CN220263128U - Folding type air-sea dual-purpose unmanned aerial vehicle - Google Patents
Folding type air-sea dual-purpose unmanned aerial vehicle Download PDFInfo
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- CN220263128U CN220263128U CN202321780407.1U CN202321780407U CN220263128U CN 220263128 U CN220263128 U CN 220263128U CN 202321780407 U CN202321780407 U CN 202321780407U CN 220263128 U CN220263128 U CN 220263128U
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- 238000007667 floating Methods 0.000 claims abstract description 15
- 230000000694 effects Effects 0.000 claims abstract description 9
- 238000005452 bending Methods 0.000 abstract description 4
- 238000013016 damping Methods 0.000 abstract description 4
- 238000001125 extrusion Methods 0.000 abstract description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 12
- 238000007599 discharging Methods 0.000 description 8
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000004308 accommodation Effects 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
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Abstract
The utility model discloses a folding type air-sea dual-purpose unmanned aerial vehicle, which relates to the technical field of unmanned aerial vehicles and comprises an unmanned aerial vehicle body, wherein a connecting seat is fixedly connected to the bottom surface of the unmanned aerial vehicle body, a T-shaped sliding groove is formed in the bottom surface of the connecting seat, a T-shaped sliding block is connected to the inner wall of the T-shaped sliding groove in a sliding clamping mode, a floating plate is fixedly connected to the bottom surface of the T-shaped sliding block, a rotating groove is formed in the bottom surface of the floating plate, a supporting plate is rotatably connected to the inner wall of the rotating groove, and an anti-skid pad is fixedly connected to the bottom surface of the supporting plate. According to the utility model, the supporting plate is contacted with the ground to be bent to a certain angle under the action of pressure, the connecting rod is driven to push the sliding block to slide on the first sliding rod through the bending of the supporting plate, the second sliding block slides to extrude the second spring, and the second extrusion spring deforms to generate reverse force, so that a good damping effect on the unmanned aerial vehicle body is achieved, the damage of electronic elements in the unmanned aerial vehicle is avoided, and the service life of the unmanned aerial vehicle is influenced.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a folding type air-sea dual-purpose unmanned aerial vehicle.
Background
Along with the gradual maturity of unmanned aerial vehicle research and development technique, manufacturing cost reduces by a wide margin, and unmanned aerial vehicle has obtained wide application in each field, except military use, still is applied to agricultural plant protection, electric power inspection, police law enforcement, geological exploration, environmental monitoring, forest fire prevention etc. that take photo by plane. The following problems exist in the prior art:
according to patent publication number CN 213262901U: the utility model discloses an air-sea dual-purpose unmanned aerial vehicle, which comprises a main body, wherein two groups of propeller components are respectively arranged on two sides of the main body, and the unmanned aerial vehicle is characterized in that a water sucking and discharging component for changing the weight of the main body is fixedly arranged in the main body, the water sucking and discharging component is biased to one side of the main body, an air cylinder is fixedly arranged in the main body, a balancing weight is fixedly arranged in the air cylinder, the air cylinder is biased to the other side of the main body, when the water sucking and discharging component sucks water, the main body turns over, the propeller components push the main body to move in water, and when the water sucking and discharging component discharges water, the sum of the weights of the air cylinder and the balancing weight is equal to the weight of the water sucking and discharging component, so that the main body keeps balanced when flying in the air; the water sucking and discharging assembly is fixedly arranged in the main body, and is biased to one side of the main body, and the weight of the main body is regulated by water sucking and discharging of the water sucking and discharging assembly, so that the unmanned aerial vehicle can be freely switched in the air and in the water, and the working efficiency of the traditional underwater unmanned aerial vehicle is improved; and has simple structure, low production cost and wide application environment.
Because unmanned aerial vehicle's supporting leg does not possess the cushioning effect in the public patent, lead to appearing when descending, cause more or less damage to support and unmanned aerial vehicle body, influence unmanned aerial vehicle's life's problem.
Disclosure of Invention
The utility model provides a folding type air-sea dual-purpose unmanned aerial vehicle, which aims to solve the problems in the background technology.
