CN212243771U - Spliced combined unmanned aerial vehicle - Google Patents
Spliced combined unmanned aerial vehicle Download PDFInfo
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- CN212243771U CN212243771U CN202020545272.0U CN202020545272U CN212243771U CN 212243771 U CN212243771 U CN 212243771U CN 202020545272 U CN202020545272 U CN 202020545272U CN 212243771 U CN212243771 U CN 212243771U
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Abstract
The utility model discloses a concatenation combination formula unmanned aerial vehicle, including the unmanned aerial vehicle main part, the mounting panel is installed to the bottom of unmanned aerial vehicle main part, the bottom of mounting panel is provided with the framework, spacing subassembly and framework fixed connection are passed through to the surface of framework, the bracket component is installed to the bottom of framework, spacing subassembly includes the fixed plate, the fixed plate is installed on the inner wall of framework. The utility model discloses a set up spacing subassembly, make unmanned aerial vehicle's installation relatively stable, when needs are dismantled unmanned aerial vehicle, only need rotate the screw, take out the screw from the framework, stimulate the framework, make mounting panel and framework separation, then rotate the handle again, make the adapter sleeve break away from the thread bush, can dismantle the support frame, and easy operation is convenient for carry out the dismouting to unmanned aerial vehicle, has reduced staff's intensity of labour, avoid expending more time and energy, bring very big facility for the user.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is a concatenation combination formula unmanned aerial vehicle.
Background
Unmanned aircraft, or drone for short, are unmanned aircraft that are operated by radio remote control devices and self-contained program control devices, or autonomously by an on-board computer, either completely or intermittently, and are often more suited to tasks that are too "foolproof, dirty, or dangerous" than manned aircraft. Unmanned aerial vehicles can be classified into military and civil according to application fields. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology. At present common unmanned aerial vehicle is not convenient for carry out the dismouting, when needs are maintained, because the dismouting is more difficult, has increased staff's intensity of labour, need consume more time and energy, brings very big inconvenience for the user, for this reason we propose a concatenation combination formula unmanned aerial vehicle.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a concatenation combination formula unmanned aerial vehicle to solve the problem that proposes in the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: a spliced combined unmanned aerial vehicle comprises an unmanned aerial vehicle main body, wherein a mounting plate is mounted at the bottom of the unmanned aerial vehicle main body, a frame body is arranged at the bottom of the mounting plate, the surface of the frame body is fixedly connected with the frame body through a limiting assembly, and a support assembly is mounted at the bottom of the frame body;
the limiting assembly comprises a fixed plate, the fixed plate is installed on the inner wall of the frame body, a fixed sleeve is installed at the top of the fixed plate, a spring is installed inside the fixed sleeve, a positioning rod is installed at the top end of the spring, the surface of the positioning rod is movably connected with the fixed sleeve, the top end of the positioning rod is fixedly connected with the installation plate, a limiting groove is formed in the top of the frame body, a limiting sleeve is installed at the bottom of the installation plate, the bottom of the limiting sleeve penetrates through the limiting groove and extends to the outside of the limiting groove, the surface of the limiting sleeve is movably connected with the limiting groove, an installation sleeve is installed at the bottom of the installation plate and located on the outer side of the frame body, a screw is arranged on the outer side of the installation sleeve, and one end, close;
the bracket component includes the connecting plate, the connecting plate sets up inside the framework, the surface of connecting plate and the inner wall swing joint of framework, install the thread bush on the inner wall of framework, the adapter sleeve is installed at the top of connecting plate, the cutting ferrule is installed at the top of thread bush, supreme thread bush and the cutting ferrule and extend to inside under the top of adapter sleeve in proper order, the surface of adapter sleeve and the inner wall threaded connection of thread bush, the support frame is installed to the bottom of connecting plate.
Preferably, the bottom of the mounting plate is in close contact with the frame.
Preferably, the surface of the frame body is provided with a positioning sleeve, and the bottom of the mounting sleeve penetrates through the positioning sleeve and extends into the positioning sleeve.
