CN216805806U - Unmanned aerial vehicle with spherical insulating anti-collision device - Google Patents
Unmanned aerial vehicle with spherical insulating anti-collision device Download PDFInfo
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- CN216805806U CN216805806U CN202121031432.0U CN202121031432U CN216805806U CN 216805806 U CN216805806 U CN 216805806U CN 202121031432 U CN202121031432 U CN 202121031432U CN 216805806 U CN216805806 U CN 216805806U
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Abstract
The utility model discloses an unmanned aerial vehicle additionally provided with a spherical insulating anti-collision device, which comprises an unmanned aerial vehicle main body, propeller wings and supporting legs, wherein the propeller wings are arranged at four corners of the unmanned aerial vehicle main body, the supporting legs are arranged at the bottom of the unmanned aerial vehicle main body, spherical anti-collision mechanisms are arranged on two sides of the bottom of the supporting legs, each spherical anti-collision mechanism consists of an anti-collision ball, a first screw hole, a first supporting rod, a first anchor ear, a second screw hole, a second supporting rod and a second anchor ear, and a protective ring mechanism is arranged on the outer wall surface of each propeller wing, thereby improving the protection safety of the propeller wing.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicle equipment, in particular to an unmanned aerial vehicle with a spherical insulating anti-collision device.
Background
An unmanned aerial vehicle, abbreviated as "unmanned aerial vehicle" ("UAV"), is an unmanned aerial vehicle that is operated using a radio remote control device and a self-contained program control device. Unmanned aerial vehicles are in fact a general term for unmanned aerial vehicles, and can be defined from a technical perspective as follows: an unmanned fixed wing airplane, an unmanned vertical take-off and landing airplane [3], an unmanned airship, an unmanned helicopter, an unmanned multi-rotor aircraft, an unmanned paravane and the like. Compared with manned aircraft, it has the advantages of small volume, low cost, convenient use, low requirement on the operation environment, strong battlefield viability and the like.
However, the existing unmanned aerial vehicle has the following disadvantages:
current unmanned aerial vehicle is when using, because the crashworthiness of self to lead to damaging when unmanned aerial vehicle meets accident and drops easily, increaseed later stage unmanned aerial vehicle's maintenance cost, and then inconvenient user uses unmanned aerial vehicle.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide an unmanned aerial vehicle additionally provided with a spherical insulating anti-collision device, and aims to solve the problems that when the existing unmanned aerial vehicle in the background art is used, the existing unmanned aerial vehicle is easy to damage when the unmanned aerial vehicle accidentally drops due to insufficient anti-collision performance, the maintenance cost of the unmanned aerial vehicle in the later period is increased, and further, the unmanned aerial vehicle is inconvenient for a user to use.
In order to achieve the purpose, the utility model provides the following technical scheme: an unmanned aerial vehicle with an additional spherical insulating anti-collision device comprises an unmanned aerial vehicle main body, propeller wings and supporting legs, wherein the propeller wings are arranged at four corners of the unmanned aerial vehicle main body, the supporting legs are arranged at the bottom of the unmanned aerial vehicle main body, spherical anti-collision mechanisms are respectively arranged at two sides of the bottom of each supporting leg, each spherical anti-collision mechanism consists of an anti-collision ball, a first screw hole, a first supporting rod, a first hoop, a second screw hole, a second supporting rod and a second hoop, a protective ring mechanism is arranged on the surface of the outer wall of the propeller wing, each protective ring mechanism is formed by compounding a rubber plastic layer, a pearl cotton layer and an adhesive layer, the anti-collision balls can be installed and fixed on the unmanned aerial vehicle main body through the mutual cooperation of the screw holes, the supporting rods and the hoops in the spherical anti-collision mechanisms, so that when the unmanned aerial vehicle falls, a high-efficiency protective effect is achieved, the anti-collision performance is improved, and the damage to the unmanned aerial vehicle is reduced, through guard ring mechanism, can play dual buffering shock-absorbing function, and then improved the protection safety of propeller wing.
Preferably, first screw has been seted up at crashproof ball top, first screw surface is equipped with first branch, first staple bolt is installed to first branch top to can install first branch on crashproof ball through first screw, then through first staple bolt, can fix on the supporting leg again to first branch, and then can play the effect fixed to crashproof ball.
Preferably, first screw internal diameter size links to each other with first strut external diameter size, and first strut rotates with first screw and links to each other to can make things convenient for the staff later stage to first strut dismouting, improve the convenience that first strut used.
