209 is fixedly connected with a clamping block 211, the left side of the clamping plate 209 is contacted with the right side of the moving plate 206, the left side of the clamping block 211 penetrates through the moving plate 206 and extends to the inside of the moving plate and is movably connected with the clamping, the work burden of the staff is greatly reduced, the staff can maintain the work main body 203 conveniently, the practicability is high, and the popularization and the use are suitable.
During the use, the staff stimulates cardboard 209 to the right side, and cardboard 209 motion extension telescopic link 208 and second spring 210, and cardboard 209 drives fixture block 211 and breaks away from movable plate 206, and later, the staff stimulates movable plate 206 downwards, and movable plate 206 drives montant 205 and breaks away from backup pad 201, and finally, the staff stimulates work main part 203 to the left, and work main part 203 drives connecting block 202 and breaks away from the surface of backup pad 201, and the dismantlement work labour saving and time saving of work main part 203.
In summary, the following steps: this easily dismantle operating device's environmental monitoring unmanned aerial vehicle through mutually supporting of flight subassembly 1 and dismouting subassembly 2, has solved the problem of proposing in the background art.
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 (4)
1. The utility model provides an environment monitoring unmanned aerial vehicle of operating device easily dismantles, includes flight subassembly (1) and dismouting subassembly (2), its characterized in that: the dismounting assembly (2) is fixedly arranged at the bottom of the flying assembly (1);
the flight assembly (1) comprises a bottom plate (101), a flight motor (102) is fixedly mounted at the top of the bottom plate (101), a flight rotating shaft (103) is fixedly connected to an output shaft at the top of the flight motor (102), flight blades (104) are fixedly mounted at the top end of the flight rotating shaft (103), an undercarriage (105) is fixedly connected to the bottom of the bottom plate (101), and a dismounting groove (106) is formed in the bottom of the bottom plate (101);
the disassembly and assembly component (2) comprises a support plate (201) fixedly mounted on the right side of the inner wall of the disassembly and assembly groove (106), a connecting block (202) is arranged on the left side of the support plate (201), the bottom of the connecting block (202) is fixedly connected with a working main body (203), the left side of the support plate (201) penetrates through the connecting block (202) and extends to the inside of the support plate and is movably connected with the supporting block, a transverse plate (204) is fixedly connected with the right side of the connecting block (202), a vertical rod (205) is movably connected with the bottom of the transverse plate (204), a moving plate (206) is fixedly connected with the bottom of the vertical rod (205), the top end of the vertical rod (205) penetrates through the transverse plate (204) and the support plate (201) in sequence and extends to the inside of the support plate (201) and is movably connected with the supporting plate, a first spring (, the improved sliding block mechanism is characterized in that the transverse plate (204) and the moving plate (206) are fixedly connected through a first spring (207), a telescopic rod (208) is fixedly connected into a groove on the right side of the transverse plate (204), the right end of the telescopic rod (208) penetrates through the transverse plate (204) and extends to an external fixedly connected clamping plate (209), a second spring (210) is sleeved on the surface of the telescopic rod (208), the transverse plate (204) and the clamping plate (209) are fixedly connected through the second spring (210), a clamping block (211) is fixedly connected to the left bottom of the clamping plate (209), and the left side of the clamping block (211) penetrates through the moving plate (206) and extends to the inside of the moving plate and is movably connected with.
2. The environment monitoring unmanned aerial vehicle of claim 1, wherein the working mechanism is easy to disassemble, and the unmanned aerial vehicle comprises: the top of the connecting block (202) is contacted with the top of the inner wall of the dismounting groove (106).
3. The environment monitoring unmanned aerial vehicle of claim 1, wherein the working mechanism is easy to disassemble, and the unmanned aerial vehicle comprises: the left end of the second spring (210) is fixedly connected with the transverse plate (204), and the right end of the second spring (210) is fixedly connected with the left side of the clamping plate (209).
4. The environment monitoring unmanned aerial vehicle of claim 1, wherein the working mechanism is easy to disassemble, and the unmanned aerial vehicle comprises: the left side of the clamping plate (209) is contacted with the right side of the moving plate (206).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020545273.5U CN212099344U (en) | 2020-04-14 | 2020-04-14 | Environmental monitoring unmanned aerial vehicle with working mechanism easy to disassemble |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020545273.5U CN212099344U (en) | 2020-04-14 | 2020-04-14 | Environmental monitoring unmanned aerial vehicle with working mechanism easy to disassemble |
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| Publication Number | Publication Date |
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| CN212099344U true CN212099344U (en) | 2020-12-08 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202020545273.5U Active CN212099344U (en) | 2020-04-14 | 2020-04-14 | Environmental monitoring unmanned aerial vehicle with working mechanism easy to disassemble |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113665814A (en) * | 2021-09-24 | 2021-11-19 | 南京拓恒无人系统研究院有限公司 | Unmanned aerial vehicle with air detection system and detection method thereof |
-
2020
- 2020-04-14 CN CN202020545273.5U patent/CN212099344U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113665814A (en) * | 2021-09-24 | 2021-11-19 | 南京拓恒无人系统研究院有限公司 | Unmanned aerial vehicle with air detection system and detection method thereof |
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