Preferably, a reinforcing rib is installed at the top of the fixing plate, and one end, close to the frame body, of the reinforcing rib is fixedly connected with the fixing plate.
Preferably, a handle is arranged at the midpoint of the bottom of the connecting plate.
Compared with the prior art, the beneficial effects of the utility model are as follows:
1. the utility model discloses a set up spacing subassembly, make unmanned aerial vehicle's installation relatively stable, when needs are dismantled unmanned aerial vehicle, only need rotate the screw, take out the screw from the framework, stimulate the framework, make mounting panel and framework separation, then rotate the handle again, make the adapter sleeve break away from the thread bush, can dismantle the support frame, and easy operation is convenient for carry out the dismouting to unmanned aerial vehicle, has reduced staff's intensity of labour, avoid expending more time and energy, bring very big facility for the user.
2. The utility model discloses a set up the position sleeve and played and carried out spacing effect to the installation cover, played through setting up the strengthening rib and carried out reinforced (rfd) effect to the junction of fixed plate and framework, played the effect of being convenient for rotate the connecting plate through setting up the handle.
Drawings
FIG. 1 is a sectional view of the front view of the present invention;
FIG. 2 is an enlarged view of a portion of A-A of FIG. 1 according to the present invention;
fig. 3 is a partial enlarged view of B-B in fig. 1 according to the present invention.
In the figure: 1 unmanned aerial vehicle main part, 2 mounting panels, 3 frameworks, 4 spacing subassemblies, 41 fixed plates, 42 fixed cover, 43 spring, 44 locating levers, 45 spacing grooves, 46 spacing cover, 47 installation cover, 48 screws, 5 bracket components, 51 connecting plate, 52 thread bush, 53 adapter sleeve, 54 cutting ferrule, 55 support frames, 6 position sleeve, 7 strengthening ribs, 8 handles.
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.
Please refer to fig. 1-3, a splicing combined type unmanned aerial vehicle comprises an unmanned aerial vehicle main body 1, a mounting plate 2 is installed at the bottom of the unmanned aerial vehicle main body 1, a frame body 3 is arranged at the bottom of the mounting plate 2, the bottom of the mounting plate 2 is in close contact with the frame body 3, the surface of the frame body 3 is fixedly connected with the frame body 3 through a limiting component 4, and a support component 5 is installed at the bottom of the frame body 3.
The limiting component 4 comprises a fixing plate 41, a reinforcing rib 7 is installed at the top of the fixing plate 41, one end of the reinforcing rib 7 close to the frame body 3 is fixedly connected with the fixing plate, the reinforcing rib 7 is arranged to reinforce the joint of the fixing plate 41 and the frame body 3, the fixing plate 41 is installed on the inner wall of the frame body 3, a fixing sleeve 42 is installed at the top of the fixing plate 41, a spring 43 is installed inside the fixing sleeve 42, a positioning rod 44 is installed at the top end of the spring 43, the surface of the positioning rod 44 is movably connected with the fixing sleeve 42, the top end of the positioning rod 44 is fixedly connected with the mounting plate 2, a limiting groove 45 is formed in the top of the frame body 3, a limiting sleeve 46 is installed at the bottom of the mounting plate 2, the bottom of the limiting sleeve 46 penetrates through the limiting groove 45 and extends to the outside of the limiting groove, the, the surface mounting of framework 3 has position sleeve 6, and the bottom of installation cover 47 runs through position sleeve 6 and extends to its inside, has played through setting up position sleeve 6 and has carried out spacing effect to installation cover 47, and the outside of installation cover 47 is provided with screw 48, and the one end that screw 48 is close to framework 3 runs through installation cover 47, stop collar 46 and framework 3 in proper order and extends to the inside of framework 3.