Preferably, the second screw has been seted up at crashproof ball inside wall middle part, second screw surface is equipped with second branch, the second staple bolt is installed to second branch bottom to can install second branch on crashproof ball through the second screw, then through the second staple bolt, can fix on the supporting leg to second branch again, and then can play the dual fixed effect of crashproof ball, strengthened crashproof ball's fixed effect.
Preferably, second screw internal diameter size links to each other with second branch external diameter size, and second branch rotates with the second screw and links to each other to can make things convenient for the staff to second branch dismouting through the second screw, improve the convenience that second branch later stage was changed.
Preferably, the top surface of the rubber plastic layer is provided with the pearl cotton layer, the top surface of the pearl cotton layer is coated with the viscose layer, so that the double-buffering and shock-absorbing functions can be achieved through the rubber plastic layer and the pearl cotton layer, the protection safety of the propeller wing is further improved, the damage to the propeller wing is reduced, the protection ring mechanism can be bonded on the propeller wing through the viscose layer, and the use convenience of the protection ring mechanism is further improved.
The utility model provides an unmanned aerial vehicle additionally provided with a spherical insulating anti-collision device, which has the following beneficial effects:
(1) according to the utility model, the unmanned aerial vehicle main body can be driven to lift off through the four groups of propeller wings, meanwhile, the support legs can also play a role in supporting the unmanned aerial vehicle main body, so that the unmanned aerial vehicle is convenient to use, the spherical anti-collision mechanisms are respectively arranged on two sides of the bottom of each support leg, and the first support rods can be arranged on the anti-collision balls through the first screw holes in the spherical anti-collision mechanisms, and then can be fixed on the support legs through the first anchor ears, so that the anti-collision balls can be fixed.
(2) According to the anti-collision device, the second support rod can be arranged on the anti-collision ball through the second screw hole, then the second support rod can be fixed on the supporting leg through the second hoop, so that the double fixing effect on the anti-collision ball can be achieved, the fixing effect of the anti-collision ball is enhanced, the inner diameter of the second screw hole is connected with the outer diameter of the second support rod, the second support rod is rotatably connected with the second screw hole, and therefore workers can conveniently assemble and disassemble the second support rod through the second screw hole, the convenience for later replacement of the second support rod is improved, the anti-collision ball can achieve a high-efficiency protection effect when the unmanned aerial vehicle falls, the anti-collision performance is improved, and the damage to the unmanned aerial vehicle is reduced.
(3) According to the utility model, the protective ring mechanism is arranged on the outer wall surface of the propeller wing, and the rubber plastic layer and the pearl wool layer in the protective ring mechanism can play a role in double buffering and damping, so that the protection safety of the propeller wing is improved, the damage of the propeller wing is reduced, the protective ring mechanism can be bonded on the propeller wing through the adhesive layer, and the use convenience of the protective ring mechanism is further improved.
Drawings
FIG. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is a schematic view of the bottom structure of the support leg of the present invention;
FIG. 3 is a schematic view of a portion A of the present invention;
FIG. 4 is a schematic view of the propeller wing configuration of the present invention;
FIG. 5 is a schematic cross-sectional view of a guard ring mechanism according to the present invention.
In the figure: 1. an unmanned aerial vehicle main body; 2. a propeller wing; 3. supporting legs; 4. a spherical anti-collision mechanism; 5. an anti-collision ball; 6. a first screw hole; 7. a first strut; 8. a first hoop; 9. a second screw hole; 10. a second support bar; 11. a second hoop; 12. a guard ring mechanism; 13. a rubber-plastic layer; 14. a pearl cotton layer; 15. and (6) gluing the layers.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention.
As shown in fig. 1 to 5, the present invention provides a technical solution: an unmanned aerial vehicle provided with a spherical insulating anti-collision device comprises an unmanned aerial vehicle main body 1, propeller wings 2 and supporting legs 3, wherein the propeller wings 2 are arranged at four corners of the unmanned aerial vehicle main body 1, the supporting legs 3 are arranged at the bottom of the unmanned aerial vehicle main body 1, spherical anti-collision mechanisms 4 are arranged at two sides of the bottom of each supporting leg 3, each spherical anti-collision mechanism 4 is composed of an anti-collision ball 5, a first screw hole 6, a first supporting rod 7, a first hoop 8, a second screw hole 9, a second supporting rod 10 and a second hoop 11, a protective ring mechanism 12 is arranged on the outer wall surface of each propeller wing 2, each protective ring mechanism 12 is formed by compounding a rubber plastic layer 13, a pearl cotton layer 14 and an adhesive layer 15, the anti-collision balls 5 can be installed and fixed on the unmanned aerial vehicle main body 1 through the mutual cooperation of the screw holes, the supporting rods and the hoops in the spherical anti-collision mechanisms 4, and further can play a high-efficiency protection effect when the unmanned aerial vehicle falls, and then improved crashproof performance, reduced unmanned aerial vehicle's damage, through guard ring mechanism 12, can play double buffering shock-absorbing function, and then improved propeller wing 2's protection safety.