In order to solve the technical problems, the utility model adopts the following technical scheme:
the utility model provides a folding type sky sea dual-purpose unmanned aerial vehicle, includes the unmanned aerial vehicle body, the bottom surface fixedly connected with connecting seat of unmanned aerial vehicle body, T type spout has been seted up to the bottom surface of connecting seat, the inner wall slip joint of T type spout has T type slider, the bottom surface fixedly connected with floating plate of T type slider, the rotation groove has been seted up to the bottom surface of floating plate, the inner wall rotation in rotation groove is connected with the backup pad, the non-slip mat of bottom surface fixedly connected with of backup pad, the spout has been seted up to the bottom surface of floating plate, the inner wall fixedly connected with slide bar one of spout, the outer wall sliding connection of slide bar has the slider, the outer wall swing joint of spout has the spring two, the one end and the inner wall fixed connection of spout of spring two, the other end and the side fixed connection of slider of spring, the bottom surface of slider articulates there is the connecting rod, the other end of connecting rod is articulated with the top surface of backup pad.
Adopt above-mentioned technical scheme, in this scheme, can make the unmanned aerial vehicle body float at sea through the floating plate, played skid-proof effect when descending the unmanned aerial vehicle body through the slipmat, take place deformation through extrusion spring two and produce reverse force and played good cushioning effect to the unmanned aerial vehicle body.
The technical scheme of the utility model is further improved as follows: the side of T type slider has seted up movable groove, the inner wall fixedly connected with slide bar two of movable groove, the outer wall sliding symmetry of slide bar two is connected with the push pedal.
By adopting the technical scheme, the T-shaped sliding block is convenient to install and detach through the push plate.
The technical scheme of the utility model is further improved as follows: the outer wall of the second sliding rod is movably connected with a first spring, and the first spring is positioned between the pushing plates.
By adopting the technical scheme, the installation between the pushing plates is more stable through the thrust of the first spring.
The technical scheme of the utility model is further improved as follows: the side fixedly connected with draw-in lever of push pedal, the draw-in groove has been seted up to the inner wall of T type spout, the inner wall joint of one end and draw-in groove of draw-in lever.
By adopting the technical scheme, the clamping rod is clamped into the clamping groove in the scheme, so that the T-shaped sliding block is conveniently installed.
The technical scheme of the utility model is further improved as follows: the outer wall of unmanned aerial vehicle body has been seted up and has been accomodate the groove, the inner wall of accomodating the groove rotates and is connected with fastening bolt, fastening bolt's top runs through the inner wall of accomodating the groove and extends to outside, fastening bolt's outer wall swing joint has the main wing.
Adopt above-mentioned technical scheme, be convenient for accomodate the main wing through accomodating the groove in this scheme, reduce the accommodation space to the unmanned aerial vehicle body, it is convenient to fix the main wing through fastening bolt.
The technical scheme of the utility model is further improved as follows: the inner wall sliding connection of main wing has the aileron, the slot has been seted up to the top surface of main wing, the inner wall activity of slot has been inserted and has been equipped with the inserted bar, the bottom of inserted bar runs through the top surface of aileron and extends to the inner wall of main wing.
Adopt above-mentioned technical scheme, slide in the main wing through the aileron in this scheme, made things convenient for folding accomodating to the unmanned aerial vehicle body, fixed the aileron in inserting the slot through inserting the inserted bar.
By adopting the technical scheme, compared with the prior art, the utility model has the following technical progress:
1. the utility model provides a folding type air-sea dual-purpose unmanned aerial vehicle, which is characterized in that a supporting plate is contacted with the ground to be bent to a certain angle under the action of pressure, a connecting rod is driven to push a sliding block to slide on a sliding rod I through the bending of the supporting plate, a spring II is extruded through the sliding block sliding, and the extrusion spring II deforms to generate reverse force, so that a good damping effect is achieved on the unmanned aerial vehicle body, the damage of electronic elements in the unmanned aerial vehicle is avoided, and the service life of the unmanned aerial vehicle is influenced.
2. The utility model provides a folding type air-sea dual-purpose unmanned aerial vehicle, which is characterized in that an aileron is slid into a main wing by pulling out a plug rod, then the plug rod is inserted into a slot, then the main wing is loosened in a storage groove by rotating a fastening bolt, and then the main wing is rotated into the storage groove, so that the unmanned aerial vehicle body is conveniently stored when not in use, and the occupied space is reduced when the unmanned aerial vehicle body is stored and placed.
Drawings
FIG. 1 is a schematic diagram of the overall structure of the present utility model;
FIG. 2 is a schematic cross-sectional view of a floating plate according to the present utility model;
FIG. 3 is a schematic cross-sectional view of a connector according to the present utility model;
fig. 4 is a schematic view of the main airfoil section structure of the present utility model.
