CN220298780U - Electric adjusting and installing structure of vertical take-off and landing unmanned aerial vehicle - Google Patents
Electric adjusting and installing structure of vertical take-off and landing unmanned aerial vehicle Download PDFInfo
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- CN220298780U CN220298780U CN202321763846.1U CN202321763846U CN220298780U CN 220298780 U CN220298780 U CN 220298780U CN 202321763846 U CN202321763846 U CN 202321763846U CN 220298780 U CN220298780 U CN 220298780U
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- 238000009434 installation Methods 0.000 claims abstract description 34
- 230000005611 electricity Effects 0.000 claims abstract description 18
- 230000001681 protective effect Effects 0.000 claims description 5
- 230000001105 regulatory effect Effects 0.000 description 5
- 238000012423 maintenance Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
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Abstract
The utility model discloses an electric adjustment installation structure of a vertical take-off and landing unmanned aerial vehicle, which comprises a vertical take-off and landing unmanned aerial vehicle main body: rectangular grooves are formed in the lower side of the vertical take-off and landing unmanned aerial vehicle main body, mounting units are arranged on the inner sides of the rectangular grooves, connecting grooves are formed in the left and right inner walls of the rectangular grooves, springs are fixedly connected to the inner sides of the connecting grooves, mounting blocks are fixedly connected to the outer sides of the springs, the mounting units comprise electric adjusting boxes, and the electric adjusting boxes are arranged on the inner sides of the rectangular grooves. Through being provided with rectangular channel, spread groove, spring, installation piece, electricity and transfer case, draw-in groove, spout, slide, retaining plate, control panel, lifting block and screw rod, the spring and the installation piece of the left and right sides of being convenient for are spacing to the left and right sides of electricity and transfer the case, when need dismantling the electricity and transfer case, rotate the screw rod and make the control panel fast control retaining plate remove, make the electricity transfer case dismantle fast, easy operation.
Description
Technical Field
The utility model relates to the technical field of vertical take-off and landing unmanned aerial vehicles, in particular to an electric adjustment installation structure of a vertical take-off and landing unmanned aerial vehicle.
Background
Unmanned aerial vehicles, abbreviated as "unmanned aerial vehicles", abbreviated as "UAVs", are unmanned aerial vehicles that are operated by means of radio remote control devices and self-contained programmed control devices, or are operated autonomously, either entirely or intermittently, by an onboard computer.
When using perpendicular unmanned aerial vehicle that takes off and land, need use electricity to transfer the structure and control unmanned aerial vehicle's motor, make unmanned aerial vehicle can take off and land perpendicularly, electricity transfers the structure setting in unmanned aerial vehicle's cabin, when unmanned aerial vehicle receives great striking, makes unmanned aerial vehicle damage easily, needs to dismantle the electricity and transfers the structure, because the inside dismantlement degree of difficulty in position cabin increases, increases later maintenance people's work load.
Disclosure of Invention
In order to overcome the defect that an electric adjusting box in an unmanned aerial vehicle is inconvenient to detach in the prior art, one of the purposes of the utility model is to provide an electric adjusting installation structure of a vertical take-off and landing unmanned aerial vehicle.
One of the purposes of the utility model is realized by adopting the following technical scheme: the utility model provides a perpendicular take off and land unmanned aerial vehicle's electricity transfers mounting structure, includes perpendicular take off and land unmanned aerial vehicle main part: the lower side of the vertical take-off and landing unmanned aerial vehicle main body is provided with a rectangular groove, the inner side of the rectangular groove is provided with a mounting unit, the left and right inner walls of the rectangular groove are provided with connecting grooves, the inner side of the connecting groove is fixedly connected with a spring, and the outer side of the spring is fixedly connected with a mounting block;
the installation unit includes the electricity and transfers the case, the electricity transfers the case setting in the inboard of rectangular channel, the draw-in groove has all been seted up to the left and right sides of electricity and transferred the case, the spout has all been seted up to the upside at both ends about the electricity transfer case, the left and right sides the inboard of spout all sliding connection has the slide, the downside fixedly connected with of slide holds out the board, the upside fixedly connected with connecting plate of slide, the left and right sides the upside of connecting plate is all fixedly connected with commentaries on classics piece one, the outside rotation of commentaries on classics piece one is connected with the control panel, the outside fixedly connected with fixed block of control panel, the outside rotation of fixed block is connected with commentaries on classics piece two, the outside fixedly connected with lifter of commentaries on classics piece two, the upside rotation of electricity transfer case is connected with the screw rod.
According to the electric adjustment installation structure of the vertical take-off and landing unmanned aerial vehicle, the screw rod is in threaded connection with the lifting block. The lifting block is convenient to control to move up and down.
According to the electric adjustment installation structure of the vertical take-off and landing unmanned aerial vehicle, the upper end of the screw is fixedly connected with the turntable. The screw is convenient to control to rotate.
