CN209739317U - Six rotary mechanism and have folding unmanned aerial vehicle of six rotors of this mechanism - Google Patents
Six rotary mechanism and have folding unmanned aerial vehicle of six rotors of this mechanism Download PDFInfo
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- CN209739317U CN209739317U CN201920061412.4U CN201920061412U CN209739317U CN 209739317 U CN209739317 U CN 209739317U CN 201920061412 U CN201920061412 U CN 201920061412U CN 209739317 U CN209739317 U CN 209739317U
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Abstract
the utility model discloses a six rotary mechanism and have folding unmanned aerial vehicle of six rotors of this mechanism, wherein, six rotary mechanism include swivel spare and lower swivel spare, go up the swivel spare and rotate with lower swivel spare and connect and realize that the swivel spare is around coaxial relative rotation with lower swivel spare, in addition, be equipped with body fixed establishment on going up the swivel spare, be equipped with four coupling mechanisms down on the swivel spare, body fixed establishment and coupling mechanism all are used for fixed long straight body. The utility model discloses a six rotary mechanism, after the fixed pipe of the upper and lower layer of unmanned aerial vehicle is connected respectively to upper and lower rotating member, realize the rotation of the upper and lower layer of unmanned aerial vehicle to reduce unmanned aerial vehicle's transportation volume under the condition of the dismantlement that reduces the part, thereby once can transport more unmanned aerial vehicle products and save the cost of transportation, in addition, unmanned aerial vehicle's packing can be done littleer, reduce the packing cost.
Description
Technical Field
The utility model relates to a connecting piece especially indicates a six rotary mechanism and have the folding unmanned aerial vehicle of six rotors of this mechanism.
Background
six rotor unmanned aerial vehicle occupation space of prior art are great, save space when the unmanned aerial vehicle of equipment is not convenient for transport. In addition, when packing unmanned aerial vehicle, the packaging material that too big space occupy is more, is unfavorable for saving the cost.
SUMMERY OF THE UTILITY MODEL
In view of this, the utility model aims to solve the technical problem that a six rotary mechanism is just provided, and it belongs to a rotary support piece, connects the fixed pipe of unmanned aerial vehicle's upper and lower floor, and the installation is used and can realize unmanned aerial vehicle's folding transportation on six rotor unmanned aerial vehicle, reduces the transportation volume and need not dismantle the part.
In order to solve the technical problem, the utility model discloses a following technical scheme realizes:
The utility model provides a six rotary mechanism, includes swivel work and lower swivel work, go up the swivel work and rotate with lower swivel work and connect and realize that swivel work and lower swivel work rotate around coaxial relative, in addition, be equipped with body fixed establishment on going up the swivel work, be equipped with four coupling mechanisms down on the swivel work, body fixed establishment and coupling mechanism all are used for fixed long straight body.
Preferably, a circular connecting hole groove is formed in the joint of the upper rotating piece and the lower rotating piece, a circular connecting column is arranged at the joint of the lower rotating piece and the upper rotating piece, and the connecting column is clamped in the connecting hole groove in a matched mode and rotates relatively.
Preferably, the pipe body fixing mechanism comprises a pipe groove and an arc-shaped fastener, and the pipe groove is connected with the arc-shaped fastener through a screw.
Preferably, the pipe joint mechanism comprises a joint groove and a joint fastener, and the joint groove and the joint fastener are connected through a screw.
The utility model provides a folding unmanned aerial vehicle of six rotors, includes lower floor's fixed part and upper rotating part, transversely wear to be equipped with four lower fixed pipes on the lower floor's fixed part, transversely wear to be equipped with fixed pipe on the upper rotating part, it connects through above-mentioned six rotary mechanism with lower fixed pipe in crossing department, specifically, it is fixed through the body fixed establishment on the last rotating part to go up fixed pipe, and four lower fixed pipes are fixed through four coupling mechanisms on the rotating part down, then the rotation between last rotating part through six rotary mechanism and the lower rotating part realizes six rotor unmanned aerial vehicle's folding, makes and goes up fixed pipe and rotates to and fix the pipe coincidence down.