In the figure: 1. an unmanned aerial vehicle body; 11. a storage groove; 12. a fastening bolt; 13. a connecting seat; 131. a T-shaped chute; 132. a clamping groove; 2. a main wing; 21. aileron; 22. a slot; 23. a rod; 3. a floating plate; 31. a T-shaped slider; 311. a movable groove; 312. a second slide bar; 313. a push plate; 314. a first spring; 315. a clamping rod; 32. a rotating groove; 33. a chute; 34. a first slide bar; 35. a slide block; 36. a second spring; 37. a connecting rod; 4. a support plate; 41. an anti-slip mat.
Detailed Description
The utility model is further illustrated by the following examples:
example 1
As shown in fig. 1-4, the utility model provides a folding type air-sea dual-purpose unmanned aerial vehicle, which comprises an unmanned aerial vehicle body 1, wherein the bottom surface of the unmanned aerial vehicle body 1 is fixedly connected with a connecting seat 13, the bottom surface of the connecting seat 13 is provided with a T-shaped sliding groove 131, the inner wall of the T-shaped sliding groove 131 is in sliding clamping connection with a T-shaped sliding block 31, the bottom surface of the T-shaped sliding block 31 is fixedly connected with a floating plate 3, the bottom surface of the floating plate 3 is provided with a rotating groove 32, the inner wall of the rotating groove 32 is rotatably connected with a supporting plate 4, the bottom surface of the supporting plate 4 is fixedly connected with a non-slip mat 41, the bottom surface of the floating plate 3 is provided with a sliding groove 33, the inner wall of the sliding groove 33 is fixedly connected with a sliding rod one 34, the outer wall of the sliding rod one 34 is in sliding connection with a sliding block 35, one end of the sliding groove 33 is fixedly connected with a second spring 36, the other end of the second spring 36 is fixedly connected with the side surface of the sliding block 35, the bottom surface of the sliding block 35 is hinged with a connecting rod 37, and the other end of the connecting rod 37 is hinged with the top surface of the supporting plate 4.
In this embodiment, the supporting plate 4 is bent to a certain angle under the action of pressure, the connecting rod 37 is driven to push the sliding block 35 to slide on the sliding rod one 34 through the bending of the supporting plate 4, the second spring 36 is extruded through the sliding block 35, the second spring 36 is deformed to generate reverse force, so that a good damping effect is achieved on the unmanned aerial vehicle body 1, and the unmanned aerial vehicle body 1 can float on the sea through the floating plate.
Example 2
As shown in fig. 1-4, on the basis of embodiment 1, the present utility model provides a technical solution: preferably, the side of the T-shaped sliding block 31 is provided with a movable groove 311, the inner wall of the movable groove 311 is fixedly connected with a second slide bar 312, the outer wall of the second slide bar 312 is in sliding symmetry connection with a push plate 313, the outer wall of the second slide bar 312 is movably connected with a first spring 314, the first spring 314 is positioned between the push plates 313, the side of the push plate 313 is fixedly connected with a clamping rod 315, the inner wall of the T-shaped sliding groove 131 is provided with a clamping groove 132, and one end of the clamping rod 315 is in clamping connection with the inner wall of the clamping groove 132.
In this embodiment, the push plate 313 is pushed to slide in the movable slot 311 to approach to each other, so as to drive the clamping rod 315 to separate from the clamping slot 132, and further, the floating plate 3 can be taken down from the bottom surface of the unmanned aerial vehicle body 1, thereby facilitating the later disassembly and maintenance of the support plate 4.
Example 3
As shown in fig. 1-4, on the basis of embodiment 1, the present utility model provides a technical solution: preferably, the outer wall of unmanned aerial vehicle body 1 has been seted up and has been accomodate groove 11, the inner wall rotation of accomodating groove 11 is connected with fastening bolt 12, the inner wall of accomodating groove 11 is run through on fastening bolt 12 is extended to outside, fastening bolt 12's outer wall swing joint has main wing 2, the inner wall sliding connection of main wing 2 has aileron 21, slot 22 has been seted up to the top surface of main wing 2, slot 22's inner wall activity has been inserted and has been inserted bar 23, the bottom of bar 23 runs through the top surface of aileron 21 and extends to the inner wall of main wing 2.
In this embodiment, through pulling out the inserted bar 23, will aileron 21 to main wing 2 internal sliding, then insert slot 22 with inserted bar 23 in, rethread rotates fastening bolt 12 and makes main wing 2 become flexible in accomodating groove 11, and then rotates main wing 2 into accomodating inslot 11 to be convenient for accomodate unmanned aerial vehicle body 1 when not using, make when accomodating the occupation that has reduced the space when placing.
