CN209852557U - Novel 6 frames of unmanned aerial vehicle - Google Patents
Novel 6 frames of unmanned aerial vehicle Download PDFInfo
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- CN209852557U CN209852557U CN201920360560.6U CN201920360560U CN209852557U CN 209852557 U CN209852557 U CN 209852557U CN 201920360560 U CN201920360560 U CN 201920360560U CN 209852557 U CN209852557 U CN 209852557U
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- blind hole
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- aerial vehicle
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Abstract
The utility model discloses a novel 6 frame frames of unmanned aerial vehicle belongs to unmanned air vehicle technique field. The unmanned aerial vehicle 6 frame comprises an upper central piece, a lower central piece and a boom pipe, wherein the upper central piece comprises a polygonal upper central plate and a plurality of first fixing seats integrally formed with the upper central plate, and each first fixing seat is provided with a first threaded blind hole; the lower central piece comprises a polygonal lower central plate and a plurality of second fixed seats integrally formed with the lower central plate, and each second fixed seat is provided with a second threaded blind hole; one end of the arm pipe is provided with a threaded through hole corresponding to the first threaded blind hole or the second threaded blind hole; and a first fastening screw is used for penetrating through the threaded through hole to be in threaded connection with the first or second threaded blind hole so as to fasten the upper center piece, the lower center piece and the horn tube together. The utility model discloses a 6 frame assembly structure of unmanned aerial vehicle's each part both can not too scattered, convenient dismantlement, equipment and change again, and portable.
Description
Technical Field
The utility model relates to a frame especially relates to a novel 6 frames of unmanned aerial vehicle frame, belongs to unmanned air vehicle technical field.
Background
The unmanned plane is an unmanned plane for short, and is an unmanned aerial vehicle operated by a radio remote control device or a self program control device. The unmanned aerial vehicle has wide application, plays an extremely important role in modern wars, and has a wide prospect in the civil field. At present, unmanned aerial vehicles are widely applied to the fields of police, city management, agriculture, geology, meteorology, electric power, rescue and relief work, video shooting and the like.
In the prior art, the unmanned aerial vehicle frame mainly includes two kinds of structures: an integrally formed structure and a structure with parts assembled together. For the integrally formed unmanned aerial vehicle frame, if part of the frame is damaged, the frame needs to be integrally replaced, so that the cost is too high; to the unmanned aerial vehicle frame of each part equipment together, each part is too scattered again, then can lead to dismantling the equipment inconvenient.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a novel 6 frame frames of unmanned aerial vehicle, it can overcome the too scattered shortcoming of each part of unmanned aerial vehicle frame package assembly, but also convenient to detach, equipment and change.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
a novel unmanned aerial vehicle 6-frame comprises an upper central piece, a lower central piece and an arm pipe, wherein the upper central piece comprises a polygonal upper central plate and a plurality of first fixing seats arranged on the upper central plate, the first fixing seats and the upper central plate are integrally formed, and each first fixing seat is provided with a first threaded blind hole; the lower central piece comprises a polygonal lower central plate and a plurality of second fixed seats arranged on the lower central plate, the second fixed seats and the lower central plate are integrally formed, and each second fixed seat is provided with a second threaded blind hole; one end of the machine arm pipe is provided with a first locking part, and the first locking part comprises a machine arm pipe seat extending outwards from the pipe wall of the machine arm pipe, a threaded through hole arranged on the machine arm pipe seat and corresponding to the first threaded blind hole or the second threaded blind hole, and a first fastening screw capable of being matched with the threaded through hole and the first threaded blind hole or the second threaded blind hole; and the first fastening screw penetrates through the threaded through hole to be in threaded connection with the first threaded blind hole or the second threaded blind hole so as to fasten the upper center piece, the lower center piece and the horn tube together.
As a further preferred aspect of the present invention, the arm tube and the arm tube seat are also integrally formed.
As a further preference of the present invention, the first fixing base is a split structure and is composed of an upper left fixing base and an upper right fixing base, and the upper left fixing base and the upper right fixing base are respectively provided with a first threaded blind hole; the second fixing base is also of a split structure and is composed of a left lower fixing base and a right lower fixing base, and the left lower fixing base and the right lower fixing base are respectively provided with a second threaded blind hole.
