CN211223863U - Unmanned aerial vehicle rotor structure convenient to dismouting and regulation - Google Patents
Unmanned aerial vehicle rotor structure convenient to dismouting and regulation Download PDFInfo
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- CN211223863U CN211223863U CN201922473277.7U CN201922473277U CN211223863U CN 211223863 U CN211223863 U CN 211223863U CN 201922473277 U CN201922473277 U CN 201922473277U CN 211223863 U CN211223863 U CN 211223863U
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Abstract
The utility model discloses an unmanned aerial vehicle rotor structure convenient to dismouting and regulation, including the unmanned aerial vehicle body, the unmanned aerial vehicle body is inside including the organism, and organism outside fixed connection has a wing pole, wing pole outside fixedly connected with motor, and motor output end fixedly connected with output shaft, the connection can be dismantled to the output shaft upper end has a wing installation piece, and the wing installation piece outside is fixed with the screw body, the screw body is inside including cup jointing the pole, and cup joint the inside movable groove that has seted up of pole, the inside swing joint of movable groove has the movable rod, and the inside location screw of having seted up of movable rod, cup joint the pole outside and can dismantle and be connected with set screw. This unmanned aerial vehicle rotor structure convenient to dismouting and regulation carries out the block through spring catch button and block groove to make things convenient for whole installation, increased holistic practicality, and make things convenient for the rotor to drive whole rising, increased holistic practicality.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle rotor structure convenient to dismouting and regulation.
Background
The unmanned plane is called unmanned plane for short, and is an unmanned plane operated by radio remote control equipment and a self-contained program control device. The unmanned aerial vehicle is not provided with a cockpit, but is provided with an automatic pilot, a program control device and other equipment, and the application of the unmanned aerial vehicle is more and more extensive along with the development of the times.
But current unmanned aerial vehicle rotor structure wholly inconvenient dismantles to inconvenient whole dismantlement to the part of damage has reduced holistic flexibility, and current unmanned aerial vehicle rotor structure is inconvenient adjusts, thereby inconvenient whole length to the rotor is adjusted, has reduced whole practicality.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle rotor structure convenient to dismouting and regulation to propose current unmanned aerial vehicle rotor structure in solving above-mentioned background, whole inconvenient dismantlement, thereby inconvenient whole dismantles the part of damage, has reduced holistic flexibility, and current unmanned aerial vehicle rotor structure is inconvenient to be adjusted, thereby inconvenient whole length to the rotor is adjusted, has reduced the problem of whole practicality.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an unmanned aerial vehicle rotor structure convenient to dismouting and regulation, includes the unmanned aerial vehicle body, the unmanned aerial vehicle body is inside including the organism, and organism outside fixed connection has a wing pole, wing pole outside fixed connection has the motor, and motor output end fixed connection has the output shaft, the output shaft upper end can be dismantled and be connected with the wing installation piece, and the wing installation piece outside is fixed with the screw body, the screw body is inside including cup jointing the pole, and cup joint the inside movable groove that has seted up of pole, the inside swing joint of movable groove has the movable rod, and the inside location screw that has seted up of movable rod, cup joint the pole outside and can dismantle and be connected with set screw, and set screw passes and cup joint the pole outside and the mutual block of location screw.
Preferably, the output shaft is internally provided with a mounting groove, the mounting groove is internally and fixedly connected with a spring body, the outer side of the spring body is fixedly connected with a spring clamping button, and the spring clamping button is movably connected with the mounting groove through the spring body.
Preferably, an insertion groove is formed in the wing installation block, a clamping groove is arranged on the outer side of the wing installation block in a clamping mode, the clamping groove is communicated with the inside of the insertion groove, the clamping groove is matched with the spring clamping button in shape and size, and the insertion groove is matched with the output shaft in shape and size.
Preferably, the movable rod is matched with the movable groove in shape and size, and a positioning screw hole in the movable rod is matched with a positioning screw in shape and size.
Preferably, the positioning screw holes are distributed in the movable rod at equal intervals, and four groups of the movable rod and the sleeve rod are distributed outside the wing installation block at equal intervals.
Preferably, the four clamping grooves are annularly distributed at equal intervals around the circular axis of the output shaft, and the four clamping grooves are distributed corresponding to the spring clamping buttons.
