CN206265302U - A kind of unmanned plane of wing adjustable angle - Google Patents
A kind of unmanned plane of wing adjustable angle Download PDFInfo
- Publication number
- CN206265302U CN206265302U CN201621087453.3U CN201621087453U CN206265302U CN 206265302 U CN206265302 U CN 206265302U CN 201621087453 U CN201621087453 U CN 201621087453U CN 206265302 U CN206265302 U CN 206265302U
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- CN
- China
- Prior art keywords
- wing
- unmanned plane
- center support
- adjustable angle
- angle adjustment
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Abstract
The utility model provides a kind of unmanned plane of wing adjustable angle, including center support and wing, the center support is connected with wing axis, the wing axis are connected with wing angle adjustment block, the side of the wing angle adjustment block is provided with curved angle adjustment groove, and the wing adjusts groove and is connected by fastener and the curved angle.The beneficial effects of the utility model are：The angle of wing can be adjusted by wing angle adjustment block, to adapt to different use environments.
Description
Technical field
The utility model is related to unmanned plane, more particularly to a kind of unmanned plane of wing adjustable angle.
Background technology
The wing angle of traditional unmanned plane is to fix nonadjustable, cannot use environments to adjustment wing according to different
Angle.
The content of the invention
In order to solve the problems of the prior art, the utility model provides a kind of unmanned plane of wing adjustable angle.
The utility model provides a kind of unmanned plane of wing adjustable angle, including center support and wing, it is described in
Scheming seat is connected with wing axis, and the wing axis are connected with wing angle adjustment block, on the side of the wing angle adjustment block
Curved angle adjustment groove is provided with, the wing adjusts groove and is connected by fastener and the curved angle.
Used as further improvement of the utility model, the curved angle adjusts groove at least two and around the wing
The circumferentially-spaced of axle is uniformly arranged.
Used as further improvement of the utility model, the curved angle adjustment groove has four weeks around the wing axis
To the setting of 90 degree of interval.
Used as further improvement of the utility model, the center support is connected with horn, and the horn is arranged with connection
Sleeve, the branch sleeve is connected with propeller module.
Used as further improvement of the utility model, the branch sleeve includes the first arc folder and the second arc folder, institute
The first arc folder, the second arc folder is stated to be bolted on the horn.
As further improvement of the utility model, the center support be section be regular hexagon tubing, it is described in
Each side of scheming seat is equipped with a jack, and a horn is respectively connected with each described jack.
Used as further improvement of the utility model, the center support is connected with battery case, is provided with the battery case
At least two independent battery compartments for overlapping up and down.
The beneficial effects of the utility model are：By such scheme, wing can be adjusted by wing angle adjustment block
Angle, to adapt to different use environments.
Brief description of the drawings
Fig. 1 is a kind of assembling schematic diagram figure of the center support of the unmanned plane of wing adjustable angle of the utility model.
Fig. 2 is a kind of schematic diagram of the wing angle adjustment block of the unmanned plane of wing adjustable angle of the utility model.
Fig. 3 is a kind of six axle schematic diagrames of the unmanned plane of wing adjustable angle of the utility model.
Fig. 4 is a kind of propeller module assembling schematic diagram of the unmanned plane of wing adjustable angle of the utility model.
Fig. 5 is a kind of propeller module assembling schematic diagram of the unmanned plane of wing adjustable angle of the utility model.
Fig. 6 is a kind of battery case schematic diagram of the unmanned plane of wing adjustable angle of the utility model.
Specific embodiment
Explanation and specific embodiment are further illustrated to the utility model below in conjunction with the accompanying drawings.
Drawing reference numeral in Fig. 1 to Fig. 6 is：Center support 1；Wing axis 2；Wing angle adjustment block 3；Curved angle is adjusted
Groove 31；Horn 4；Propeller module 5；Branch sleeve 6；Battery case 7.
As shown in Figures 1 to 6, a kind of unmanned plane of wing adjustable angle, including center support 1 and wing, it is described in
Scheming seat 1 is connected with wing axis 2, and the wing axis 2 are connected with wing angle adjustment block 3, the side of the wing angle adjustment block 3
Face is provided with curved angle adjustment groove 31, and the wing adjusts groove 31 and is connected by fastener and the curved angle.
As shown in Figures 1 to 6, the curved angle adjusts groove 31 at least two and around the circumference of the wing axis 2
Interval is uniformly arranged.
As shown in Figures 1 to 6, the curved angle adjustment groove 31 has four around circumferentially-spaced the 90 of the wing axis 2
Degree is set.