As a further preferred aspect of the present invention, the arm tube is a two-fold arm tube structure.
As a further preference of the present invention, the arm tube includes a first arm tube and a second arm tube, the first locking portion is provided at one end of the second arm tube, the other end of the second arm tube is provided with a second locking portion, one end of the first arm tube is provided with a third locking portion, one side of the second locking portion is pivoted with one side of the third locking portion, and the other side of the second locking portion is detachably connected with the other side of the third locking portion.
As a further preference of the present invention, the other side of the second locking portion is provided with a groove, the other side of the third locking portion is provided with a protrusion, the protrusion is fittingly placed in the groove, the protrusion is provided with a first through hole penetrating through both ends of the protrusion, one side of the groove is provided with a jack, and the other side is provided with a third threaded blind hole; the second locking part further comprises a second fastening screw, and the second fastening screw penetrates through the jack, the first through hole and the third threaded blind hole to be in threaded connection, so that the first machine arm pipe and the second machine arm pipe are locked.
As a further preferred aspect of the present invention, the present invention further comprises a support leg, wherein the top of the support leg is fixedly connected to the lower central plate.
As a further preferred feature of the present invention, the upper central plate, the lower central plate and the arm pipe are thin-walled members made of LF6-R- δ 50 material.
Compared with the prior art, the utility model discloses following beneficial technological effect has:
the utility model provides a novel 6 frame frames of unmanned aerial vehicle, through adopting in the center plate, with last center plate integrated into one piece's first fixing base, center plate down, with center plate integrated into one piece's second fixing base down and set up at the first locking portion of horn pipe one end with the center part, center part and horn pipe detachably link together down, make each part of unmanned aerial vehicle frame package assembly not only can be too scattered, convenient to detach again, equipment and change, and in case certain part damages, only need to replace this damage part can, the cost is reduced. In addition, the horn pipe adopts folding mechanism, conveniently carries.
Drawings
Fig. 1 is a schematic view of an overall structure of a 6-frame of a novel unmanned aerial vehicle according to an embodiment of the present invention;
fig. 2 is a schematic structural view of an upper center piece and a lower center piece according to an embodiment of the present invention;
fig. 3 is a schematic structural diagram of a boom pipe according to an embodiment of the present invention;
fig. 4 is a schematic view of a folding structure of the boom pipe according to an embodiment of the present invention;
fig. 5 is a schematic structural view of a lower center piece according to another embodiment of the present invention.
Wherein, 1 is an upper central plate; 2 a lower center plate; 3 a first fixed seat; 4 a second fixed seat; 5 a first threaded blind hole; 6 second threaded blind holes; 8, a horn tube seat; 9, a threaded through hole; 10 a first fastening screw; 11 a first arm tube; 12 a second arm tube; 13 a second locking portion; 14 a third locking portion; 15 a second fastening screw; 16 protrusions; 17, grooves; 18 a first via hole; 20 a third threaded blind hole; 21 support the foot rest.
Detailed Description
The invention will be further described with reference to specific embodiments. The following examples are only for illustrating the technical solutions of the present invention more clearly, and the protection scope of the present invention is not limited thereby.
As shown in fig. 1 to 3, in an embodiment of the present invention, a novel unmanned aerial vehicle 6-frame includes an upper center piece, a lower center piece, a boom pipe, and a support foot frame 21.
The upper central piece comprises a polygonal upper central plate 1 and a plurality of first fixing seats 3 arranged on the upper central plate 1, the first fixing seats 3 are integrally formed with the upper central plate 1, and each first fixing seat 3 is provided with two first threaded blind holes 5.
The lower central piece comprises a polygonal lower central plate 2 and a plurality of second fixed seats 4 arranged on the lower central plate 2, the second fixed seats 4 are integrally formed with the lower central plate 2, and each second fixed seat 4 is provided with two second threaded blind holes 6.
Fig. 2 shows that the first fixing seat 3 and the second fixing seat 4 are rectangular parallelepiped structures, which may be structures of other shapes.
