CN207956051U - A kind of novel more rotor links of unmanned plane - Google Patents
A kind of novel more rotor links of unmanned plane Download PDFInfo
- Publication number
- CN207956051U CN207956051U CN201820176901.XU CN201820176901U CN207956051U CN 207956051 U CN207956051 U CN 207956051U CN 201820176901 U CN201820176901 U CN 201820176901U CN 207956051 U CN207956051 U CN 207956051U
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- CN
- China
- Prior art keywords
- chassis
- sides
- unmanned plane
- clamping block
- fixedly connected
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Abstract
The utility model discloses a kind of novel more rotor links of unmanned plane, including chassis, cushion block and supporting rack, one end both sides of the chassis are fixedly connected with cushion block, the other end both sides of the chassis are uniformly fixedly connected with clamping block, the both sides of the clamping block are provided with convex block, one end position of support frame as described above is welded with connecting rod, the stack shell both sides of the connection rotation cylinder offer buckling groove, the connection rotation cylinder is connect with clamping block, the both-side ends of support frame as described above have been fixedly connected with side plate, the top of the side plate and supporting rack is uniformly provided with wire casing, wire casing side on support frame as described above is rotatably connected to geometrical clamp, the both ends of the side plate have been fixedly connected with erecting bed.The utility model is by adding wire casing, so that putting for wire rod is more beautiful, rotation cylinder and clamping block are connected by adding so that device, which is provided simultaneously with, to be connected firmly and advantage easy to disassemble, by adding gasket, the phenomenon that metal chassis scratches unmanned aerial vehicle body is prevented.
Description
Technical field
The utility model is related to unmanned plane related accessory technical field, specially a kind of unmanned plane is connected with novel more rotors
Connect frame.
Background technology
Multi-rotor unmanned aerial vehicle is a kind of tool there are three and the above rotor shaft special pilotless helicopter.It passes through
Motor rotation on each axis, drives rotor, to generate a liter thrust.Rotor always away from fixation, rather than general helicopter
It is variable like that.By changing the relative rotation speed between different rotors, thus it is possible to vary the size of uniaxial propulsive force, to control flight
The running orbit of device.Generally there are structures to be not sufficiently stable for the existing more rotor links of unmanned plane, and dismounting not enough facilitates and line
Putting for material is mixed and disorderly unordered, while link may cause to damage while installation to unmanned aerial vehicle body.Therefore, I provides
A kind of novel more rotor links of unmanned plane.
Utility model content
The purpose of this utility model is to provide a kind of novel more rotor links of unmanned plane, to solve above-mentioned background skill
The problem of being proposed in art.
To achieve the above object, the utility model provides the following technical solutions：A kind of novel more rotors connections of unmanned plane
One end both sides of frame, including chassis, cushion block and supporting rack, the chassis are fixedly connected with cushion block, the other end of the chassis
Both sides are uniformly fixedly connected with clamping block, and the both sides of the clamping block are provided with convex block, the end position welding of support frame as described above
There are connecting rod, the both ends of the connecting rod to be evenly arranged with annulus, and is connected with connection rotation cylinder in annulus, the connection rotation cylinder
Stack shell both sides offer buckling groove, and the connection rotation cylinder is connect with clamping block, and the both-side ends of support frame as described above are fixed to be connected
It is connected to side plate, the top of the side plate and supporting rack is uniformly provided with wire casing, the wire casing side rotation connection on support frame as described above
There are geometrical clamp, the both ends of the side plate to be fixedly connected with erecting bed.
Preferably, the connection of the connection rotation cylinder and clamping block is realized by the clamping of buckling groove and convex block.
Preferably, mounting hole, and the mounting hole position on chassis and cushion block are offered on the chassis, cushion block and erecting bed
It sets and matches.
Preferably, the material of support frame as described above and chassis is aircraft aluminum 7075, and the material of the erecting bed is stainless
Steel.