6 internal diameter sizes of first screw link to each other with 7 external diameter sizes of first bracing piece, and first bracing piece 7 rotates with first screw 6 and links to each other to can make things convenient for the staff later stage to 7 dismouting of first bracing piece, improve the convenience that 7 uses of first bracing piece.
The size of the inner diameter of the second screw hole 9 is connected with the size of the outer diameter of the second supporting rod 10, and the second supporting rod 10 is connected with the second screw hole 9 in a rotating mode, so that the second supporting rod 10 can be conveniently dismounted and mounted by workers through the second screw hole 9, and convenience in later-stage replacement of the second supporting rod 10 is improved.
The top surface of the rubber layer 13 is provided with the pearl wool layer 14, the top surface of the pearl wool layer 14 is coated with the adhesive layer 15, so that the double-buffering and shock-absorbing functions can be achieved through the rubber layer 13 and the pearl wool layer 14, the protection safety of the propeller wing 2 is improved, the damage to the propeller wing 2 is reduced, the protection ring mechanism 12 can be bonded on the propeller wing 2 through the adhesive layer 15, and the use convenience of the protection ring mechanism 12 is improved.
It should be noted that, an unmanned aerial vehicle with a spherical insulating anti-collision device is characterized in that, when in operation, the propeller wings 2 are arranged at four corners of the main body 1 of the unmanned aerial vehicle, and the bottom of the main body 1 of the unmanned aerial vehicle is provided with the supporting legs 3, so that the four groups of propeller wings 2 can drive the main body 1 of the unmanned aerial vehicle to lift off, and the supporting legs 3 can also play a role of supporting the main body 1 of the unmanned aerial vehicle, so that the unmanned aerial vehicle can be conveniently used, the spherical anti-collision mechanisms 4 are arranged at two sides of the bottom of the supporting legs 3, and each spherical anti-collision mechanism 4 is composed of an anti-collision ball 5, a first screw hole 6, a first supporting rod 7, a first hoop 8, a second screw hole 9, a second supporting rod 10 and a second hoop 11, the top of the anti-collision ball 5 is provided with the first screw hole 6, the surface of the first screw hole 6 is provided with the first supporting rod 7, and the top end of the first supporting rod 7 is provided with the first hoop 8, so that the first supporting rod 7 can be arranged on the anti-collision ball 5 through the first screw hole 6, then the first support rod 7 can be fixed on the supporting leg 3 through the first hoop 8, and further the fixing effect of the anti-collision ball 5 can be achieved, because the inner diameter of the first screw hole 6 is connected with the outer diameter of the first support rod 7, and the first support rod 7 is rotatably connected with the first screw hole 6, so that the first support rod 7 can be conveniently disassembled and assembled by workers in the later period, the convenience of the use of the first support rod 7 is improved, the second screw hole 9 is arranged in the middle of the inner side wall of the anti-collision ball 5, the surface of the second screw hole 9 is provided with the second support rod 10, and the bottom end of the second support rod 10 is provided with the second hoop 11, so that the second support rod 10 can be arranged on the anti-collision ball 5 through the second screw hole 9, and then the second support rod 10 can be fixed on the supporting leg 3 through the second hoop 11, and further the double fixing effect of the anti-collision ball 5 can be achieved, and the fixing effect of the anti-collision ball 5 is enhanced, because the inner diameter of the second screw hole 9 is connected with the outer diameter of the second supporting rod 10, and the second supporting rod 10 is rotatably connected with the second screw hole 9, the second supporting rod 10 can be conveniently assembled and disassembled by workers through the second screw hole 9, the convenience of later replacement of the second supporting rod 10 is improved, the anti-collision ball 5 can play a role in high-efficiency protection when the unmanned aerial vehicle falls, the anti-collision performance is improved, the damage of the unmanned aerial vehicle is reduced, the protective ring mechanism 12 is arranged on the outer wall surface of the propeller wing 2 and is formed by compounding a rubber plastic layer 13, a pearl cotton layer 14 and an adhesive layer 15, the pearl cotton layer 14 is arranged on the top surface of the rubber plastic layer 13, the adhesive layer 15 is coated on the top surface of the pearl cotton layer 14, and therefore, the double buffering and shock absorption functions can be achieved through the rubber plastic layer 13 and the pearl cotton layer 14, and the safety protection of the propeller wing 2 is improved, the damage of propeller wing 2 is reduced, and protective ring mechanism 12 can be bonded on propeller wing 2 through adhesive layer 15, so that the convenience of use of protective ring mechanism 12 is improved.