Further, the upper central plate, the lower central plate and the horn tube are all thin-walled pieces made of LF 6-R-delta 50 material.
In another embodiment of the present invention, the second fixing base 4 can be configured as a split structure, as shown in fig. 5 (only the second fixing base is shown), the second fixing base 4 is composed of a lower left fixing base and a lower right fixing base, and the lower left fixing base and the lower right fixing base are respectively provided with a second threaded blind hole 6. Similarly, first fixing base 3 also is split type structure, comprises upper left fixing base, upper right fixing base, upper left fixing base, upper right fixing base respectively are provided with a first screw thread blind hole 5.
One end of the arm pipe is provided with a first locking part, and the other end of the arm pipe is connected with the motor. The first locking portion comprises a horn tube seat 8, a threaded through hole 9 and a first fastening screw 10, wherein the horn tube seat 8 extends outwards from the outer tube wall of the horn tube, the threaded through hole 9 is formed in the horn tube seat 8 and corresponds to the first threaded blind hole 5 or the second threaded blind hole 6, and the first fastening screw can be matched with the threaded through hole 9 and the first threaded blind hole 5 or the second threaded blind hole 6. Wherein the first fastening screw 10 is threaded with the first threaded blind hole 5 or the second threaded blind hole 6 through the threaded through hole 9 to fasten the upper center piece, the lower center piece and the horn tube together. Preferably, the boom pipe and the boom pipe base 8 are integrally formed.
The top of the supporting foot frame 21 is fixedly connected with the lower central plate 2, so that the unmanned aerial vehicle can stably stand after falling to the ground.
In another preferred embodiment of the present invention, the arm tube is a two-folded arm tube structure, and the folding structure is convenient for the user to carry. As shown in fig. 4, the arm pipe includes a first arm pipe 11 and a second arm pipe 12, the first locking portion is provided at one end of the second arm pipe 12, the other end of the second arm pipe 12 is provided with a second locking portion 13, one end of the first arm pipe 11 is provided with a third locking portion 14, and the other end is connected to a motor. One side of the second locking portion 13 is pivotally connected to one side of the third locking portion 14 by a pivot pin, and the other side of the second locking portion 13 is connected to the other side of the third locking portion 14 by a second fastening screw 15.
Specifically, a groove 17 is formed in the other side of the second locking portion 13, a protrusion 16 is formed in the other side of the third locking portion 14, the protrusion 16 is fittingly disposed in the groove 17, a first through hole 18 penetrating through two ends of the protrusion 16 is formed in the protrusion 16, an insertion hole is formed in one side of the groove 17, a third threaded blind hole 20 is formed in the other side of the groove 17, and the second fastening screw 15 penetrates through the insertion hole, the first through hole 18 and the third threaded blind hole 20 to be in threaded connection, so that the first boom pipe 11 and the second boom pipe 1214 are locked.
In other embodiments of the present invention, the slot 17 is provided with a jack on one side, the other side is provided with a second through hole, and the second fastening screw 15 is locked by a nut after passing through the jack, the first through hole 18 and the second through hole, so as to lock the first boom pipe 11 and the second boom pipe 1214.
Owing to adopt above-mentioned structure, the utility model discloses a novel 6 frame package assembly of unmanned aerial vehicle's each part both can not too scattered, conveniently dismantle equipment and change again, in case certain part damages moreover, only need replace this damage part can to the cost that integrated into one piece structure part damages needs whole replacement has been reduced.
The present invention has been disclosed in the foregoing with reference to the preferred embodiments, but it is not intended to limit the present invention, and all technical solutions obtained by adopting equivalent replacement or equivalent transformation schemes fall within the protection scope of the present invention.