According to the electric adjustment installation structure of the vertical take-off and landing unmanned aerial vehicle, the retaining plate is located at the inner side of the clamping groove and is in sliding connection with the clamping groove. And the moving of the retaining plate is facilitated.
According to the electric adjustment installation structure of the vertical take-off and landing unmanned aerial vehicle, a protective cover is fixedly connected to the upper side of the electric adjustment box. The internal control board is convenient to protect.
According to the electric adjustment installation structure of the vertical take-off and landing unmanned aerial vehicle, the installation block is in sliding connection with the connecting groove.
The beneficial effects are that:
through being provided with rectangular channel, spread groove, spring, installation piece, electricity and transfer case, draw-in groove, spout, slide, retaining plate, control panel, lifting block and screw rod, the spring and the installation piece of the left and right sides of being convenient for are spacing to the left and right sides of electricity and transfer the case, when need dismantling the electricity and transfer case, rotate the screw rod and make the control panel fast control retaining plate remove, make the electricity transfer case dismantle fast, easy operation.
Additional aspects and advantages of the utility model will be set forth in part in the description which follows, and in part will be obvious from the description, or may be learned by practice of the utility model.
Drawings
The utility model is further described below with reference to the drawings and examples;
FIG. 1 is a perspective view of the whole structure of an electric adjustment installation structure of a vertical take-off and landing unmanned aerial vehicle;
FIG. 2 is a cross-sectional perspective view of a vertical take-off and landing unmanned aerial vehicle of the present utility model with an electrically tunable mounting structure with a mounting unit removed;
FIG. 3 is an enlarged view of FIG. 2 at A;
FIG. 4 is a cross-sectional perspective view of a mounting unit in an electrically tunable mounting structure of a vertical take-off and landing unmanned aerial vehicle according to the present utility model;
FIG. 5 is an enlarged view at B in FIG. 4;
fig. 6 is an enlarged view at C in fig. 4.
Legend description:
1. a vertical take-off and landing unmanned aerial vehicle main body; 2. rectangular grooves; 3. an installation unit; 301. an electric regulating box; 302. a clamping groove; 303. a protective cover; 304. a chute; 305. a slide plate; 306. a connecting plate; 307. a first rotating block; 308. a control board; 309. a fixed block; 310. a second rotating block; 311. a lifting block; 312. a screw; 313. a turntable; 314. a retaining plate; 4. a connecting groove; 5. a spring; 6. and (5) installing a block.
Detailed Description
Reference will now be made in detail to the present embodiments of the present utility model, examples of which are illustrated in the accompanying drawings, wherein the accompanying drawings are used to supplement the description of the written description so that one can intuitively and intuitively understand each technical feature and overall technical scheme of the present utility model, but not to limit the scope of the present utility model.
Referring to fig. 1-6, an electric adjustment installation structure of a vertical take-off and landing unmanned aerial vehicle according to an embodiment of the present utility model includes a vertical take-off and landing unmanned aerial vehicle main body 1: rectangular slot 2 has been seted up to the downside of perpendicular take off and land unmanned aerial vehicle main part 1, rectangular slot 2's inboard is provided with installation unit 3, rectangular slot 2's the left and right sides inner wall has all been seted up spread groove 4, spread groove 4's inboard fixedly connected with spring 5, spring 5's outside fixedly connected with installation piece 6, installation piece 6 and spread groove 4 sliding connection, when using, through the elasticity of spring 5 of left and right sides, make spring 5 drive installation piece 6 remove, make installation piece 6 and draw-in groove 302 cooperation, be convenient for spacing to electric regulating box 301 of left and right sides, make electric regulating box 301 be installed in rectangular slot 2, wherein installation piece 6's outside is provided with the fillet (as shown in figure 3), when convenient installation, electric regulating box 301 supports installation piece 6, make installation piece 6 remove in spread groove 4.
The installation unit 3 includes electric adjustment case 301, electric adjustment case 301 sets up the inboard in rectangular channel 2, draw-in groove 302 has all been seted up to electric adjustment case 301's left and right sides, spout 304 has all been seted up to electric adjustment case 301's the upside at both ends, the inboard of left and right sides spout 304 all sliding connection has slide plate 305, slide plate 305's downside fixedly connected with retaining plate 314, retaining plate 314 is located the inboard of draw-in groove 302, and retaining plate 314 and draw-in groove 302 sliding connection, slide plate 305's upside fixedly connected with connecting plate 306, the upside of left and right sides connecting plate 306 all fixedly connected with rotary block 307, rotary block 307's outside rotates and is connected with control panel 308, control panel 308's outside fixedly connected with fixed block 309, rotary block 309's outside rotates and is connected with rotary block two 310, rotary block 311 is connected with screw 312 in the upside rotation of this moment, screw 312 and lifting block 311 threaded connection, the upper end fixedly connected with carousel 313 of screw 312, when electric adjustment case 301 is required to dismantle, install piece 6 is located draw-in groove 302, the upside fixedly connected with connecting plate 306, rotary block 313 is rotated to the rotary block 313, then the rotary block 308 is driven to rotate by the rotary block 313, drive rotary block 308, make the rotary block 308 take off the rotary block 308, and then take off the rotary block 308 and take off the rotary block 308, and take off the rotary block 308 simply.