As shown in Figures 1 to 6, the center support 1 is connected with horn 4, and the horn 4 is arranged with branch sleeve 6, described
Branch sleeve 6 is connected with propeller module 5, and branch sleeve 6 can be positive and negative on horn 4, can realize spiral shell by branch sleeve 6
The positive and negative installation of rotation oar module 5.
As shown in Figures 1 to 6, the branch sleeve 6 includes the first arc folder and the second arc folder, first arc
Folder, the second arc folder are bolted on the horn 4.
As shown in Figures 1 to 6, the center support 1 be section be regular hexagon tubing, the center support 1 it is every
Individual side is equipped with a jack, and a horn 4 is respectively connected with each described jack, realizes six axle construction.
As shown in Figures 1 to 6, the center support 1 is connected with battery case 7, the battery case 7 and is provided with least two solely
The vertical battery compartment for overlapping up and down, flexibly can install battery according to use demand.
A kind of unmanned plane of wing adjustable angle that the utility model is provided, can be adjusted by wing angle adjustment block
The angle of wing, to adapt to different use environments.
Above content is to combine specific preferred embodiment further detailed description of the utility model, it is impossible to
Assert that specific implementation of the present utility model is confined to these explanations.For the ordinary skill of the utility model art
For personnel, without departing from the concept of the premise utility, some simple deduction or replace can also be made, should all regarded
To belong to protection domain of the present utility model.
Claims (7)
1. a kind of unmanned plane of wing adjustable angle, it is characterised in that：Including center support and wing, the center support connects
Wing axis are connected to, the wing axis are connected with wing angle adjustment block, and the side of the wing angle adjustment block is provided with arc
Angle adjustment groove, the wing adjusts groove and is connected by fastener and the curved angle.
2. the unmanned plane of wing adjustable angle according to claim 1, it is characterised in that：The curved angle adjustment is recessed
Groove at least two is simultaneously uniformly arranged around the circumferentially-spaced of the wing axis.
3. the unmanned plane of wing adjustable angle according to claim 1, it is characterised in that：The curved angle adjustment is recessed
Groove has four circumferentially-spaced 90 degree of settings around the wing axis.
4. the unmanned plane of wing adjustable angle according to claim 1, it is characterised in that：The center support is connected with
Horn, the horn is arranged with branch sleeve, and the branch sleeve is connected with propeller module.
5. the unmanned plane of wing adjustable angle according to claim 4, it is characterised in that：The branch sleeve includes the
One arc is pressed from both sides and the second arc folder, and the first arc folder, the second arc folder are bolted on the horn.
6. the unmanned plane of wing adjustable angle according to claim 4, it is characterised in that：The center support is section
It is the tubing of regular hexagon, each side of the center support is equipped with a jack, is respectively connected with each described jack
One horn.
7. the unmanned plane of wing adjustable angle according to claim 1, it is characterised in that：The center support is connected with
Battery case, is provided with least two independent battery compartments for overlapping up and down in the battery case.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621087453.3U CN206265302U (en) | 2016-09-28 | 2016-09-28 | A kind of unmanned plane of wing adjustable angle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621087453.3U CN206265302U (en) | 2016-09-28 | 2016-09-28 | A kind of unmanned plane of wing adjustable angle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206265302U true CN206265302U (en) | 2017-06-20 |
Family
ID=59036219
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621087453.3U Active CN206265302U (en) | 2016-09-28 | 2016-09-28 | A kind of unmanned plane of wing adjustable angle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206265302U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106347658A (en) * | 2016-09-28 | 2017-01-25 | 深圳智航无人机有限公司 | Unmanned aerial vehicle with adjustable wing angle |
| CN107826244A (en) * | 2017-11-15 | 2018-03-23 | 安徽工程大学 | A kind of six shaft rotating devices of aircraft |
-
2016
- 2016-09-28 CN CN201621087453.3U patent/CN206265302U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106347658A (en) * | 2016-09-28 | 2017-01-25 | 深圳智航无人机有限公司 | Unmanned aerial vehicle with adjustable wing angle |
| CN106347658B (en) * | 2016-09-28 | 2019-05-17 | 深圳智航无人机有限公司 | A kind of unmanned plane of wing adjustable angle |
| CN107826244A (en) * | 2017-11-15 | 2018-03-23 | 安徽工程大学 | A kind of six shaft rotating devices of aircraft |
| CN107826244B (en) * | 2017-11-15 | 2021-03-09 | 安徽工程大学 | Six rotary device of aircraft |
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| GR01 | Patent grant |