CN220616197U - Modularized unmanned aerial vehicle - Google Patents
Modularized unmanned aerial vehicle Download PDFInfo
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- CN220616197U CN220616197U CN202322395312.4U CN202322395312U CN220616197U CN 220616197 U CN220616197 U CN 220616197U CN 202322395312 U CN202322395312 U CN 202322395312U CN 220616197 U CN220616197 U CN 220616197U
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- 230000003014 reinforcing effect Effects 0.000 abstract description 4
- 230000009286 beneficial effect Effects 0.000 abstract description 3
- 238000009434 installation Methods 0.000 description 5
- 230000000694 effects Effects 0.000 description 4
- 230000003139 buffering effect Effects 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000003760 hair shine Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 238000004904 shortening Methods 0.000 description 1
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Abstract
The utility model discloses a modularized unmanned aerial vehicle, which relates to the technical field of modularized unmanned aerial vehicles and comprises an unmanned aerial vehicle body, wherein a supporting frame is fixedly arranged at the bottom of the unmanned aerial vehicle body, fixing plates are symmetrically arranged at the top of the supporting frame, telescopic rods are symmetrically arranged at the bottoms of two fixing plates, a spring is fixedly arranged at the outer end of each telescopic rod, and a reinforcing plate is fixedly arranged at the bottom of each spring and at the bottom of each telescopic rod. The beneficial effects of the utility model are as follows: through the cooperation between telescopic link and the spring, the telescopic link can recover with the help of the elasticity of spring, reduces unmanned aerial vehicle body to the damage of support frame when descending, and then guaranteed the result of use of support frame, through the cooperation between connecting rod and the pulley, carries out the auxiliary slip with pulley inertia and descends, and then avoids the direct friction between support frame and the contact surface, has improved modularized unmanned aerial vehicle's life.
Description
Technical Field
The utility model relates to the technical field of modularized unmanned aerial vehicles, in particular to a modularized unmanned aerial vehicle.
Background
The modularized unmanned aerial vehicle in the prior life is beneficial to realizing flexible and rapid deployment, shortening the development period, realizing project development in a short period and realizing economic and effective performance improvement.
Chinese patent CN216783852U proposes a modularization unmanned aerial vehicle, which comprises a frame, the top of frame is provided with the host computer, the bottom of frame is provided with the battery piece, be connected with the horn all around of frame, the tip fixed mounting of horn has the rotor, the bottom of frame is connected with the supporting leg, the equal fixedly connected with L shape cardboard in both sides of frame roof, the slip draw-in groove has all been seted up to the bottom of host computer both sides, slip draw-in groove and L shape cardboard slip block, be provided with locking device between L shape cardboard and the host computer, realize modularization disconnect-type design through messenger's frame, host computer and battery piece to when in-service use, selectively assemble the three according to different operation requirement, simultaneously, each module damage can be changed alone or maintained, thereby avoids unmanned aerial vehicle whole to scrap, and then has greatly improved convenience and the practicality that unmanned aerial vehicle used.
According to the scheme, the three can be selectively assembled according to different use requirements, the modules can be singly replaced or maintained due to damage, but when the modularized unmanned aerial vehicle falls, the modularized unmanned aerial vehicle has a general buffering effect, can slide above the ground for a certain distance, and is easy to wear the bottom of the support frame, so that the service life of the modularized unmanned aerial vehicle is reduced.
The utility model comprises the following steps:
the utility model aims to solve the problems and provide the modularized unmanned aerial vehicle, the device utilizes the cooperation between the connecting rod and the pulley to achieve the effect of landing by auxiliary sliding by the inertia of the pulley, thereby avoiding direct friction between the supporting frame and the contact surface, improving the service life of the modularized unmanned aerial vehicle and solving the problems in the background art.
In order to solve the problems, the utility model provides a technical scheme that:
the utility model provides a modularization unmanned aerial vehicle, includes the unmanned aerial vehicle body, the bottom fixed mounting of unmanned aerial vehicle body has braced frame, braced frame's top symmetry installs the fixed plate, two the telescopic link is installed to the bottom symmetry of fixed plate, every the outer fixed mounting of telescopic link has the spring, and every the bottom of spring just is located the bottom fixed mounting of telescopic link has the gusset plate, the inside fixed mounting of gusset plate has the connecting rod, a plurality of pulleys are evenly installed to the outer end of connecting rod.
As a preferable scheme of the utility model, the outer end of the unmanned aerial vehicle body is uniformly provided with a plurality of wings, the top of each wing is fixedly provided with a propeller, the top of the unmanned aerial vehicle body is fixedly provided with a radiator, and the radiator is positioned among the plurality of wings.
As a preferable scheme of the utility model, the bottom of the supporting frame is fixedly provided with a mounting shell, an adjusting component is arranged in the mounting shell, and a replacing component is arranged at the bottom of the adjusting component.
As a preferable scheme of the utility model, the adjusting component comprises a driving motor, the driving motor is fixedly arranged on one side of the supporting frame, a movable rotating shaft is fixedly arranged at the output end of the driving motor, and the movable rotating shaft extends to the inside of the mounting shell to be connected in a rotating way.