The working principle of the folding type unmanned aerial vehicle for the air and the sea is specifically described below.
As shown in fig. 1 to 4, when the unmanned aerial vehicle body 1 falls, the supporting plate 4 is contacted with the ground to be bent to a certain angle under the action of pressure, the connecting rod 37 is driven to push the sliding block 35 to slide on the sliding rod one 34 through the bending of the supporting plate 4, the second spring 36 is extruded through the sliding block 35 in a sliding manner, the second spring 36 is extruded to generate a reverse force to play a good damping role on the unmanned aerial vehicle body 1, when the unmanned aerial vehicle body 1 needs to be stored, the aileron 21 is slid towards the main wing 2 through pulling out the inserting rod 23, then the inserting rod 23 is inserted into the slot 22, the main wing 2 is loosened in the storage slot 11 through the rotation of the fastening bolt 12, and then the main wing 2 is rotated into the storage slot 11, so that the unmanned aerial vehicle body 1 is convenient to store when not in use, and the space occupation is reduced when the unmanned aerial vehicle body 1 is stored.
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 (6)
1. The utility model provides a folding empty dual-purpose unmanned aerial vehicle in sea, includes unmanned aerial vehicle body (1), its characterized in that: the utility model provides a unmanned aerial vehicle body (1) bottom surface fixedly connected with connecting seat (13), T type spout (131) have been seted up to the bottom surface of connecting seat (13), the inner wall sliding joint of T type spout (131) has T type slider (31), the bottom surface fixedly connected with of T type slider (31) floats board (3), rotation groove (32) have been seted up to the bottom surface of floating board (3), the inner wall rotation of rotation groove (32) is connected with backup pad (4), the bottom surface fixedly connected with slipmat (41) of backup pad (4), spout (33) have been seted up to the bottom surface of floating board (3), the inner wall fixedly connected with slide bar (34) of slide bar (33), the outer wall swing joint of slide bar (33) has spring two (36), the one end of spring two (36) and the inner wall fixedly connected with of spout (33), the other end of spring two (36) and the side fixedly connected with of slide bar (35), the bottom surface of slider (3) has been seted up spout (33), the outer end fixedly connected with slide bar (34) of slide bar (34), the top surface of slide bar (37).
2. The folding air-sea dual-purpose unmanned aerial vehicle according to claim 1, wherein: the side of T type slider (31) has seted up movable slot (311), the inner wall fixedly connected with slide bar two (312) of movable slot (311), the outer wall slip symmetry of slide bar two (312) is connected with push pedal (313).
3. The folding air-sea dual-purpose unmanned aerial vehicle according to claim 2, wherein: the outer wall of the second sliding rod (312) is movably connected with a first spring (314), and the first spring (314) is positioned between the pushing plates (313).
4. The folding air-sea dual-purpose unmanned aerial vehicle according to claim 2, wherein: the side of push pedal (313) fixedly connected with draw-in lever (315), draw-in groove (132) have been seted up to the inner wall of T type spout (131), the inner wall joint of draw-in lever (315) one end and draw-in groove (132).
5. The folding air-sea dual-purpose unmanned aerial vehicle according to claim 1, wherein: the unmanned aerial vehicle comprises an unmanned aerial vehicle body (1), wherein a storage groove (11) is formed in the outer wall of the unmanned aerial vehicle body (1), a fastening bolt (12) is rotatably connected to the inner wall of the storage groove (11), the top end of the fastening bolt (12) penetrates through the inner wall of the storage groove (11) to extend to the outside, and a main wing (2) is movably connected to the outer wall of the fastening bolt (12).
6. The folding air-sea dual-purpose unmanned aerial vehicle according to claim 5, wherein: the inner wall sliding connection of main wing (2) has aileron (21), slot (22) have been seted up to the top surface of main wing (2), the inner wall activity of slot (22) is inserted and is equipped with inserted bar (23), the bottom of inserted bar (23) runs through the top surface of aileron (21) and extends to the inner wall of main wing (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321780407.1U CN220263128U (en) | 2023-07-07 | 2023-07-07 | Folding type air-sea dual-purpose unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321780407.1U CN220263128U (en) | 2023-07-07 | 2023-07-07 | Folding type air-sea dual-purpose unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220263128U true CN220263128U (en) | 2023-12-29 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321780407.1U Active CN220263128U (en) | 2023-07-07 | 2023-07-07 | Folding type air-sea dual-purpose unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220263128U (en) |
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2023
- 2023-07-07 CN CN202321780407.1U patent/CN220263128U/en active Active
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