Preferably, the middle position of the wire casing offers circular hole, and circular hole runs through supporting rack.
Compared with prior art, the utility model has the beneficial effects that：The utility model is reasonable for structure, is skillfully constructed, wound
Meaning Nover practical, passes through and adds wire casing so that putting for wire rod not only orderly maintains easily, also more beautiful, passes through the company of addition
Connect rotation cylinder and clamping block so that device, which is provided simultaneously with, to be connected firmly and advantage easy to disassemble, by adding gasket, prevents
Metal chassis scratches the phenomenon that unmanned aerial vehicle body.
Description of the drawings
Fig. 1 is the structural schematic diagram of the utility model；
Fig. 2 is the Undercarriage structure schematic diagram of the utility model；
Fig. 3 is that sketch drawing is revolved in the connection of the utility model.
In figure：1 chassis, 2 cushion blocks, 3 connecting rods, 4 connection rotation cylinders, 5 supporting racks, 6 wire casings, 7 side plates, 8 erecting beds, 9 are fixed
Folder, 10 clamping blocks, 11 convex blocks, 12 buckling grooves.
Specific implementation mode
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
The every other embodiment obtained, shall fall within the protection scope of the present invention.
In the description of the utility model, it should be noted that the side of the instructions such as term "vertical", "upper", "lower", "horizontal"
Either position relationship is orientation based on ... shown in the drawings or position relationship for position, is merely for convenience of describing this practicality and simplification is retouched
State, rather than indicate either to imply that signified device or element must have a particular orientation, with specific azimuth configuration and
Operation, therefore should not be understood as limiting the present invention.In addition, " first ", " second ", " third ", " the 4th " are only used for
Purpose is described, and should not be understood as indicating or implying relative importance.
In the description of the utility model, it is also necessary to which explanation " is set unless otherwise specific regulation and limitation, term
Set ", " installation ", " connected ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection,
Or be integrally connected, it can be mechanical connection, can also be electrical connection, can be directly connected to, can also be by intermediate matchmaker
It is situated between and is connected, can is the connection inside two elements.It for the ordinary skill in the art, can be as the case may be
Understand the concrete meaning of above-mentioned term in the present invention.
- 3 are please referred to Fig.1, the utility model provides a kind of technical solution：A kind of novel more rotor links of unmanned plane,
Including chassis 1, cushion block 2 and supporting rack 5, one end both sides of the chassis 1 are fixedly connected with cushion block 2, the chassis 1 it is another
End both sides are uniformly fixedly connected with clamping block 10, and the both sides of the clamping block 10 are provided with convex block 11, one end of support frame as described above 5
Position is welded with connecting rod 3, and the both ends of the connecting rod 3 are evenly arranged with annulus, and connection rotation cylinder 4 is connected in the middle part of annulus,
The stack shell both sides of the connection rotation cylinder 4 offer buckling groove 12, and the connection rotation cylinder 4 is connect with clamping block 10, the connection
It revolves cylinder 4 and the connection of clamping block 10 is realized by buckling groove 12 and the clamping of convex block 11, by taking clamping connecting structure so that
Device, which is provided simultaneously with, to be connected firmly and advantage easy to disassemble, and the both-side ends of support frame as described above 5 have been fixedly connected with side plate 7,
The side plate 7 and the top of supporting rack 5 are uniformly provided with wire casing 6, and the middle position of the wire casing 6 offers circular hole, and circular hole
Through supporting rack 5 so that the connection of wire rod more rational and orderly and beauty, 6 side of the wire casing rotation connection on support frame as described above 5
There is a geometrical clamp 9, the both ends of the side plate 7 have been fixedly connected with erecting bed 8, and the material of support frame as described above 5 and chassis 1 is aviation
The material of aluminium 7075, the erecting bed 8 is stainless steel, while reducing the weight of the device, the quality of lifting device structure, institute
It states and offers mounting hole on chassis 1, cushion block 2 and erecting bed 8, and the position of mounting hole on chassis 1 and cushion block 2 matches, lead to
Cross reserving installation hole so that the installation of device more standard and convenient.
