CN220054162U - Debugging tool for unmanned aerial vehicle mounting device - Google Patents
Debugging tool for unmanned aerial vehicle mounting device Download PDFInfo
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- CN220054162U CN220054162U CN202321462613.8U CN202321462613U CN220054162U CN 220054162 U CN220054162 U CN 220054162U CN 202321462613 U CN202321462613 U CN 202321462613U CN 220054162 U CN220054162 U CN 220054162U
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- fixedly connected
- mounting device
- unmanned aerial
- aerial vehicle
- groove
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- 230000001681 protective effect Effects 0.000 claims description 19
- 229920000742 Cotton Polymers 0.000 claims description 9
- 238000009413 insulation Methods 0.000 claims 1
- 238000000034 method Methods 0.000 description 4
- 208000033999 Device damage Diseases 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000000630 rising effect Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 1
Abstract
The utility model discloses a debugging tool for an unmanned aerial vehicle mounting device, which relates to the technical field of unmanned aerial vehicles and comprises two cylindrical frames, wherein the top of each cylindrical frame is fixedly connected with a first fixing ball, one side of each first fixing ball is fixedly connected with a first transverse frame, one side of each first transverse frame is fixedly connected with a second fixing ball, the bottom of each cylindrical frame is fixedly connected with a third fixing ball, one side of each second fixing ball is fixedly connected with a second transverse frame, and a lifting assembly is arranged in each cylindrical frame. According to the utility model, the column-shaped frame, the transverse frame I and the transverse frame II can be fixed by arranging the column-shaped frame, the fixing ball I, the transverse frame I, the fixing ball II, the fixing ball III, the transverse frame II and the fixing ball IV which are matched with each other, so that the damage of the support when an unmanned aerial vehicle falls due to misoperation of an operator is prevented, and the damage of materials is prevented.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a debugging tool for an unmanned aerial vehicle mounting device.
Background
Unmanned aerial vehicle is abbreviated as "unmanned aerial vehicle", and english abbreviation is "UAV", is unmanned aerial vehicle that utilizes radio remote control equipment and self-contained program control device to operate, or by on-vehicle computer completely or intermittently independently operate, and current unmanned aerial vehicle can carry out data acquisition through the mounting device to upload remote control center, control center will acquire data and carry out analysis, helps improving actual work efficiency.
The existing mounting device is easy to be unstable when being used on an unmanned aerial vehicle, the mounting device is easy to fall off the unmanned aerial vehicle when the unmanned aerial vehicle works, materials are damaged, normal work cannot be achieved, angles cannot be adjusted, and the mounting device is inconvenient to acquire more accurate data.
Disclosure of Invention
The utility model aims to provide a debugging tool for an unmanned aerial vehicle mounting device, so as to solve the problems in the background technology.
In order to solve the technical problems, the utility model adopts the following technical scheme: including cylindricality frame, its characterized in that: the number of the column frames is two, the top of the column frames is fixedly connected with a first fixed ball, one side of the first fixed ball is fixedly connected with a first transverse frame, one side of the first transverse frame is fixedly connected with a second fixed ball, the bottom of the column frames is fixedly connected with a third fixed ball, one side of the fixed ball is fixedly connected with a second transverse frame, one side of the first transverse frame is fixedly connected with a fourth fixed ball, and a lifting assembly is arranged in the column frames.
A debugging frock for unmanned aerial vehicle mounting device, including cylindricality frame, its characterized in that: the number of the column frames is two, the top of the column frames is fixedly connected with a first fixed ball, one side of the first fixed ball is fixedly connected with a first transverse frame, one side of the first transverse frame is fixedly connected with a second fixed ball, the bottom of the column frames is fixedly connected with a third fixed ball, one side of the fixed ball is fixedly connected with a second transverse frame, one side of the first transverse frame is fixedly connected with a fourth fixed ball, and a lifting assembly is arranged in the column frames.