As a preferable scheme of the utility model, the outer end of the movable rotating shaft is fixedly provided with a worm, one side of the worm is connected with a worm wheel in a meshed manner, the worm wheel is rotationally connected with the mounting shell, and a fixing rod is fixedly arranged at the bottom of the worm wheel and extends to the bottom of the mounting shell.
As a preferable scheme of the utility model, the replacing component comprises a threaded rod, the threaded rod is in threaded connection with the inside of the fixed rod, a camera is fixedly arranged at the outer end of the threaded rod and extends to the lower part of the fixed rod, a threaded hole is formed in the camera, and the threaded hole is in threaded connection with the threaded rod.
The beneficial effects of the utility model are as follows: through the cooperation between telescopic link and the spring, the telescopic link can recover with the help of the elasticity of spring, reduces unmanned aerial vehicle body to the damage of support frame when descending, and then guaranteed the result of use of support frame, through the cooperation between connecting rod and the pulley, carries out the auxiliary slip with pulley inertia and descends, and then avoids the direct friction between support frame and the contact surface, has improved modularized unmanned aerial vehicle's life.
Description of the drawings:
for ease of illustration, the utility model is described in detail by the following detailed description and the accompanying drawings.
FIG. 1 is a schematic view of the overall structure of the present utility model;
FIG. 2 is a schematic diagram of the overall internal structure of the present utility model;
FIG. 3 is a schematic view of the wear prevention structure of the present utility model;
fig. 4 is an enlarged view of fig. 2 a in accordance with the present utility model.
In the figure: 1. an unmanned aerial vehicle body; 2. a support frame; 3. a fixing plate; 4. a telescopic rod; 5. a spring; 6. a reinforcing plate; 7. a connecting rod; 8. a pulley; 9. a wing; 10. a propeller; 11. a heat sink; 12. a mounting shell; 13. an adjustment assembly; 131. a driving motor; 132. a movable rotating shaft; 133. a worm; 134. a worm wheel; 135. a fixed rod; 14. replacing the component; 141. a threaded rod; 142. a camera; 143. and (3) a threaded hole.
The specific embodiment is as follows:
the technical solutions in the embodiments of the present utility model will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present utility model.
Examples:
as shown in fig. 1, 2 and 3, the present utility model provides a technical solution: a modularized unmanned aerial vehicle comprises an unmanned aerial vehicle body 1, a supporting frame 2 is fixedly arranged at the bottom of the unmanned aerial vehicle body 1, a fixing plate 3 is symmetrically arranged at the top of the supporting frame 2, telescopic rods 4 are symmetrically arranged at the bottoms of the two fixing plates 3, springs 5 are fixedly arranged at the outer ends of each telescopic rod 4, impact force generated by contact between the unmanned aerial vehicle body 1 and a contact surface can be transmitted to the springs 5 through the telescopic rods 4, the springs 5 are used for buffering the generated vibration, so that the impact effect of the impact force on the supporting frame 2 is reduced, the springs 5 have certain elasticity, the damping effect is achieved, a reinforcing plate 6 is fixedly arranged at the bottom of each spring 5 and at the bottom of the telescopic rod 4, a connecting rod 7 is fixedly arranged in the reinforcing plate 6, a plurality of pulleys 8 are uniformly arranged at the outer ends of the connecting rod 7, the pulleys 8 have inertia, the auxiliary use is achieved, the unmanned aerial vehicle body 1 descends, the pulleys 8 slide on the ground, the pulleys 8 can support the unmanned aerial vehicle body 1,
as shown in fig. 1 and 2, further, the outer end of unmanned aerial vehicle body 1 evenly is provided with a plurality of wings 9, wing 9 drives unmanned aerial vehicle body 1 and flies, wing 9 is in order to support unmanned aerial vehicle body 1 and fly in the air, it still plays certain stability and manipulation, the top fixed mounting of every wing 9 has screw 10, start a plurality of screw 10 and rotate, screw 10 drives wing 9 and flies, the top fixed mounting of unmanned aerial vehicle body 1 has radiator 11, radiator 11 is located between a plurality of wings 9, the bottom fixed mounting of braced frame 2 has installation shell 12, the inside of installation shell 12 is provided with adjusting part 13, the bottom of adjusting part 13 is provided with replacement subassembly 14.
As shown in fig. 1, fig. 2 and fig. 4, further, the adjusting component 13 includes a driving motor 131, the driving motor 131 is fixedly arranged at one side of the supporting frame 2, a movable rotating shaft 132 is fixedly arranged at the output end of the driving motor 131, the driving motor 131 drives the movable rotating shaft 132 to rotate, the movable rotating shaft 132 drives a worm 133 to rotate, the movable rotating shaft 132 extends to the inside of the installation shell 12 to rotate and connect, a worm 133 is fixedly arranged at the outer end of the movable rotating shaft 132, two shafts driven by the worm gear 134 are mutually intersected and perpendicular to each other, a worm gear 134 is connected to one side of the worm 133 in a meshing manner, the worm gear 133 drives the worm gear 134 to rotate, the worm gear 134 drives the camera 142 to rotate, the irradiation angle of the camera 142 is adjusted, the worm gear 134 is rotationally connected with the installation shell 12, and a fixing rod 135 is fixedly arranged at the bottom of the worm gear 134 and extends to the installation shell 12.