Claims (8)
1. The novel unmanned aerial vehicle 6-frame is characterized by comprising an upper central piece, a lower central piece and an arm pipe, wherein the upper central piece comprises a polygonal upper central plate (1) and a plurality of first fixing seats (3) arranged on the upper central plate (1), the first fixing seats (3) and the upper central plate (1) are integrally formed, and each first fixing seat (3) is provided with a first threaded blind hole (5); the lower central piece comprises a polygonal lower central plate (2) and a plurality of second fixed seats (4) arranged on the lower central plate (2), the second fixed seats (4) and the lower central plate (2) are integrally formed, and each second fixed seat (4) is provided with a second threaded blind hole (6); one end of the machine arm pipe is provided with a first locking part, the first locking part comprises a machine arm pipe seat (8) extending outwards from the outer pipe wall of the machine arm pipe, a threaded through hole (9) which is arranged on the machine arm pipe seat (8) and corresponds to the first threaded blind hole (5) or the second threaded blind hole (6), and a first fastening screw (10) which can be matched with the threaded through hole (9) and the first threaded blind hole (5) or the second threaded blind hole (6); the first fastening screw (10) penetrates through the threaded through hole (9) to be in threaded connection with the first threaded blind hole (5) or the second threaded blind hole (6) so as to fasten the upper center piece, the lower center piece and the machine arm pipe together.
2. The new unmanned 6-frame of claim 1, wherein the boom pipe and the boom pipe seat (8) are also of an integral structure.
3. The novel unmanned aerial vehicle 6-frame according to claim 1, wherein the first fixing seat (3) is of a split structure and is composed of an upper left fixing seat and an upper right fixing seat, and the upper left fixing seat and the upper right fixing seat are respectively provided with a first threaded blind hole (5); the second fixing seat (4) is also of a split structure and is composed of a left lower fixing seat and a right lower fixing seat, and the left lower fixing seat and the right lower fixing seat are respectively provided with a second threaded blind hole (6).
4. The novel unmanned aerial vehicle 6 frame of claim 1, wherein the boom pipe is a two fold boom pipe structure.
5. A novel unmanned aerial vehicle 6 frame of claim 4, characterized in that, the arm pipe includes a first arm pipe (11) and a second arm pipe (12), the first locking portion is arranged at one end of the second arm pipe (12), the other end of the second arm pipe (12) is provided with a second locking portion (13), one end of the first arm pipe (11) is provided with a third locking portion (14), one side of the second locking portion (13) is pivoted with one side of the third locking portion (14), and the other side of the second locking portion (13) is detachably connected with the other side of the third locking portion (14).
6. The novel unmanned aerial vehicle 6-frame of claim 5, wherein a groove (17) is formed in the other side of the second locking portion (13), a protrusion (16) is formed in the other side of the third locking portion (14), the protrusion (16) is fittingly placed in the groove (17), the protrusion (16) is provided with a first through hole (18) penetrating through two ends of the protrusion (16), a jack is formed in one side of the groove (17), and a third threaded blind hole (20) is formed in the other side of the groove; the second locking part (13) further comprises a second fastening screw (15), and the second fastening screw (15) penetrates through the insertion hole, the first through hole (18) and the third threaded blind hole (20) to be in threaded connection, so that the first arm pipe (11) and the second arm pipe (12) are locked.
7. The novel unmanned aerial vehicle 6 frame of claim 1, further comprising a support foot stand (21), wherein the top of the support foot stand (21) is fixedly connected with the lower central plate (2).
8. The novel unmanned aerial vehicle 6-frame framework of claim 1, wherein the upper central plate, the lower central plate and the horn tube are thin-walled pieces made of LF6-R- δ 50 material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920360560.6U CN209852557U (en) | 2019-03-20 | 2019-03-20 | Novel 6 frames of unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920360560.6U CN209852557U (en) | 2019-03-20 | 2019-03-20 | Novel 6 frames of unmanned aerial vehicle |
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| CN209852557U true CN209852557U (en) | 2019-12-27 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201920360560.6U Active CN209852557U (en) | 2019-03-20 | 2019-03-20 | Novel 6 frames of unmanned aerial vehicle |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109911170A (en) * | 2019-03-20 | 2019-06-21 | 南京儒一航空机械装备有限公司 | A kind of 6 circle frame of novel unmanned plane |
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2019
- 2019-03-20 CN CN201920360560.6U patent/CN209852557U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109911170A (en) * | 2019-03-20 | 2019-06-21 | 南京儒一航空机械装备有限公司 | A kind of 6 circle frame of novel unmanned plane |
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