The working principle is as follows: through setting up spacing subassembly 4, locating lever 44 hold-down spring 43 in spacing subassembly 4, make stop collar 46 get into spacing groove 45, make installation cover 47 and stop collar 46 fix on framework 3 through screw 48, make unmanned aerial vehicle's installation more stable, when needs dismantle unmanned aerial vehicle, only need rotate screw 48, take out screw 48 from framework 3, pulling framework 3, make mounting panel 2 and framework 3 separation, then rotate handle 8 again, make adapter sleeve 53 break away from thread bush 52, can dismantle support frame 55, and the operation is thus simple, be convenient for carry out the dismouting to unmanned aerial vehicle, staff's intensity of labour has been reduced, avoid consuming more time and energy, bring very big facility for the user.
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 concatenation combination formula unmanned aerial vehicle, includes unmanned aerial vehicle main part (1), its characterized in that: the unmanned aerial vehicle is characterized in that a mounting plate (2) is mounted at the bottom of the unmanned aerial vehicle main body (1), a frame body (3) is arranged at the bottom of the mounting plate (2), the surface of the frame body (3) is fixedly connected with the frame body (3) through a limiting component (4), and a support component (5) is mounted at the bottom of the frame body (3);
the limiting component (4) comprises a fixing plate (41), the fixing plate (41) is installed on the inner wall of the frame body (3), a fixing sleeve (42) is installed at the top of the fixing plate (41), a spring (43) is installed inside the fixing sleeve (42), a positioning rod (44) is installed at the top end of the spring (43), the surface of the positioning rod (44) is movably connected with the fixing sleeve (42), the top end of the positioning rod (44) is fixedly connected with the mounting plate (2), a limiting groove (45) is formed in the top of the frame body (3), a limiting sleeve (46) is installed at the bottom of the mounting plate (2), the bottom of the limiting sleeve (46) penetrates through the limiting groove (45) and extends to the outside of the limiting groove (45), the surface of the limiting sleeve (46) is movably connected with the limiting groove (45), and the mounting sleeve (47) is installed at the bottom of the mounting plate (2) and located, a screw (48) is arranged on the outer side of the mounting sleeve (47), and one end, close to the frame body (3), of the screw (48) penetrates through the mounting sleeve (47), the limiting sleeve (46) and the frame body (3) in sequence and extends into the frame body (3);
bracket component (5) are including connecting plate (51), connecting plate (51) set up inside framework (3), the surface of connecting plate (51) and the inner wall swing joint of framework (3), install thread bush (52) on the inner wall of framework (3), adapter sleeve (53) are installed at the top of connecting plate (51), cutting ferrule (54) is installed at the top of thread bush (52), supreme thread bush (52) and cutting ferrule (54) and extend to inside from down run through in proper order in the top of adapter sleeve (53), the surface of adapter sleeve (53) and the inner wall threaded connection of thread bush (52), support frame (55) are installed to the bottom of connecting plate (51).
2. The spliced combined unmanned aerial vehicle of claim 1, wherein: the bottom of the mounting plate (2) is in close contact with the frame body (3).
3. The spliced combined unmanned aerial vehicle of claim 1, wherein: the surface mounting of framework (3) has position sleeve (6), the bottom of installation cover (47) runs through position sleeve (6) and extends to inside.
4. The spliced combined unmanned aerial vehicle of claim 1, wherein: reinforcing ribs (7) are installed at the top of the fixing plate (41), and one end, close to the frame body (3), of each reinforcing rib (7) is fixedly connected with the reinforcing rib.
5. The spliced combined unmanned aerial vehicle of claim 1, wherein: and a handle (8) is arranged at the midpoint of the bottom of the connecting plate (51).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020545272.0U CN212243771U (en) | 2020-04-14 | 2020-04-14 | Spliced combined unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020545272.0U CN212243771U (en) | 2020-04-14 | 2020-04-14 | Spliced combined unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212243771U true CN212243771U (en) | 2020-12-29 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020545272.0U Active CN212243771U (en) | 2020-04-14 | 2020-04-14 | Spliced combined unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212243771U (en) |
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2020
- 2020-04-14 CN CN202020545272.0U patent/CN212243771U/en active Active
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