By adopting the technical scheme, in the scheme, through setting up the mutual cooperation of cylindricality frame, fixed ball, horizontal type frame one, fixed ball two, fixed ball three, horizontal type frame two and fixed ball four, fixed ball one, fixed ball two, fixed ball three and fixed ball four can fix cylindricality frame, horizontal type frame one and horizontal type frame two, have prevented that operating personnel from making the unmanned aerial vehicle fall time support damage because of misoperation, lead to the material damage.
The technical scheme of the utility model is further improved as follows: the lifting assembly comprises a limiting plate, a concave groove is formed in the upper surface of the limiting plate, a square box is fixedly connected to the inside of the concave groove, and a square groove is formed in the square box.
By adopting the technical scheme, in the scheme, through the mutual matching of the limiting plate, the concave groove, the square box and the square groove, the screw rod drives the square box and the push plate to slide upwards in the T-shaped sliding plate II in the T-shaped groove, so that the square box is separated from the limiting plate.
The technical scheme of the utility model is further improved as follows: the utility model discloses a square groove, including square groove, square box, motor, protection shell, top swing joint has the push pedal of screw rod, the inside fixedly connected with soundproof cotton of protection shell, the inside of protection shell is provided with the motor, the top fixedly connected with screw rod of motor, the top of screw rod runs through to the top of protection shell, the bottom of push pedal and the top contact of square box.
Adopt above-mentioned technical scheme, through setting up protective housing, soundproof cotton, motor, screw rod and push pedal mutually supporting in this scheme, the user starts the motor, and the motor drives the inside rotation of screw rod protective housing, and the inside soundproof cotton of protective housing can prevent that noise can be made at unmanned aerial vehicle in flight in-process motor, influences the attention of controlling personnel.
The technical scheme of the utility model is further improved as follows: the inside fixedly connected with spacing shell one of concave long board and spacing shell two, the right side of spacing shell one and the left side contact of spacing shell two, the bottom of spacing shell one and spacing shell two and the top contact of push pedal.
By adopting the technical scheme, the stability of the mounting device is improved by arranging the first limiting shell and the second limiting shell to be matched with each other, the mounting device is prevented from falling off when rising, the material is easy to damage, and the mounting device cannot work normally.
The technical scheme of the utility model is further improved as follows: the screw hole is formed in one side of the first limiting shell, the bolt is connected with the inner thread of the screw hole, and the left side of the first limiting shell is detachably connected with the right side of the second limiting shell through the bolt.
By adopting the technical scheme, the screw holes and the bolts are matched with each other in the scheme, so that the first limit shell and the second limit shell can be conveniently installed or disassembled.
The technical scheme of the utility model is further improved as follows: the inside of spacing shell one and spacing shell two has all seted up the semicircle groove, the inside of semicircle groove is provided with the mounting device.
By adopting the technical scheme, through setting up the cooperation of semicircle groove and mounting device in this scheme, can carry out spacingly to mounting device, prevent that mounting device from breaking away from because of unmanned aerial vehicle upset or when descending fast when the during operation, lead to mounting device damage, unable normal work.
The technical scheme of the utility model is further improved as follows: the T-shaped groove is formed in the cylindrical frame, the T-shaped first sliding plate and the T-shaped second sliding plate are connected in the T-shaped groove in a sliding mode, a concave gripper is fixedly connected to one side of the T-shaped first sliding plate, one side of the concave gripper is contacted with one side of the first limiting shell, and one side of the T-shaped second sliding plate is fixedly connected with one side of the push plate.
By adopting the technical scheme, through setting up the mutually supporting of T type groove, T type slide two and concave tongs in this scheme, the screw rod drives square box and push pedal at the inside of T type slide two at T type groove upwards slides, and T type slide one drives concave tongs, spacing shell one, spacing shell two and the inside upwards sliding of mounting device at T type groove simultaneously, when mounting device risees to the required position, the operating personnel is convenient for acquire more accurate data from mounting device.
By adopting the technical scheme, compared with the prior art, the utility model has the following technical progress: the mounting device is conveniently protected, the mounting device is conveniently subjected to angle adjustment, and operating personnel can conveniently acquire more accurate data from the mounting device.
1. The utility model provides a debugging tool for an unmanned aerial vehicle mounting device, which is characterized in that a column-shaped frame, a first fixing ball, a first transverse frame, a second fixing ball, a third fixing ball, a second transverse frame and a fourth fixing ball are arranged to be matched with each other, so that the column-shaped frame, the first transverse frame and the second transverse frame can be fixed, and the damage of a bracket when an operator falls down the unmanned aerial vehicle due to misoperation is prevented, thereby avoiding the damage of materials.
2. The utility model provides a debugging tool for an unmanned aerial vehicle mounting device, which is characterized in that a limiting plate, a concave groove, a square box and a square groove are arranged to be matched with each other, a screw rod drives the square box and a push plate to slide upwards in a T-shaped sliding plate II in the T-shaped groove, so that the square box is separated from the limiting plate.
3. The utility model provides a debugging tool for an unmanned aerial vehicle mounting device, which is characterized in that a motor is started by arranging a protective shell, soundproof cotton, a motor, a screw and a push plate to be matched with each other, the motor drives the screw to rotate in the protective shell, and the soundproof cotton in the protective shell can prevent noise from being produced by the motor in the flight process of the unmanned aerial vehicle, so that the attention of operators is influenced.
Drawings
FIG. 1 is a schematic diagram of the main structure of the present utility model;
FIG. 2 is a schematic view of a cylindrical frame structure according to the present utility model;
FIG. 3 is a schematic view of the first and second limiting shells according to the present utility model;
FIG. 4 is a schematic view of a lifting assembly according to the present utility model;
fig. 5 is a schematic diagram of a limiting plate structure according to the present utility model.
In the figure: 1. a cylindrical frame; 2. a first fixed ball; 3. a transverse frame I; 4. fixing a second ball; 5. a third fixed ball; 6. a transverse frame II; 7. a fixed ball IV; 8. a lifting assembly; 801. a limiting plate; 802. a concave groove; 803. square box; 804. a square groove; 805. a motor; 806. a screw; 807. a push plate; 808. a first limiting shell; 809. a second limiting shell; 810. a T-shaped groove; 811. a T-shaped sliding plate I; 812. a concave gripper; 813. a T-shaped sliding plate II; 9. a protective shell; 10. a semicircular groove.
Detailed Description
The utility model is further illustrated by the following examples:
example 1
As shown in fig. 1-5, the utility model provides a debugging tool for an unmanned aerial vehicle mounting device, which comprises two cylindrical frames 1, wherein the number of the cylindrical frames 1 is two, the top of each cylindrical frame 1 is fixedly connected with a first fixing ball 2, one side of each fixing ball 2 is fixedly connected with a first transverse frame 3, one side of each transverse frame is fixedly connected with a second fixing ball 4, the bottom of each cylindrical frame 1 is fixedly connected with a third fixing ball 5, one side of each fixing ball is fixedly connected with a second transverse frame 6, one side of each transverse frame is fixedly connected with a fourth fixing ball 7, a lifting assembly 8 is arranged in each cylindrical frame 1, each lifting assembly 8 comprises a limiting plate 801, a concave groove 802 is formed in the upper surface of each limiting plate 801, a square box 803 is fixedly connected with the inside of each concave groove 802, a square groove 804 is formed in the inside of each square box 803, the bottom of the inner wall of each square groove 804 is fixedly connected with a protective shell 9, a motor 805 is arranged in the inside each protective shell 9, the top of each motor 805 is fixedly connected with a screw 806, the top of each screw 806 penetrates to the top of the protective shell 9, the top of each screw 806 is movably connected with the top of each square 803, and the top of each square 803 is movably connected with a pushing plate 807.