The upper side of the electric regulating box 301 is fixedly connected with a protective cover 303, and the protective cover 303 is convenient for protecting the control board 308 and the screw 312.
Working principle: when the electric box is used, a worker firstly places the electric box 301 in the rectangular groove 2, and during the placing process, the spring 5 and the mounting block 6 enable the mounting block 6 to enter the clamping groove 302, so that the electric box 301 is mounted in the rectangular groove 2.
When the electric box 301 needs to be disassembled, the staff rotates the rotary table 313 to drive the screw rods 312 to rotate, the screw rods 312 drive the control plates 308 on two sides to rotate, the control plates 308 drive the abutting plates 314 on the sliding plates 305 to move, the abutting plates 314 push the mounting blocks 6 out of the clamping grooves 302, and then the electric box 301 is taken out, so that the operation is simple, and the later maintenance is convenient.
The embodiments of the present utility model have been described in detail with reference to the accompanying drawings, but the present utility model is not limited to the above embodiments, and various changes can be made within the knowledge of one of ordinary skill in the art without departing from the spirit of the present utility model.
Claims (6)
1. The utility model provides an unmanned aerial vehicle's that takes off and land perpendicularly electricity transfers mounting structure which characterized in that, including unmanned aerial vehicle main part that takes off and land perpendicularly (1): rectangular grooves (2) are formed in the lower side of the vertical take-off and landing unmanned aerial vehicle main body (1), mounting units (3) are arranged on the inner sides of the rectangular grooves (2), connecting grooves (4) are formed in the left inner wall and the right inner wall of the rectangular grooves (2), springs (5) are fixedly connected to the inner sides of the connecting grooves (4), and mounting blocks (6) are fixedly connected to the outer sides of the springs (5);
the installation unit (3) comprises an electric adjusting box (301), the electric adjusting box (301) is arranged on the inner side of a rectangular groove (2), clamping grooves (302) are formed in the left side and the right side of the electric adjusting box (301), sliding grooves (304) are formed in the upper sides of the left end and the right end of the electric adjusting box (301), sliding plates (305) are slidably connected to the inner sides of the sliding grooves (304) in the left side and the right side, a retaining plate (314) is fixedly connected to the lower side of the sliding plates (305), a connecting plate (306) is fixedly connected to the upper side of the sliding plates (305), a rotating block I (307) is fixedly connected to the upper side of the connecting plate (306), a control plate (308) is rotatably connected to the outer side of the rotating block I (307), a rotating block II (310) is rotatably connected to the outer side of the fixing block (309), a lifting block (311) is fixedly connected to the outer side of the rotating block II (310), and the upper side of the electric adjusting box (301) is rotatably connected with a screw rod (312).
2. The electric adjustment installation structure of the vertical take-off and landing unmanned aerial vehicle according to claim 1, wherein the screw (312) is in threaded connection with the lifting block (311).
3. The electric adjustment installation structure of the vertical take-off and landing unmanned aerial vehicle according to claim 1, wherein the upper end of the screw (312) is fixedly connected with a turntable (313).
4. The electric adjustment installation structure of the vertical take-off and landing unmanned aerial vehicle according to claim 1, wherein the retaining plate (314) is located at the inner side of the clamping groove (302), and the retaining plate (314) is slidably connected with the clamping groove (302).
5. The electric tuning installation structure of the vertical take-off and landing unmanned aerial vehicle according to claim 1, wherein a protective cover (303) is fixedly connected to the upper side of the electric tuning box (301).
6. The electric adjustment installation structure of the vertical take-off and landing unmanned aerial vehicle according to claim 1, wherein the installation block (6) is in sliding connection with the connecting groove (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321763846.1U CN220298780U (en) | 2023-07-06 | 2023-07-06 | Electric adjusting and installing structure of vertical take-off and landing unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321763846.1U CN220298780U (en) | 2023-07-06 | 2023-07-06 | Electric adjusting and installing structure of vertical take-off and landing unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220298780U true CN220298780U (en) | 2024-01-05 |
Family
ID=89375709
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321763846.1U Active CN220298780U (en) | 2023-07-06 | 2023-07-06 | Electric adjusting and installing structure of vertical take-off and landing unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220298780U (en) |
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2023
- 2023-07-06 CN CN202321763846.1U patent/CN220298780U/en active Active
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