Preferably, the rotors of the six-rotor folding unmanned aerial vehicle are respectively arranged on the upper fixing circular tube and the lower fixing circular tube.
Compared with the prior art, the utility model discloses the beneficial effect who has does:
The utility model discloses a six rotary mechanism, after the fixed pipe of the upper and lower layer of unmanned aerial vehicle is connected respectively to upper and lower rotating member, realize the rotation of the upper and lower layer of unmanned aerial vehicle to reduce unmanned aerial vehicle's transportation volume under the condition of the dismantlement that reduces the part, thereby once can transport more unmanned aerial vehicle products and save the cost of transportation, in addition, unmanned aerial vehicle's packing can be done littleer, reduce the packing cost.
Drawings
fig. 1 is one of the schematic three-dimensional structures of embodiment 1 of the present invention;
fig. 2 is a second schematic perspective view of embodiment 1 of the present invention;
Fig. 3 is a schematic side view of embodiment 1 of the present invention;
Fig. 4 is a schematic structural view of a six-rotor folding unmanned aerial vehicle according to embodiment 2 of the present invention;
Fig. 5 is a partially enlarged schematic view of fig. 4 according to the present invention;
Fig. 6 is the utility model discloses six rotor folding unmanned aerial vehicle's of embodiment 2 looks sideways at the schematic diagram.
Detailed Description
in order to make the technical personnel in this field more clear and intuitive to understand the present invention, the present invention will be further described with reference to the accompanying drawings.
Example 1
The six-axis rotating mechanism of this embodiment is shown in fig. 1-3, and includes an upper rotating member 1 and a lower rotating member 2, and the upper rotating member 1 and the lower rotating member 2 are connected in a rotating manner to realize that the upper rotating member 1 and the lower rotating member 2 rotate around the same axis relatively, and in addition, a pipe fixing mechanism 11 is provided on the upper rotating member 1, four pipe joint mechanisms 21 are provided on the lower rotating member 2, and both the pipe fixing mechanism 11 and the pipe joint mechanisms 21 are used for fixing a long straight pipe.
The joint of the upper rotating part 1 and the lower rotating part 2 is provided with a circular connecting hole groove, the joint of the lower rotating part 2 and the upper rotating part 1 is provided with a circular connecting column, and the connecting column is matched with the card to rotate relatively in the connecting hole groove. The joint pin cooperation card relatively rotates in the joint hole groove and can not separate, and it can adopt among the prior art can reach the mode realization of the same effect wantonly, if set up a bearing in the circular joint hole groove of last revolving part 1, the bearing cooperates with the joint pin of lower revolving part 2 and realizes on revolving part 1 with only relatively rotating of lower revolving part 2 and not separating, also can be simple nested technical realization.
The pipe fixing mechanism 11 includes a pipe groove 111 and an arc fastener 112, the pipe groove 111 is connected to the arc fastener 112 by screws, the pipe joint mechanism 21 includes a joint groove 211 and a joint fastener 212, and the joint groove 211 is connected to the joint fastener 212 by screws.
Example 2
The folding unmanned aerial vehicle of six rotors of this embodiment is as shown in fig. 4-6, including lower floor's fixed part 30 and upper rotating part 40, transversely wear to be equipped with four lower fixed pipes 31 on the lower floor's fixed part 30, transversely wear to be equipped with last fixed pipe 41 on the upper rotating part 40, it connects through the six rotary mechanism of embodiment 1 to go up fixed pipe 41 and lower fixed pipe 31 in crossing department, specifically, it is fixed that last fixed pipe 41 passes through body fixed establishment 11 on the rotating member 1, four lower fixed pipes 31 are fixed through four coupling mechanisms 21 on the rotating member 2 down, then the rotation between last rotating member 1 through six rotary mechanism and the lower rotating member 2 realizes the folding of six rotor unmanned aerial vehicle, make on fixed pipe 41 rotate to coincide with fixed pipe 31 down.