Operation principle：In use, the wire rod on unmanned plane is placed to across circular hole in wire casing 6 first, then by solid
Clamp 9 is fixed, and then, chassis 1 is threadedly coupled by bolt with unmanned plane, and connection rotation cylinder 4 blocks with clamping block 10 at this time
It connects, after being fixed, the rotor of unmanned plane is mounted on erecting bed 8, wherein cushion block 2, which plays, prevents metal bottom
Frame 1 scratches the effect of unmanned aerial vehicle body, and wire casing 6 plays so that wire rod is orderly put so that wire rod puts beauty, connection rotation cylinder
4 buckling groove makes the connection between apparatus structure more stablize.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is appreciated that can these embodiments be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaiied
Change, replace and modification, the scope of the utility model are defined by the appended claims and the equivalents thereof.
Claims (5)
1. a kind of novel more rotor links of unmanned plane, including chassis (1), cushion block (2) and supporting rack (5), it is characterised in that：
One end both sides of the chassis (1) are fixedly connected with cushion block (2), and the other end both sides of the chassis (1) are uniformly fixedly connected
There are clamping block (10), the both sides of the clamping block (10) to be provided with convex block (11), an end position of support frame as described above (5) is welded with
The both ends of connecting rod (3), the connecting rod (3) are evenly arranged with annulus, and connection rotation cylinder (4) is connected in the middle part of annulus, described
The stack shell both sides of connection rotation cylinder (4) offer buckling groove (12), and the connection rotation cylinder (4) connect with clamping block (10), described
The both-side ends of supporting rack (5) have been fixedly connected with side plate (7), and the side plate (7) and the top of supporting rack (5) are uniformly provided with
Wire casing (6), wire casing (6) side on support frame as described above (5) are rotatably connected to geometrical clamp (9), and the both ends of the side plate (7) are solid
Surely it is connected with erecting bed (8).
2. a kind of novel more rotor links of unmanned plane according to claim 1, it is characterised in that：Cylinder is revolved in the connection
(4) it is realized by the clamping of buckling groove (12) and convex block (11) with the connection of clamping block (10).
3. a kind of novel more rotor links of unmanned plane according to claim 1, it is characterised in that：The chassis (1),
Mounting hole is offered on cushion block (2) and erecting bed (8), and the position of mounting hole on chassis (1) and cushion block (2) matches.
4. a kind of novel more rotor links of unmanned plane according to claim 1, it is characterised in that：Support frame as described above
(5) and the material of chassis (1) is aircraft aluminum 7075, and the material of the erecting bed (8) is stainless steel.
5. a kind of novel more rotor links of unmanned plane according to claim 1, it is characterised in that：The wire casing (6)
Middle position offer circular hole, and circular hole runs through supporting rack (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820176901.XU CN207956051U (en) | 2018-02-01 | 2018-02-01 | A kind of novel more rotor links of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820176901.XU CN207956051U (en) | 2018-02-01 | 2018-02-01 | A kind of novel more rotor links of unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207956051U true CN207956051U (en) | 2018-10-12 |
Family
ID=63736752
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820176901.XU Expired - Fee Related CN207956051U (en) | 2018-02-01 | 2018-02-01 | A kind of novel more rotor links of unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207956051U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2023128955A1 (en) * | 2021-12-31 | 2023-07-06 | İstanbul Geli̇şi̇m Üni̇versi̇tesi̇ | Coaxial aluminum sigma drone chassis |
-
2018
- 2018-02-01 CN CN201820176901.XU patent/CN207956051U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2023128955A1 (en) * | 2021-12-31 | 2023-07-06 | İstanbul Geli̇şi̇m Üni̇versi̇tesi̇ | Coaxial aluminum sigma drone chassis |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20181012 Termination date: 20220201 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |