CN216762158U - Floated unmanned aerial vehicle of improved generation - Google Patents
Floated unmanned aerial vehicle of improved generation Download PDFInfo
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- CN216762158U CN216762158U CN202220623985.3U CN202220623985U CN216762158U CN 216762158 U CN216762158 U CN 216762158U CN 202220623985 U CN202220623985 U CN 202220623985U CN 216762158 U CN216762158 U CN 216762158U
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Abstract
The utility model belongs to the technical field of unmanned aerial vehicles, and particularly relates to an improved suspended unmanned aerial vehicle, aiming at the problems that the undercarriage of the suspended unmanned aerial vehicle is inconvenient to disassemble and assemble and replace when damaged, the improved suspended unmanned aerial vehicle comprises a machine body, wherein a plurality of motors are fixedly arranged at the top of the machine body, rotors are fixedly arranged on output shafts of the motors, a mounting plate is fixedly arranged at the bottom of the machine body, two undercarriages are arranged at the bottom of the mounting plate, a supporting plate is fixedly arranged at the bottoms of the two undercarriages, a first T-shaped block and a second T-shaped block are fixedly arranged at the tops of the two undercarriages respectively, two T-shaped grooves with openings at one sides are formed in the bottom of the mounting plate, the outer sides of the first T-shaped block and the second T-shaped block are respectively contacted with the inner walls of the two T-shaped grooves, and a threaded groove is formed in one side of the mounting plate. The utility model is convenient for dismounting the two undercarriages and is convenient for replacing when damaged.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to an improved suspended unmanned aerial vehicle.
Background
The unmanned plane is an unmanned plane which is operated by a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by an on-board computer, and the suspended unmanned plane refers to an unmanned plane which can be suspended in the air.
The undercarriage of the existing suspension type unmanned aerial vehicle is not convenient to disassemble and assemble, and is not convenient to replace when damaged, so that the improved suspension type unmanned aerial vehicle is provided, and the problem is solved.
SUMMERY OF THE UTILITY MODEL
The utility model aims to solve the defect that a landing gear of a suspension type unmanned aerial vehicle is inconvenient to assemble and disassemble, and provides an improved suspension type unmanned aerial vehicle.
In order to achieve the purpose, the utility model adopts the following technical scheme:
the utility model provides a floated unmanned aerial vehicle of improved generation, includes the organism, the top fixed mounting of organism has a plurality of motors, and equal fixed mounting has the rotor on the output shaft of a plurality of motors, the bottom fixed mounting of organism has the mounting panel, and two undercarriage are installed to the bottom of mounting panel, and the equal fixed mounting in bottom of two undercarriage has the backup pad, and the top of two undercarriage is fixed mounting respectively first T-shaped piece and second T-shaped piece, and two one side has been seted up to the bottom of mounting panel and has been established to open-ended T-shaped groove, the outside of first T-shaped piece and second T-shaped piece respectively with the inner wall contact in two T-shaped grooves, the thread groove has been seted up to one side of mounting panel, and the locking bolt is installed to the thread groove internal thread, has seted up the fixed orifices on the first T-shaped piece, and the one end of locking bolt runs through the fixed orifices, be equipped with fixed establishment on the mounting panel.
Preferably, the fixing mechanism comprises a fixing rod, a slot is formed in one side of the second T-shaped block, and one end of the fixing rod is clamped with the slot.
Preferably, a sliding hole is formed in the inner wall of one side of the threaded groove, the outer side of the fixing rod is connected with the inner wall of the sliding hole in a sliding mode, and one end of the locking bolt is in contact with the other end of the fixing rod.
Preferably, the inner wall of the sliding hole is provided with a reset groove, a reset block is arranged in the reset groove in a sliding mode, and the reset block is fixedly connected with the fixed rod.
Preferably, one side of the reset block is fixedly provided with one end of a spring, and the other end of the spring is fixedly connected with the inner wall of one side of the reset groove.
Compared with the prior art, the utility model has the advantages that:
(1) when the scheme is installed, the first T-shaped block and the second T-shaped block are inserted into the two T-shaped grooves from side openings of the two T-shaped grooves, the locking bolt penetrates through the fixing hole to be fixedly connected with the thread groove through threads, the first T-shaped block is fixed in the T-shaped groove on the left side, the fixing rod is clamped into the slot rightwards, the second T-shaped block is fixed in the T-shaped groove on the right side, and then the two landing gears are installed;
(2) during disassembly, the locking bolt is withdrawn from the fixing hole, the spring is reset, the reset block drives the fixing rod to be separated from the slot, the second T-shaped block is removed from being fixed, then the two undercarriage are pushed to move horizontally, the first T-shaped block and the second T-shaped block are separated from the two T-shaped slots, the two undercarriage are disassembled, and replacement is convenient;
the utility model is convenient for dismounting the two undercarriage, and is convenient for replacing when damaged.
Drawings
Fig. 1 is a schematic structural view of an improved suspension type unmanned aerial vehicle according to the present invention;
fig. 2 is an enlarged schematic structural diagram of a portion a in fig. 1 of an improved suspension type unmanned aerial vehicle according to the present invention;
fig. 3 is an enlarged schematic structural diagram of a portion B in fig. 1 of an improved suspension type unmanned aerial vehicle according to the present invention;
fig. 4 is a schematic perspective view of a mounting plate of an improved suspension type unmanned aerial vehicle according to the present invention;
fig. 5 is a schematic structural diagram of a second embodiment of an improved suspension-type unmanned aerial vehicle according to the present invention;
fig. 6 is an enlarged schematic structural diagram of a portion C in fig. 5 of an improved suspension type unmanned aerial vehicle according to the present invention.
In the figure: 1. a body; 2. a motor; 3. a rotor; 4. mounting a plate; 5. a landing gear; 6. a support plate; 7. a T-shaped slot; 8. a first T-shaped block; 9. a second T-shaped block; 10. a fixing hole; 11. a slot; 12. a thread groove; 13. locking the bolt; 14. fixing the rod; 15. a reset block; 16. a spring; 17. placing the blocks; 18. a buffer block; 19. a buffer spring.
Detailed Description
The technical solutions in the embodiments will be described clearly and completely with reference to the drawings in the embodiments, and it is obvious that the described embodiments are only a part of the embodiments, but not all embodiments.
Example one
Referring to fig. 1-4, an improved suspension type unmanned aerial vehicle comprises a machine body 1, a plurality of motors 2 are fixedly mounted at the top of the machine body 1, rotors 3 are fixedly mounted on output shafts of the motors 2, a mounting plate 4 is fixedly mounted at the bottom of the machine body 1, two landing gears 5 are mounted at the bottom of the mounting plate 4, a support plate 6 is fixedly mounted at the bottoms of the two landing gears 5, a first T-shaped block 8 and a second T-shaped block 9 are fixedly mounted at the tops of the two landing gears 5 respectively, two T-shaped grooves 7 with openings formed at one sides are formed at the bottom of the mounting plate 4, the outer sides of the first T-shaped block 8 and the second T-shaped block 9 are in contact with the inner walls of the two T-shaped grooves 7 respectively, a threaded groove 12 is formed at one side of the mounting plate 4, a locking bolt 13 is mounted in the threaded groove 12, a fixing hole 10 is formed in the first T-shaped block 8, and one end of the locking bolt 13 penetrates through the fixing hole 10, the mounting plate 4 is provided with a fixing mechanism.
In this embodiment, the fixing mechanism includes a fixing rod 14, a slot 11 is formed on one side of the second T-shaped block 9, and one end of the fixing rod 14 is clamped with the slot 11.
In this embodiment, a sliding hole is formed in an inner wall of one side of the thread groove 12, an outer side of the fixing rod 14 is slidably connected to the inner wall of the sliding hole, and one end of the locking bolt 13 contacts with the other end of the fixing rod 14.
In this embodiment, the inner wall of the sliding hole is provided with a reset groove, a reset block 15 is slidably installed in the reset groove, and the reset block 15 is fixedly connected with the fixing rod 14.
In this embodiment, one side of the reset block 15 is fixedly installed with one end of a spring 16, and the other end of the spring 16 is fixedly connected with the inner wall of one side of the reset groove.
In this embodiment, during installation, the first T-shaped block 8 and the second T-shaped block 9 are inserted into the two T-shaped slots 7 from the side openings of the two T-shaped slots 7, then the locking bolt 13 is rotated, the locking bolt 13 passes through the fixing hole 10 to be fixed with the thread groove 12 in a threaded manner, the first T-shaped block 8 is fixed in the T-shaped slot 7 on the left, when the locking bolt 13 enters the thread groove 12, the fixing rod 14 is pushed to move rightwards, the fixing rod 14 drives the resetting block 15 to move, the resetting block 15 extrudes the spring 16, the fixing rod 14 is clamped into the slot 11 rightwards, the second T-shaped block 9 is fixed in the T-shaped slot 7 on the right, and then installation of the two landing gears 5 is completed, when the locking bolt 13 is reversed, the locking bolt 13 exits the fixing hole 10, fixing of the first T-shaped block 8 is released, and simultaneously, the spring 16 is reset, so that the resetting block 15 drives the fixing rod 14 to move leftwards, the fixing rod 14 is separated from the slot 11, the fixing of the second T-shaped block 9 is released, and then the two undercarriage 5 are pushed to move horizontally, so that the first T-shaped block 8 and the second T-shaped block 9 are separated from the two T-shaped grooves 7, the two undercarriage 5 are disassembled, and the replacement is convenient.
Example two
Referring to fig. 5 and 6, the difference from the first embodiment is that: comprises a machine body 1, a plurality of motors 2 are fixedly arranged at the top of the machine body 1, rotors 3 are fixedly arranged on output shafts of the motors 2, a mounting plate 4 is fixedly arranged at the bottom of the machine body 1, two landing gears 5 are arranged at the bottom of the mounting plate 4, buffer grooves are formed at the bottoms of the landing gears 5, buffer blocks 18 are slidably arranged in the buffer grooves, placing blocks 17 are fixedly arranged at the bottoms of the buffer blocks 18, buffer springs 19 are fixedly arranged at the tops of the buffer blocks 18, the top ends of the buffer springs 19 are fixedly connected with the inner walls of the tops of the two buffer grooves respectively, a first T-shaped block 8 and a second T-shaped block 9 are fixedly arranged at the tops of the landing gears 5 respectively, two T-shaped grooves 7 with openings are formed at one side of the bottom of the mounting plate 4, the outer sides of the first T-shaped block 8 and the second T-shaped block 9 are contacted with the inner walls of the two T-shaped grooves 7 respectively, thread groove 12 has been seted up to one side of mounting panel 4, and locking bolt 13 has been installed to 12 internal threads of thread groove, has seted up fixed orifices 10 on the first T-shaped piece 8, and fixing hole 10 is run through to the one end of locking bolt 13, is equipped with fixed establishment on mounting panel 4.
The rest is the same as the first embodiment.
The above descriptions are only preferred embodiments of the present invention, but the scope of the present invention is not limited thereto, and any person skilled in the art should be considered to be within the scope of the present invention, and the technical solutions and the utility model concepts of the present invention are equivalent to, replaced or changed.
Claims (5)
1. An improved suspension type unmanned aerial vehicle comprises a machine body (1), wherein a plurality of motors (2) are fixedly mounted at the top of the machine body (1), and rotors (3) are fixedly mounted on output shafts of the motors (2), the improved suspension type unmanned aerial vehicle is characterized in that a mounting plate (4) is fixedly mounted at the bottom of the machine body (1), two landing gears (5) are mounted at the bottom of the mounting plate (4), a supporting plate (6) is fixedly mounted at the bottom of the two landing gears (5), a first T-shaped block (8) and a second T-shaped block (9) are fixedly mounted at the tops of the two landing gears (5) respectively, two T-shaped grooves (7) with openings formed at one sides are formed at the bottom of the mounting plate (4), the outer sides of the first T-shaped block (8) and the second T-shaped block (9) are in contact with the inner walls of the two T-shaped grooves (7) respectively, a threaded groove (12) is formed at one side of the mounting plate (4), locking bolt (13) are installed to thread groove (12) internal thread, have seted up on first T-shaped piece (8) fixed orifices (10), and fixed orifices (10) are run through to the one end of locking bolt (13), be equipped with fixed establishment on mounting panel (4).
2. The improved suspended unmanned aerial vehicle of claim 1, wherein the fixing mechanism comprises a fixing rod (14), one side of the second T-shaped block (9) is provided with a slot (11), and one end of the fixing rod (14) is clamped with the slot (11).
3. The improved suspended unmanned aerial vehicle as claimed in claim 2, wherein a sliding hole is formed in an inner wall of one side of the thread groove (12), an outer side of the fixing rod (14) is slidably connected with an inner wall of the sliding hole, and one end of the locking bolt (13) is in contact with the other end of the fixing rod (14).
4. The improved suspended unmanned aerial vehicle as claimed in claim 3, wherein a reset groove is formed in an inner wall of the sliding hole, a reset block (15) is slidably mounted in the reset groove, and the reset block (15) is fixedly connected with the fixing rod (14).
5. The improved suspended unmanned aerial vehicle of claim 4, wherein one side of the reset block (15) is fixedly provided with one end of a spring (16), and the other end of the spring (16) is fixedly connected with the inner wall of one side of the reset groove.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220623985.3U CN216762158U (en) | 2022-03-22 | 2022-03-22 | Floated unmanned aerial vehicle of improved generation |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220623985.3U CN216762158U (en) | 2022-03-22 | 2022-03-22 | Floated unmanned aerial vehicle of improved generation |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216762158U true CN216762158U (en) | 2022-06-17 |
Family
ID=81959417
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202220623985.3U Active CN216762158U (en) | 2022-03-22 | 2022-03-22 | Floated unmanned aerial vehicle of improved generation |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216762158U (en) |
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2022
- 2022-03-22 CN CN202220623985.3U patent/CN216762158U/en active Active
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