Compared with the prior art, the beneficial effects of the utility model are that:
1. according to the unmanned aerial vehicle rotor wing structure convenient to disassemble, assemble and adjust, the rotor wing is conveniently and integrally replaced by clamping the wing installation block and the output shaft, the overall flexibility is improved, and the spring clamping button is clamped with the clamping groove, so that the unmanned aerial vehicle rotor wing structure is convenient to integrally install, and the overall practicability is improved;
2. according to the unmanned aerial vehicle rotor wing structure convenient to disassemble, assemble and adjust, the movable rod is used for moving in the movable groove, so that the length of the rotor wing can be adjusted conveniently integrally, the whole body can be conveniently jumped according to the terrain, the flexibility of the whole body is improved, the rotor wing can conveniently drive the whole body to ascend, and the practicability of the whole body is improved;
3. this unmanned aerial vehicle rotor structure convenient to dismouting and regulation through the mutual block in spring catch button and the block groove that uses four equidistant distributions, has increased the stability of integral erection, and whole easy to assemble and regulation, and convenient whole changes damage part to holistic practicality has been guaranteed.
Drawings
FIG. 1 is a schematic perspective view of the present invention;
fig. 2 is a schematic perspective view of the wing installation block of the present invention;
fig. 3 is a schematic view of a disassembled structure of the wing mounting block of the present invention;
fig. 4 is the schematic view of the split structure of the movable rod of the present invention.
In the figure: 1. an unmanned aerial vehicle body; 2. a body; 3. a wing rod; 4. a motor; 5. an output shaft; 6. a wing mounting block; 7. a propeller body; 8. a sleeved rod; 9. a movable groove; 10. a movable rod; 11. positioning the screw hole; 12. mounting grooves; 13. a spring body; 14. a spring snap button; 15. inserting grooves; 16. a clamping groove; 17. and (5) positioning the screw.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-4, the present invention provides a technical solution: the utility model provides an unmanned aerial vehicle rotor structure convenient to dismouting and regulation, including unmanned aerial vehicle body 1, 1 inside organism 2 that includes of unmanned aerial vehicle body, and 2 outside fixed connections of organism have wing pole 3, 3 outside fixed connection of wing pole has motor 4, and motor 4 output end fixed connection has output shaft 5, 5 upper ends of output shaft can be dismantled and be connected with wing installation piece 6, and 6 outside of wing installation piece are fixed with screw body 7, 7 inside including cup jointing the pole 8 of screw body, and cup joint 8 inside and seted up movable groove 9, the inside swing joint in movable groove 9 has movable rod 10, and movable rod 10 is inside has seted up location screw 11, cup joint 8 outside of pole and can dismantle and be connected with set screw 17, and set screw 17 passes the 8 outside of cup jointing pole and 11 mutual blocks in location screw.
Further, the inside mounting groove 12 of having seted up of output shaft 5, and the inside fixedly connected with spring body 13 of mounting groove 12, the fixedly connected with spring clip button 14 in the spring body 13 outside, and spring clip button 14 passes through spring body 13 and mounting groove 12 swing joint, and spring clip button 14 conveniently carries out the block with block groove 16 under spring body 13 drives to holistic block stability has been increased.
Furthermore, an inserting groove 15 is formed in the wing installation block 6, a clamping groove 16 is clamped on the outer side of the wing installation block 6, the clamping groove 16 is communicated with the inside of the inserting groove 15, the clamping groove 16 is matched with the spring clamping button 14 in shape and size, the inserting groove 15 is matched with the output shaft 5 in shape and size, and the clamping groove 16 is clamped with the spring clamping button 14 in amount, so that the stability of integral clamping is improved, and the integral take-off is guaranteed.
Furthermore, the movable rod 10 is matched with the movable groove 9 in shape and size, the positioning screw hole 11 in the movable rod 10 is matched with the positioning screw 17 in shape and size, and the movable rod 10 can be fixed by mutually clamping the positioning screw hole 11 and the positioning screw 17, so that the overall fixing stability is improved.
Furthermore, the positioning screw holes 11 are distributed in the movable rod 10 at equal intervals, four groups of movable rods 10 and the sleeve connecting rod 8 are distributed outside the wing installation block 6 at equal intervals, the movable rods 10 and the sleeve connecting rod 8 distributed at equal intervals are convenient to adjust the length of the wing integrally, and the overall practicability is improved.
Furthermore, four groups of clamping grooves 16 are annularly distributed on the circular center line of the output shaft 5 at equal intervals, and the clamping grooves 16 and the spring clamping buttons 14 are correspondingly distributed, so that the clamping is convenient to integrally carry out, the integral installation and the disassembly are convenient, and the integral practicability is improved.
