CN206412478U - A kind of unmanned plane signal enhancing antenna structure - Google Patents
A kind of unmanned plane signal enhancing antenna structure Download PDFInfo
- Publication number
- CN206412478U CN206412478U CN201720043859.XU CN201720043859U CN206412478U CN 206412478 U CN206412478 U CN 206412478U CN 201720043859 U CN201720043859 U CN 201720043859U CN 206412478 U CN206412478 U CN 206412478U
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- grades
- steering
- antenna structure
- steering mechanism
- parabola
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- 230000002708 enhancing effect Effects 0.000 title claims abstract description 20
- 230000007246 mechanism Effects 0.000 claims abstract description 65
- 230000003321 amplification Effects 0.000 claims abstract description 18
- 238000003199 nucleic acid amplification method Methods 0.000 claims abstract description 18
- 238000003780 insertion Methods 0.000 claims abstract description 4
- 230000037431 insertion Effects 0.000 claims abstract description 4
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 4
- 229910052802 copper Inorganic materials 0.000 claims description 4
- 239000010949 copper Substances 0.000 claims description 4
- 230000000694 effects Effects 0.000 claims description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000002860 competitive effect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 239000003595 mist Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Abstract
The utility model discloses a kind of unmanned plane signal enhancing antenna structure, the antenna structure includes I grades of steering mechanism, II grades of steering mechanism, II grades of steering lock mechanisms, antenna body mechanism, parabola amplification board, the parabola amplification board has former and later two holes, one end of the antenna body mechanism is by former and later two described holes through the insertion parabola amplification board, connected between one end of the other end of the antenna body mechanism and the II grades of steering mechanism by the II grades of steering lock mechanism, the other end of the II grades of steering mechanism is connected with the I grades of steering mechanism again.The foldable parabola unmanned plane signal enhancing antenna structure of the utility model design, on the one hand can ensure the enhancing of unmanned plane antenna command range, on the other hand can quickly change antenna direction in time, make unmanned plane all the time within the scope of remote control.
Description
Technical field
The utility model design unmanned plane field, more particularly to foldable parabola unmanned plane signal enhancing antenna structure.
Background technology
At present, nobody, which rises, is widely used in each field such as civilian, commercial.More it is used for extreme sport, for items
Competitive sports are reported, for logistic industry, for shooting fan and wider market prospects, more next as audient
More new things, safer more reliable in the wide variety of spring tide of unmanned plane to ensure, unmanned plane antenna has widely
Development prospect.
During unmanned plane flight in the air, the accidents such as weather, cloud and mist, strong wind can be run into, especially to energy flying for long time
Unmanned plane, more need strengthen signal far distance controlled, and can in time launch/receive unmanned plane during flying direction instruction
Antenna Design.
The above is only used for auxiliary and understands the technical solution of the utility model, does not represent and recognizes that the above is existing
Technology.
Utility model content
Main purpose of the present utility model is to provide a kind of foldable unmanned plane signal enhancing antenna structure, it is intended to solve
The not enough technical problem turned to control direction not in time of command range faced during unmanned plane long-distance flight.
To achieve these goals, the utility model provides a kind of foldable unmanned plane signal enhancing antenna structure, institute
The foldable unmanned plane signal enhancing antenna structure of utility model：
A kind of unmanned plane signal enhancing antenna structure, the antenna structure include I grades of steering mechanism, II grades of steering mechanism,
II grades of steering lock mechanisms, antenna body mechanism, parabola amplification boards, the parabola amplification board have former and later two holes, institute
The insertion parabola amplification board, the antenna body machine are run through in the one end for stating antenna body mechanism by former and later two described holes
Connected between one end of the other end of structure and the II grades of steering mechanism by the II grades of steering lock mechanism, described II grades turns
It is connected again with the I grades of steering mechanism to the other end of mechanism.
Further, the parabola amplification board is copper facing parabola amplification board.
Further, the I grades of steering mechanism has 90 ° of steering capability.
Further, when the I grades of steering mechanism is not enough in use, the II grades of steering mechanism can by antenna structure and
When turn to reach required orientation in the range of 90 °.
Further, the remote control of the I grades of steering mechanism has corresponding steering blind area, the I grades of steering when turning to
Mechanism and the II grades of steering mechanism use cooperatively.
Further, the II grades of steering lock mechanism can according to the actual requirements, by the work of the II grades of steering mechanism
Dynamic property carries out lock locking/unlocking.
The beneficial effects of the utility model are mainly reflected in：
The utility model solves existing unmanned controller antenna towards single technical problem.The utility model is designed
Foldable parabola unmanned plane signal enhancing antenna structure, on the one hand can ensure the enhancing of unmanned plane antenna command range,
On the other hand it can quickly change antenna direction in time, make unmanned plane all the time within the scope of remote control.
Brief description of the drawings
Fig. 1 is the front elevation of the foldable unmanned plane signal enhancing antenna structure of the utility model.
Fig. 2 is the back view of the foldable unmanned plane signal enhancing antenna structure of the utility model.
Fig. 3 is the oblique view of the foldable unmanned plane signal enhancing antenna structure of the utility model.