The rotors (not shown in the figure) of the six-rotor folding unmanned aerial vehicle are respectively arranged on the upper fixing circular tube 41 and the lower fixing circular tube 31.
The embodiments described above are intended to facilitate one of ordinary skill in the art in understanding and using the present invention. It will be readily apparent to those skilled in the art that various modifications to these embodiments may be made, and the generic principles described herein may be applied to other embodiments without the use of the inventive faculty. Therefore, the present invention is not limited to the embodiments herein, and those skilled in the art should make improvements and modifications to the present invention according to the disclosure of the present invention within the protection scope of the present invention.
Claims (6)
1. The utility model provides a six rotary mechanism, its characterized in that includes revolving part and lower revolving part, go up the revolving part and rotate with lower revolving part and connect and realize that revolving part and lower revolving part rotate around coaxial relative, in addition, be equipped with body fixed establishment on going up the revolving part, be equipped with four coupling mechanisms down on the revolving part, body fixed establishment and coupling mechanism all are used for fixed long straight body.
2. The six-axis rotating mechanism according to claim 1, wherein a circular connecting hole groove is formed in the joint of the upper rotating member and the lower rotating member, a circular connecting column is arranged in the joint of the lower rotating member and the upper rotating member, and the connecting column is clamped in the connecting hole groove in a matched mode and rotates relatively.
3. the six-axis rotating mechanism according to claim 1, wherein the pipe fixing mechanism comprises a pipe groove and an arc fastener, and the pipe groove and the arc fastener are connected through a screw.
4. the six-axis rotation mechanism of claim 1, wherein the coupling mechanism comprises a coupling slot and a coupling fastener, and the coupling slot and the coupling fastener are connected by a screw.
5. The utility model provides a folding unmanned aerial vehicle of six rotors, its characterized in that includes lower floor's fixed part and upper rotating part, transversely wear to be equipped with four fixed pipes down on the lower floor's fixed part, transversely wear to be equipped with fixed pipe on the upper rotating part, go up fixed pipe and fixed pipe down and pass through right 1 ~ 4 arbitrary department in crossing department six rotary mechanism connect, it is fixed that it passes through body fixed establishment on the rotating part to go up fixed pipe, and four fixed pipes are fixed through four coupling mechanisms on the lower rotating part down.
6. The folding unmanned aerial vehicle of claim 5, wherein the rotors of the folding unmanned aerial vehicle of six rotors are respectively disposed on the upper and lower fixed circular tubes.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920061412.4U CN209739317U (en) | 2019-01-14 | 2019-01-14 | Six rotary mechanism and have folding unmanned aerial vehicle of six rotors of this mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920061412.4U CN209739317U (en) | 2019-01-14 | 2019-01-14 | Six rotary mechanism and have folding unmanned aerial vehicle of six rotors of this mechanism |
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| Publication Number | Publication Date |
|---|---|
| CN209739317U true CN209739317U (en) | 2019-12-06 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201920061412.4U Active CN209739317U (en) | 2019-01-14 | 2019-01-14 | Six rotary mechanism and have folding unmanned aerial vehicle of six rotors of this mechanism |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109720546A (en) * | 2019-01-14 | 2019-05-07 | 珠海卡特瑞科农林航空装备研究所有限公司 | A kind of six axis rotating mechanism and six rotors with the mechanism fold unmanned plane |
-
2019
- 2019-01-14 CN CN201920061412.4U patent/CN209739317U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109720546A (en) * | 2019-01-14 | 2019-05-07 | 珠海卡特瑞科农林航空装备研究所有限公司 | A kind of six axis rotating mechanism and six rotors with the mechanism fold unmanned plane |
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