The unmanned aerial vehicle comprises an unmanned aerial vehicle main body 1, propeller wings 2, supporting legs 3, a spherical anti-collision mechanism 4, anti-collision balls 5, first screw holes 6, first supporting rods 7, a first hoop 8, second screw holes 9, second supporting rods 10, a second hoop 11, a protective ring mechanism 12, an elastic plastic layer 13, a pearl cotton layer 14 and an adhesive layer 15, wherein the components are all universal standard components or components known by technicians in the field, the structure and the principle of the components can be known by technicians in the field through technical manuals or conventional experimental methods, normal operation of all devices is guaranteed, and excessive limiting requirements are not required.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments 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 an install spherical insulating buffer stop's unmanned aerial vehicle additional, includes unmanned aerial vehicle main part (1), propeller wing (2) and supporting leg (3), propeller wing (2) set up in unmanned aerial vehicle main part (1) four corners, supporting leg (3), its characterized in that are installed to unmanned aerial vehicle main part (1) bottom: spherical anticollision institution (4) are all installed to supporting leg (3) bottom both sides, spherical anticollision institution (4) comprise anticollision ball (5), first screw (6), first branch (7), first staple bolt (8), second screw (9), second branch (10) and second staple bolt (11), propeller wing (2) outer wall surface is equipped with guard ring mechanism (12), guard ring mechanism (12) are formed by rubber plastic layer (13), the cotton layer of pearl (14) and viscose layer (15) complex.
2. The unmanned aerial vehicle with the spherical insulating anti-collision device as claimed in claim 1, wherein: first screw (6) have been seted up at anti-collision ball (5) top, first screw (6) surface is equipped with first branch (7), first staple bolt (8) are installed on first branch (7) top.
3. The unmanned aerial vehicle with the spherical insulating anti-collision device as claimed in claim 1, wherein the unmanned aerial vehicle comprises: the inner diameter of the first screw hole (6) is connected with the outer diameter of the first supporting rod (7), and the first supporting rod (7) is rotatably connected with the first screw hole (6).
4. The unmanned aerial vehicle with the spherical insulating anti-collision device as claimed in claim 1, wherein the unmanned aerial vehicle comprises: a second screw hole (9) is formed in the middle of the inner side wall of the anti-collision ball (5), a second supporting rod (10) is arranged on the surface of the second screw hole (9), and a second hoop (11) is installed at the bottom end of the second supporting rod (10).
5. The unmanned aerial vehicle with the spherical insulating anti-collision device as claimed in claim 1, wherein: the inner diameter of the second screw hole (9) is connected with the outer diameter of the second supporting rod (10), and the second supporting rod (10) is rotatably connected with the second screw hole (9).
6. The unmanned aerial vehicle with the spherical insulating anti-collision device as claimed in claim 1, wherein: the top surface of the rubber layer (13) is provided with a pearl cotton layer (14), and the top surface of the pearl cotton layer (14) is coated with an adhesive layer (15).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121031432.0U CN216805806U (en) | 2021-05-14 | 2021-05-14 | Unmanned aerial vehicle with spherical insulating anti-collision device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121031432.0U CN216805806U (en) | 2021-05-14 | 2021-05-14 | Unmanned aerial vehicle with spherical insulating anti-collision device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216805806U true CN216805806U (en) | 2022-06-24 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121031432.0U Active CN216805806U (en) | 2021-05-14 | 2021-05-14 | Unmanned aerial vehicle with spherical insulating anti-collision device |
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| Country | Link |
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| CN (1) | CN216805806U (en) |
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2021
- 2021-05-14 CN CN202121031432.0U patent/CN216805806U/en active Active
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