Fig. 4 is the explosive view of the foldable unmanned plane signal enhancing antenna structure of the utility model.
1：I grades of steering mechanism；2：II grades of steering mechanism；3：II grades of steering lock mechanisms；4：Antenna body mechanism；5：Parabolic
Line amplification board
Embodiment
The specific implementation of the foldable unmanned plane signal enhancing antenna structure provided below in conjunction with the accompanying drawings the utility model
Mode elaborates.
As Figure 1-4, the foldable unmanned plane signal enhancing antenna structure includes I grades of steering mechanism 1, II grades of steerings
Mechanism 2, II grade steering lock mechanism 3, antenna body mechanism 4, parabola amplification board 5, parabola amplification board 5 have former and later two
Insertion copper facing parabola amplification board 5, antenna body machine are run through in hole, one end of antenna body mechanism 4 by former and later two described holes
Connected between one end of the other end and II grade steering mechanism 2 of structure 4 by II grades of steering lock mechanisms 3, the II grades of steering machine
The other end of structure 2 is connected with I grades of steering mechanism 1 again.The parabola amplification board 5 is copper facing parabola amplification board.
I grades of steering mechanism 1 remain traditional interface with remote control main frame, and remain its 90 ° of steering capability；When
I grades of steering mechanism's deficiencies are in use, II grades of steering mechanism can timely turn to antenna structure to reach in the range of 90 °
The orientation needed.
The remote control of I grades of steering mechanism has corresponding steering blind area when turning to, and the I level steering mechanism of design and II grades turn
Used cooperatively to mechanism, can in time, quickly realize that non-blind area is turned to.
The activity of II grades of steering mechanism can be carried out lock locking/unlocking by II grades of steering lock mechanisms according to the actual requirements,
The foldable unmanned plane signal enhancing antenna structure of the utility model is set to meet more flexible application demand.
Preferred embodiment of the present utility model is the foregoing is only, the numerical value mentioned in the description of description above
And number range is not limited to the utility model, simply provides preferred embodiment, be not used to for the utility model
The utility model is limited, for those skilled in the art, the utility model there can be various modifications and variations.It is all this
Within the spirit and principle of utility model, any modification, equivalent substitution and improvements made etc. should be included in the utility model
Protection domain within.
Claims (6)
1. a kind of unmanned plane signal enhancing antenna structure, the antenna structure includes I grades of steering mechanism, II grades of steering mechanism, II
Level steering lock mechanism, antenna body mechanism, parabola amplification board, the parabola amplification board have former and later two holes, described
One end of antenna body mechanism is by former and later two described holes through the insertion parabola amplification board, the antenna body mechanism
The other end and the II grades of steering mechanism one end between pass through the II grades of steering lock mechanism connect, it is described II grade turn to
The other end of mechanism is connected with the I grades of steering mechanism again.
2. antenna structure according to claim 1, it is characterised in that the parabola amplification board amplifies for copper facing parabola
Plate.
3. antenna structure according to claim 1 or 2, it is characterised in that the I grades of steering mechanism has 90 ° of steering
Ability.
4. antenna structure according to claim 1 or 2, it is characterised in that when the I grades of steering mechanism it is not enough in use,
The II grades of steering mechanism can timely turn to antenna structure to reach required orientation in the range of 90 °.
5. antenna structure according to claim 1 or 2, it is characterised in that the remote control of the I grades of steering mechanism is being turned to
When have corresponding steering blind area, the I grades of steering mechanism and the II grades of steering mechanism use cooperatively.
6. antenna structure according to claim 1 or 2, it is characterised in that the II grades of steering lock mechanism being capable of basis
Actual demand, lock locking/unlocking is carried out by the activity of the II grades of steering mechanism.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720043859.XU CN206412478U (en) | 2017-01-13 | 2017-01-13 | A kind of unmanned plane signal enhancing antenna structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720043859.XU CN206412478U (en) | 2017-01-13 | 2017-01-13 | A kind of unmanned plane signal enhancing antenna structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206412478U true CN206412478U (en) | 2017-08-15 |
Family
ID=59555228
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720043859.XU Expired - Fee Related CN206412478U (en) | 2017-01-13 | 2017-01-13 | A kind of unmanned plane signal enhancing antenna structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206412478U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106711606A (en) * | 2017-01-13 | 2017-05-24 | 深圳市天鼎微波科技有限公司 | Unmanned aerial vehicle signal enhancement antenna structure |
| CN110083169A (en) * | 2019-04-04 | 2019-08-02 | 上海歌尔泰克机器人有限公司 | Unmanned aerial vehicle control system, method, apparatus and electronic equipment |
-
2017
- 2017-01-13 CN CN201720043859.XU patent/CN206412478U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106711606A (en) * | 2017-01-13 | 2017-05-24 | 深圳市天鼎微波科技有限公司 | Unmanned aerial vehicle signal enhancement antenna structure |
| CN110083169A (en) * | 2019-04-04 | 2019-08-02 | 上海歌尔泰克机器人有限公司 | Unmanned aerial vehicle control system, method, apparatus and electronic equipment |
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170815 |