CN214930561U - Unmanned aerial vehicle with multiple flight mode - Google Patents
Unmanned aerial vehicle with multiple flight mode Download PDFInfo
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- CN214930561U CN214930561U CN202121258156.1U CN202121258156U CN214930561U CN 214930561 U CN214930561 U CN 214930561U CN 202121258156 U CN202121258156 U CN 202121258156U CN 214930561 U CN214930561 U CN 214930561U
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- aerial vehicle
- unmanned aerial
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- connecting rod
- rod
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Abstract
The utility model belongs to an unmanned aerial vehicle with multiple flight pattern, including the unmanned aerial vehicle body, be provided with connection structure on the unmanned aerial vehicle body, connection structure, include: connecting rod, fixed part, paddle and pars contractilis, the connecting rod passes through the fixed part is connected the unmanned aerial vehicle body side surface, the paddle passes through the pars contractilis sets up on the connecting rod, the utility model discloses can fold to according to strong wind weather increase flabellum, strengthen power, the dismouting at any time, it is nimble convenient to use, is fit for multiple weather.
Description
Technical Field
The utility model belongs to the technical field of an unmanned aerial vehicle, especially, relate to an unmanned aerial vehicle with multiple flight mode.
Background
The unmanned plane is an unmanned plane which is operated by using 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, the fan blade part of the existing unmanned plane is distributed in four parts, is fixed in position and cannot be detached, and the situation of blockage is easy to occur in windy weather, so that the improvement is needed.
SUMMERY OF THE UTILITY MODEL
In order to achieve the purpose, the technical scheme adopted by the utility model is that the utility model provides an unmanned aerial vehicle with multiple flight modes, which comprises an unmanned aerial vehicle body, wherein the unmanned aerial vehicle body is provided with a connecting structure;
the connection structure includes: the connecting rod, the fixing part, the blades and the telescopic part;
the connecting rod passes through the fixed part is connected unmanned aerial vehicle body side surface, the paddle passes through the pars contractilis sets up on the connecting rod.
Preferably, the fixing portion includes: the fixing device comprises a fixing sleeve, a swinging block, a butt joint groove, a clamping hole, a spring ball, a slot, a fixing block, a round hole, a round rod, a movable sleeve and a spring;
the fixed cover sets up unmanned aerial vehicle body side surface, swing piece round pin axle rotates to be connected in the fixed cover, the butt joint groove is opened swing piece side end face, the card hole is opened the butt joint inslot side surface, the spring ball sets up in the connecting rod, the slot is opened fixed cover side end face, the fixed block sets up swing piece side end face, the round hole is opened fixed block side end face, round bar activity suit is in the round hole and one end cartridge are in the slot, movable sleeve activity suit is connected swing on the piece and with the round bar is connected, spring coupling be in the fixed block with between the movable sleeve.
Preferably, the telescopic part includes: the device comprises an elongated slot, an inner rod, a movable cavity, an inner thread block, a cavity, a side hole, a rotating block and a screw rod;
the long groove is formed in the end face of the side of the connecting rod, the inner rod is movably sleeved in the long groove, the movable cavity is formed in the end face of the side of the inner rod, the inner thread block is arranged in the movable cavity, the cavity is formed in the connecting rod, the side holes are formed in the opposite two side surfaces in the cavity, the rotating block is rotatably connected in the cavity, the screw penetrates through the inner side surface of the long groove and is connected to the rotating block, and one end of the screw is in threaded screwing connection with the inner thread block.
Preferably, the side surface of the turning block is of an anti-slip structure.
Preferably, the cross sections of the long groove and the inner rod are rectangular structures.
Compared with the prior art, the utility model discloses an advantage lies in with positive effect, can fold to according to strong wind weather increase flabellum, strengthen power, the dismouting at any time, and it is nimble convenient to use, is fit for multiple weather.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings required to be used in the description of the embodiments are briefly introduced below, and it is obvious that the drawings in the following description are some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without inventive labor.