The working principle is as follows: firstly, the spring clamping button 14 is pressed, the spring clamping button 14 is driven by the spring body 13 to move into the mounting groove 12, so that the output shaft 5 is conveniently inserted into the inserting groove 15 in the wing mounting block 6, when the spring clamping button 14 on the inner side of the output shaft 5 moves to the clamping groove 16 on the inner side of the wing mounting block 6, the spring body 13 drives the spring clamping button 14 to be clamped with the clamping groove 16, so that the wing mounting block 6 is fixed, so that the propeller body 7 is mounted, the whole installation and adjustment are convenient, then the movable rod 10 moves in the movable groove 9 in the sleeving rod 8 through the movable rod 10, so that the length of the propeller body 7 is adjusted, after the adjustment is finished, the movable rod 10 and the sleeving rod 8 are fixed through the positioning screw 17 passing through the outer side of the sleeving rod 8 and the positioning screw hole 11 in a mutual clamping manner, so that the damaged part can be conveniently replaced, the overall practicability is increased.
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 invention, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The utility model provides an unmanned aerial vehicle rotor structure convenient to dismouting and regulation, includes the unmanned aerial vehicle body, its characterized in that: the utility model discloses an unmanned aerial vehicle, including unmanned aerial vehicle body, and organism outside fixed connection has the wing pole, wing pole outside fixedly connected with motor, and motor output end fixedly connected with output shaft, the connection can be dismantled to the output shaft upper end has the wing installation piece, and is fixed with the screw body outside the wing installation piece, the screw body is inside including cup jointing the pole, and cup joints the inside movable groove of having seted up of pole, the inside swing joint of movable groove has the movable rod, and the inside location screw that has seted up of movable rod, cup joint the pole outside and can dismantle and be connected with set screw, and set screw passes and cup joints the pole outside and the mutual block of location screw.
2. The rotor structure of unmanned aerial vehicle convenient to dismouting and regulation of claim 1, characterized in that: the output shaft is internally provided with a mounting groove, the mounting groove is internally and fixedly connected with a spring body, the outer side of the spring body is fixedly connected with a spring clamping button, and the spring clamping button is movably connected with the mounting groove through the spring body.
3. The rotor structure of unmanned aerial vehicle convenient to dismouting and regulation of claim 2, characterized in that: the wing installation block is internally provided with an insertion groove, the outer side of the wing installation block is clamped with a clamping groove, the clamping groove is communicated with the inside of the insertion groove, the clamping groove is matched with the spring clamping button in shape and size, and the insertion groove is matched with the output shaft in shape and size.
4. The rotor structure of unmanned aerial vehicle convenient to dismouting and regulation of claim 1, characterized in that: the movable rod is matched with the movable groove in shape and size, and a positioning screw hole in the movable rod is matched with a positioning screw in shape and size.
5. The rotor structure of unmanned aerial vehicle convenient to dismouting and regulation of claim 1, characterized in that: the positioning screw holes are distributed in the movable rod at equal intervals, and four groups of movable rods and sleeve rods are distributed outside the wing installation block at equal intervals.
6. An unmanned aerial vehicle rotor structure convenient to dismouting and regulation according to claim 3, characterized in that: four groups of clamping grooves are annularly distributed at equal intervals around the circular axis of the output shaft, and the clamping grooves and the spring clamping buttons are correspondingly distributed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922473277.7U CN211223863U (en) | 2019-12-31 | 2019-12-31 | Unmanned aerial vehicle rotor structure convenient to dismouting and regulation |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922473277.7U CN211223863U (en) | 2019-12-31 | 2019-12-31 | Unmanned aerial vehicle rotor structure convenient to dismouting and regulation |
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| Publication Number | Publication Date |
|---|---|
| CN211223863U true CN211223863U (en) | 2020-08-11 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201922473277.7U Active CN211223863U (en) | 2019-12-31 | 2019-12-31 | Unmanned aerial vehicle rotor structure convenient to dismouting and regulation |
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| CN (1) | CN211223863U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112856338A (en) * | 2021-03-02 | 2021-05-28 | 金华创祥雷玩具有限公司 | Clapping lamp convenient to disassemble and assemble and processing method thereof |
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2019
- 2019-12-31 CN CN201922473277.7U patent/CN211223863U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112856338A (en) * | 2021-03-02 | 2021-05-28 | 金华创祥雷玩具有限公司 | Clapping lamp convenient to disassemble and assemble and processing method thereof |
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Effective date of registration: 20211227 Address after: Room 301-3, building A10, No. 9 Kechuang Avenue, intelligent manufacturing Industrial Park (Zhihe Park), Jiangbei new area, Nanjing, Jiangsu 210000 Patentee after: Jiangsu Shangdao Intelligent Technology Co.,Ltd. Address before: 243000 the 4 tier of intelligent equipment Industrial Park in Yushan Economic Development Zone, Ma'anshan, Anhui, 6. Patentee before: Anhui peace flies intelligent technology Ltd. |