In this embodiment, through setting up cylindricality frame 1, fixed ball one 2, horizontal type frame one 3, fixed ball two 4, fixed ball three 5, horizontal type frame two 6 and mutually supporting of fixed ball four 7, fixed ball one 2, fixed ball two 4, fixed ball three 5 and fixed ball four 7 can fix cylindricality frame 1, horizontal type frame one 3 and horizontal type frame two 6, the support damages when having prevented that operating personnel from making unmanned aerial vehicle fall because of misoperation, lead to the material to damage, through setting up limiting plate 801, concave groove 802, square box 803 and square groove 804 mutually supporting, screw rod 806 drives square box 803 and push pedal 807 at the inside of T type slide two 813 in groove 810, make square box 803 break away from with limiting plate 801, through setting up protective housing 9, soundproof cotton, motor 805, screw rod 806 and push pedal 807 mutually supporting, user's start motor 805, motor 805 drives the inside rotation of protective housing 9, the soundproof cotton inside protective housing 9 can prevent that motor 805 can make noise in the unmanned aerial vehicle in-flight process, control personnel's attention is influenced.
Example 2
As shown in fig. 1-5, on the basis of embodiment 1, the present utility model provides a technical solution: preferably, the inside fixedly connected with spacing shell one 808 and spacing shell two 809 of push pedal 807, the right side of spacing shell one 808 and the left side contact of spacing shell two 809, the bottom of spacing shell one 808 and spacing shell two 809 and the top contact of push pedal 807, the screw has been seted up to one side of spacing shell one 808, the inside threaded connection of screw has the bolt, the right side detachable connection of bolt and spacing shell two 809 is passed through in the left side of spacing shell one 808, semi-circular groove 10 has all been seted up to the inside of spacing shell one 808 and spacing shell two 809, the inside of semi-circular groove 10 is provided with the hanging device, T type groove 810 has been seted up to the inside of cylindricality frame 1, the inside sliding connection of T type groove 810 has T type slide one 811 and T type slide two 813, one side fixedly connected with concave tongs 812 of T type slide one side of 811 and one side contact of spacing shell one 808, one side of T type slide two 813 and one side fixed connection of push pedal 807.
In this embodiment, through setting up the mutually supporting of spacing shell one 808 and spacing shell two 809, the stability to the mounting device has been improved, the material damage has been caused easily to drop when having prevented to mount the device and rise, unable normal work, through setting up the mutually supporting of screw and bolt, be convenient for the installation or the disassembling of spacing shell one 808 and spacing shell two 809, through setting up the mutually supporting of semicircle groove 10 and mounting device, can carry out spacingly to the mounting device, prevent that mounting device breaks away from because of the mounting device breaks away from when unmanned aerial vehicle upset or descends fast in the during operation, lead to mounting device damage, unable normal work, through setting up T type groove 810, T type slide one 811, T type slide two 813 and concave type tongs 812 mutually supporting, screw 806 drives square box 803 and push pedal 813 at the inside of T type groove 810 upwards sliding, T type slide one 811 drives concave tongs 812 simultaneously, spacing shell two 809 and mounting device are upwards slid at the inside of T type groove 810, when mounting device rises to the required position, it is more accurate from the personnel to obtain the accurate data of controlling of being convenient for from the device.
The working principle of the debugging tool for the unmanned aerial vehicle mounting device is specifically described below.
As shown in fig. 1-5, when the angle adjustment needs to be performed on the mounting device, the motor 805 drives the screw rod 806 to rotate in the protective shell 9, the soundproof cotton in the protective shell 9 can prevent noise from being produced by the motor 805 in the flight process of the unmanned aerial vehicle, the attention of a control person is affected, the screw rod 806 drives the square box 803 and the push plate 807 to slide upwards in the T-shaped groove 810 in the T-shaped slide plate 813, meanwhile, the first T-shaped slide plate 811 drives the concave gripper 812, the first limit shell 808, the second limit shell 809 and the mounting device to slide upwards in the T-shaped groove 810, the first limit shell 808 and the second limit shell 809 are prevented from falling off when rising, the material is easy to damage, the mounting device cannot be protected, and when the mounting device rises to a required position, the control person is convenient to acquire more accurate data from the mounting device.