Fig. 1 is a schematic structural diagram of an unmanned aerial vehicle with multiple flight modes according to this embodiment;
fig. 2 is a schematic structural diagram of a connecting rod portion of the unmanned aerial vehicle with multiple flight modes according to the present embodiment;
fig. 3 is a partially enlarged view of the fastening sleeve portion of the drone according to the present embodiment, with various flight modes;
in the above figures, 1, an unmanned aerial vehicle body; 2. a connecting rod; 3. a paddle; 4. fixing a sleeve; 5. a swing block; 6. a slot; 7. a clamping hole; 8. a spring bead; 9. a slot; 10. a fixed block; 11. a circular hole; 12. a round bar; 13. a movable sleeve; 14. a spring; 15. a long groove; 16. an inner rod; 17. a movable cavity; 18. an internal thread block; 19. a cavity; 20. a side hole; 21. rotating the block; 22. a screw.
Detailed Description
In order to make the above objects, features and advantages of the present invention more clearly understood, the present invention will be further described with reference to the accompanying drawings and examples. It should be noted that the embodiments and features of the embodiments of the present application may be combined with each other without conflict.
In the following description, numerous specific details are set forth in order to provide a thorough understanding of the present invention, however, the present invention may be practiced in other ways than those specifically described herein, and therefore the present invention is not limited to the limitations of the specific embodiments of the present disclosure.
In the embodiment, as can be seen from fig. 1-3 in the specification, the unmanned aerial vehicle comprises an unmanned aerial vehicle body 1, wherein a connecting structure is arranged on the unmanned aerial vehicle body 1;
the connection structure includes: a connecting rod 2, a fixing part, a blade 3 and a telescopic part;
the connecting rod 2 is connected to the side surface of the unmanned aerial vehicle body 1 through the fixing part, and the blades 3 are arranged on the connecting rod 2 through the telescopic parts;
the fixing portion includes: the fixing sleeve 4, the swinging block 5, the butt joint groove 6, the clamping hole 7, the spring 14 bead 8, the slot 9, the fixing block 10, the round hole 11, the round rod 12, the movable sleeve 13 and the spring 14;
the fixed sleeve 4 is arranged on the side surface of the unmanned aerial vehicle body 1, the swinging block 5 is rotationally connected in the fixed sleeve 4 through a pin shaft, the butt joint groove 6 is formed in the side end surface of the swinging block 5, the clamping hole 7 is formed in the inner side surface of the butt joint groove 6, the spring 14 bead 8 is arranged in the connecting rod 2, the slot 9 is formed in the side end surface of the fixed sleeve 4, the fixed block 10 is arranged on the side surface of the swinging block 5, the round hole 11 is formed in the side end surface of the fixed block 10, the round rod 12 is movably sleeved 13 in the round hole 11, one end of the round rod is inserted in the slot 9, the movable sleeve 13 of the movable sleeve 13 is connected to the swinging block 5 in a mounting manner and is connected with the round rod 12, and the spring 14 is connected between the fixed block 10 and the movable sleeve 13;
the expansion part includes: the structure comprises an elongated slot 15, an inner rod 16, a movable cavity 17, an internal thread block 18, a cavity 19, a side hole 20, a rotating block 21 and a screw 22;
the long groove 15 is arranged on the end surface of the side of the connecting rod 2, the movable sleeve 13 of the inner rod 16 is arranged in the long groove 15, the movable cavity 17 is arranged on the end surface of the side of the inner rod 16, the inner thread block 18 is arranged in the movable cavity 17, the cavity 19 is arranged in the connecting rod 2, the side holes 20 are arranged on the opposite side surfaces in the cavity 19, the rotating block 21 is rotatably connected in the cavity 19, the screw rod 22 penetrates through the inner side surface of the long groove 15 and is connected to the rotating block 21, and one end of the screw rod is in threaded connection with the inner thread block 18;
the side surface of the rotating block 21 is of an anti-slip structure, and the cross sections of the long groove 15 and the inner rod 16 are of rectangular structures.