As shown in fig. 1, 2 and 4, further, the replacing component 14 includes a threaded rod 141, when the camera 142 needs to be replaced, the threaded rod 141 is rotated, the threaded rod 141 is in threaded connection with the inside of the fixed rod 135, the camera 142 is fixedly installed below the fixed rod 135 at the outer end of the threaded rod 141 and extends to the lower end of the fixed rod 135, the camera 142 is hemispherical, a threaded hole 143 is formed in the inside of the camera 142, the threaded rod 141 is adjusted out of the threaded hole 143, and then the camera 142 is taken out for replacement, and the threaded hole 143 is in threaded connection with the threaded rod 141.
Working principle: starting a plurality of propellers 10 and rotating, the propellers 10 drive wing 9 and fly, wing 9 drives unmanned aerial vehicle body 1 and flies, when needing angle regulation, start driving motor 131, driving motor 131 drives movable pivot 132 and rotates, movable pivot 132 drives worm 133 and rotates, worm 133 drives worm wheel 134 and rotates, worm wheel 134 drives camera 142 and rotates, adjust the angle that camera 142 shines, when descending, unmanned aerial vehicle body 1 descends, a plurality of pulleys 8 slide on the ground, make pulley 8 can support unmanned aerial vehicle body 1, the impact force that produces at unmanned aerial vehicle body 1 and contact surface contact can pass through telescopic link 4 and transmit spring 5, buffer memory with the vibrations that spring 5 produced, thereby also reduced impact force to braced frame 2's impact effect, when needing to replace camera 142, rotate threaded rod 141, 141 is adjusted out from the inside of screw hole 143, then take out camera 142 and replace.
Although embodiments of the present utility model have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The utility model provides a modularization unmanned aerial vehicle, its characterized in that, includes unmanned aerial vehicle body (1), the bottom fixed mounting of unmanned aerial vehicle body (1) has braced frame (2), fixed plate (3) are installed to the top symmetry of braced frame (2), two telescopic link (4) are installed to the bottom symmetry of fixed plate (3), every the outer fixed mounting of telescopic link (4) has spring (5), and every the bottom of spring (5) just is located the bottom fixed mounting of telescopic link (4) has gusset plate (6), the inside fixed mounting of gusset plate (6) has connecting rod (7), a plurality of pulleys (8) are evenly installed to the outer end of connecting rod (7).
2. A modular unmanned aerial vehicle according to claim 1, wherein the outer end of the unmanned aerial vehicle body (1) is uniformly provided with a plurality of wings (9), the top of each wing (9) is fixedly provided with a propeller (10), the top of the unmanned aerial vehicle body (1) is fixedly provided with a radiator (11), and the radiator (11) is located between the plurality of wings (9).
3. A modular unmanned aerial vehicle according to claim 1, wherein the bottom of the support frame (2) is fixedly provided with a mounting shell (12), the inside of the mounting shell (12) is provided with an adjusting assembly (13), and the bottom of the adjusting assembly (13) is provided with a replacement assembly (14).
4. A modular unmanned aerial vehicle according to claim 3, wherein the adjustment assembly (13) comprises a drive motor (131), the drive motor (131) is fixedly arranged on one side of the support frame (2), a movable rotating shaft (132) is fixedly arranged at the output end of the drive motor (131), and the movable rotating shaft (132) extends to the inner rotary connection of the mounting shell (12).
5. The modularized unmanned aerial vehicle according to claim 4, wherein a worm (133) is fixedly arranged at the outer end of the movable rotating shaft (132), a worm wheel (134) is connected to one side of the worm (133) in a meshed manner, the worm wheel (134) is rotatably connected with the mounting shell (12), and a fixing rod (135) is fixedly arranged at the bottom of the worm wheel (134) and extends to the bottom of the mounting shell (12).
6. A modular unmanned aerial vehicle according to claim 3, wherein the replacement assembly (14) comprises a threaded rod (141), the threaded rod (141) is in threaded connection with the inside of the fixed rod (135), a camera (142) is fixedly arranged at the outer end of the threaded rod (141) and extends to the lower part of the fixed rod (135), a threaded hole (143) is formed in the camera (142), and the threaded hole (143) is in threaded connection with the threaded rod (141).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322395312.4U CN220616197U (en) | 2023-09-05 | 2023-09-05 | Modularized unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322395312.4U CN220616197U (en) | 2023-09-05 | 2023-09-05 | Modularized unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220616197U true CN220616197U (en) | 2024-03-19 |
Family
ID=90226191
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322395312.4U Active CN220616197U (en) | 2023-09-05 | 2023-09-05 | Modularized unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220616197U (en) |
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2023
- 2023-09-05 CN CN202322395312.4U patent/CN220616197U/en active Active
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