The foregoing utility model has been generally described in great detail, but it will be apparent to those skilled in the art that modifications and improvements can be made thereto. Accordingly, it is intended to cover modifications or improvements within the spirit of the inventive concepts.
Claims (7)
1. A debug frock for unmanned aerial vehicle mounting device, includes cylindricality frame (1), its characterized in that: the number of the column frames (1) is two, the top of the column frames (1) is fixedly connected with a first fixed ball (2), one side of the first fixed ball (2) is fixedly connected with a first transverse frame (3), one side of the first transverse frame is fixedly connected with a second fixed ball (4), the bottom of the column frames (1) is fixedly connected with a third fixed ball (5), one side of the fixed ball is fixedly connected with a second transverse frame (6), one side of the second transverse frame is fixedly connected with a fourth fixed ball (7), and a lifting assembly (8) is arranged in the column frames (1).
2. The debugging tool for the unmanned aerial vehicle mounting device according to claim 1, wherein: lifting assembly (8) are including limiting plate (801), concave groove (802) have been seted up to the upper surface of limiting plate (801), the inside fixedly connected with square box (803) of concave groove (802), square groove (804) are seted up to the inside of square box (803).
3. The debugging tool for the unmanned aerial vehicle mounting device according to claim 2, wherein: the utility model discloses a sound insulation box, including square groove (804) and square box (803), the bottom fixedly connected with protective housing (9) of square groove (804) inner wall, the inside fixedly connected with soundproof cotton of protective housing (9), the inside of protective housing (9) is provided with motor (805), the top fixedly connected with screw rod (806) of motor (805), the top of screw rod (806) runs through to the top of protective housing (9), the top swing joint of screw rod (806) has push pedal (807), the bottom of push pedal (807) and the top contact of square box (803).
4. A debugging tooling for an unmanned aerial vehicle mounting device according to claim 3, wherein: the inside fixedly connected with spacing shell one (808) of push pedal (807) and spacing shell two (809), the right side of spacing shell one (808) and the left side contact of spacing shell two (809), the bottom of spacing shell one (808) and spacing shell two (809) and the top contact of push pedal (807).
5. The debugging tool for the unmanned aerial vehicle mounting device according to claim 4, wherein: screw holes are formed in one side of the first limiting shell (808), bolts are connected to the inner threads of the screw holes, and the left side of the first limiting shell (808) is detachably connected with the right side of the second limiting shell (809) through the bolts.
6. The debugging tool for the unmanned aerial vehicle mounting device according to claim 4, wherein: the inside of spacing shell one (808) and spacing shell two (809) has all been seted up semicircle groove (10), the inside of semicircle groove (10) is provided with the mounting device.
7. The debugging tool for the unmanned aerial vehicle mounting device according to claim 1, wherein: t type groove (810) have been seted up to the inside of cylindricality frame (1), the inside sliding connection in T type groove (810) has T type slide (811) and T type slide two (813), one side fixedly connected with concave type tongs (812) of T type slide one (811), one side of concave type tongs (812) and one side contact of spacing shell one (808), one side of T type slide two (813) and one side fixed connection of push pedal (807).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321462613.8U CN220054162U (en) | 2023-06-09 | 2023-06-09 | Debugging tool for unmanned aerial vehicle mounting device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321462613.8U CN220054162U (en) | 2023-06-09 | 2023-06-09 | Debugging tool for unmanned aerial vehicle mounting device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220054162U true CN220054162U (en) | 2023-11-21 |
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ID=88788224
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321462613.8U Active CN220054162U (en) | 2023-06-09 | 2023-06-09 | Debugging tool for unmanned aerial vehicle mounting device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220054162U (en) |
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2023
- 2023-06-09 CN CN202321462613.8U patent/CN220054162U/en active Active
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