When in specific use: firstly pulling the movable sleeve 13, then outwards rotating the swinging block 5, then loosening the movable sleeve 13 to enable the round rod 12 to be inserted into the slot 9, inserting one end of the connecting rod 2 into the butt joint slot 6 of the swinging block 5 and being connected with the clamping hole 7 in a matched mode through the bead 8 of the spring 14, selecting four or eight paddles 3 according to use requirements, and further enabling the inner rod 16 to be extended through the matching of the inner thread block 18 and the screw rod 22 by screwing the rotating block 21.
The above description is only a preferred embodiment of the present invention, and is not intended to limit the present invention in other forms, and any person skilled in the art may use the above-mentioned technical contents to change or modify the equivalent embodiment into equivalent changes and apply to other fields, but any simple modification, equivalent change and modification made to the above embodiments according to the technical matters of the present invention will still fall within the protection scope of the technical solution of the present invention.
Claims (5)
1. An unmanned aerial vehicle with multiple flight modes comprises an unmanned aerial vehicle body (1), and is characterized in that a connecting structure is arranged on the unmanned aerial vehicle body (1);
the connection structure includes: a connecting rod (2), a fixing part, a blade (3) and a telescopic part;
connecting rod (2) pass through the fixed part is connected unmanned aerial vehicle body (1) side surface, paddle (3) pass through the pars contractilis sets up on connecting rod (2).
2. A drone with multiple flight modes according to claim 1, characterised in that the fixed part comprises: the device comprises a fixed sleeve (4), a swinging block (5), a butt joint groove (6), a clamping hole (7), a spring (14), a bead (8), a slot (9), a fixed block (10), a round hole (11), a round rod (12), a movable sleeve (13) and a spring (14);
fixed cover (4) set up unmanned aerial vehicle body (1) side surface, swing piece (5) round pin axle rotates to be connected in fixed cover (4), open butt joint groove (6) swing piece (5) side end face, card hole (7) are opened butt joint groove (6) inboard surface, spring (14) pearl (8) set up in connecting rod (2), slot (9) are opened fixed cover (4) side end face, fixed block (10) set up swing piece (5) side surface, round hole (11) are opened fixed block (10) side end face, circle pole (12) movable sleeve (13) dress is in round hole (11) and one end cartridge are in slot (9), movable sleeve (13) dress connect in swing piece (5) on and with circle pole (12) are connected, the spring (14) is connected between the fixed block (10) and the movable sleeve (13).
3. A drone having multiple flight modes, according to claim 1, wherein the telescopic section comprises: the device comprises an elongated slot (15), an inner rod (16), a movable cavity (17), an internal thread block (18), a cavity (19), a side hole (20), a rotating block (21) and a screw (22);
the long groove (15) is formed in the end face of the side of the connecting rod (2), the inner rod (16) is movably sleeved (13) in the long groove (15), the movable cavity (17) is formed in the end face of the side of the inner rod (16), the inner thread block (18) is arranged in the movable cavity (17), the cavity (19) is formed in the connecting rod (2), the side holes (20) are formed in the opposite side surfaces in the cavity (19), the rotating block (21) is rotatably connected in the cavity (19), the screw rod (22) penetrates through the inner side surface of the long groove (15) and is connected to the rotating block (21), and one end of the screw rod is in threaded connection with the inner thread block (18).
4. A drone with multiple flight modes according to claim 3, characterised in that the side surface of the turning block (21) is of anti-skid construction.
5. A drone with multiple flight modes according to claim 3, characterised in that the long slot (15) and the inner rod (16) are rectangular in section.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121258156.1U CN214930561U (en) | 2021-06-07 | 2021-06-07 | Unmanned aerial vehicle with multiple flight mode |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121258156.1U CN214930561U (en) | 2021-06-07 | 2021-06-07 | Unmanned aerial vehicle with multiple flight mode |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214930561U true CN214930561U (en) | 2021-11-30 |
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ID=79055965
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121258156.1U Active CN214930561U (en) | 2021-06-07 | 2021-06-07 | Unmanned aerial vehicle with multiple flight mode |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214930561U (en) |
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2021
- 2021-06-07 CN CN202121258156.1U patent/CN214930561U/en active Active
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