CN106711606A - Unmanned aerial vehicle signal enhancement antenna structure - Google Patents
Unmanned aerial vehicle signal enhancement antenna structure Download PDFInfo
- Publication number
- CN106711606A CN106711606A CN201710027294.0A CN201710027294A CN106711606A CN 106711606 A CN106711606 A CN 106711606A CN 201710027294 A CN201710027294 A CN 201710027294A CN 106711606 A CN106711606 A CN 106711606A
- Authority
- CN
- China
- Prior art keywords
- grades
- steering
- antenna structure
- steering mechanism
- parabola
- Prior art date
- 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.)
- Pending
Links
- 230000003321 amplification Effects 0.000 claims abstract description 18
- 238000003199 nucleic acid amplification method Methods 0.000 claims abstract description 18
- 230000002708 enhancing effect Effects 0.000 claims description 16
- 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
- 230000007812 deficiency Effects 0.000 claims description 3
- 238000003780 insertion Methods 0.000 claims description 3
- 230000037431 insertion Effects 0.000 claims description 3
- 230000000694 effects Effects 0.000 claims description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000002860 competitive effect Effects 0.000 description 1
- 238000005516 engineering process Methods 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
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q3/00—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
- H01Q3/02—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole
- H01Q3/08—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole for varying two co-ordinates of the orientation
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/36—Structural form of radiating elements, e.g. cone, spiral, umbrella; Particular materials used therewith
Abstract
The present invention discloses an unmanned aerial vehicle signal enhancement antenna structure. The antenna structure comprises an I-grade steering mechanism, an II-grade steering mechanism, an II-grade steering lock mechanism, an antenna main body mechanism and a parabola amplification board. The parabola amplification board has two holes at the front and the back, one end of the antenna main body mechanism runs through the parabola amplification board through the holes at the front and the back, the other end of the antenna main body mechanism is connected with one end of the II-grade steering mechanism through the II-grade steering lock mechanism, and the other end of the II-grade steering mechanism is connected with the I-grade steering mechanism. The foldable parabola unmanned aerial vehicle signal enhancement antenna structure can ensure that the enhancement of the antenna control distance of the unmanned aerial vehicle and timely and rapidly change the orientation of the antenna to allow the unmanned aerial vehicle to be always in the remote controller range.
Description
Technical field
Present invention design unmanned plane field, more particularly to foldable parabola unmanned plane signal enhancing antenna structure.
Background technology
At present, nobody rises and is widely used in each field such as civilian, commercial.More for extreme sport, for items
Competitive sports are reported, for logistic industry, for shooting fan and wider market prospects, it is more next as audient
More new things, for ensure the wide variety of spring tide of unmanned plane in it is safer more reliable, 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 technical scheme, does not represent and recognizes that the above is existing skill
Art.
The content of the invention
It is a primary object of the present invention to provide a kind of foldable unmanned plane signal enhancing antenna structure, it is intended to solve nobody
The not enough technical problem for being turned to control direction not in time of command range faced during machine long-distance flight.
To achieve these goals, the invention provides a kind of foldable unmanned plane signal enhancing antenna structure, invented
Foldable unmanned plane signal enhancing antenna structure：
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 mechanism, antenna body mechanism, parabola amplification board, the parabola amplification board have former and later two holes, institute
The one end for stating antenna body mechanism passes through described former and later two holes through the insertion parabola amplification board, the antenna body machine
Connected by the II grades of steering lock mechanism between one end of the other end of structure and the II grades of steering mechanism, described II grades turns
It is connected with the I grades of steering mechanism again 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 I grades of steering mechanism's deficiency is used, 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 are mainly as follows：
The present invention solves existing unmanned controller antenna towards single technical problem.It is foldable that the present invention is designed
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
Antenna direction can quickly be changed 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 foldable unmanned plane signal enhancing antenna structure of the invention.
Fig. 2 is the back view of foldable unmanned plane signal enhancing antenna structure of the invention.
Fig. 3 is the oblique view of foldable unmanned plane signal enhancing antenna structure of the invention.
Fig. 4 is the explosive view of foldable unmanned plane signal enhancing antenna structure of the invention.
1：I grades of steering mechanism；2：II grades of steering mechanism；3：II grades of steering lock mechanism；4：Antenna body mechanism；5：Parabolic
Line amplification board
Specific embodiment
The specific embodiment of the foldable unmanned plane signal enhancing antenna structure for providing the present invention below in conjunction with the accompanying drawings
Elaborate.
As Figure 1-4, the foldable unmanned plane signal enhancing antenna structure includes that I grades of steering mechanism 1, II grade turns to
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
Hole, one end of antenna body mechanism 4 passes through described former and later two holes through insertion copper facing parabola amplification board 5, antenna body machine
Connected by II grades of steering lock mechanism 3 between one end of the other end and II grade steering mechanism 2 of structure 4, 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 remains traditional interface with remote control main frame, and remains its 90 ° of steering capability；When
When I grades of steering mechanism's deficiency is used, II grades of steering mechanism can be timely turned to reach antenna structure in the range of 90 °
The orientation of needs.
The I grades of remote control of steering mechanism has corresponding steering blind area when turning to, and I grades of 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 II grades of activity of steering mechanism can be carried out lock locking/unlocking by II grades of steering lock mechanism according to the actual requirements,
Foldable unmanned plane signal enhancing antenna structure of the invention is set to meet more flexible application demand.
The preferred embodiments of the present invention are the foregoing is only, the numerical value and number mentioned in the description of description above
Value scope is not intended to limit the invention, and simply for the present invention is provided preferred embodiment, is not intended to limit the invention, right
For those skilled in the art, the present invention can have various modifications and variations.It is all within the spirit and principles in the present invention,
Any modification, equivalent substitution and improvements made etc., should be included within the scope of the present invention.
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 passes through described former and later two holes through the insertion parabola amplification board, the antenna body mechanism
The other end and one end of the II grades of steering mechanism between by 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 is that copper facing parabola amplifies
Plate.
3. antenna structure according to claim 1 and 2, it is characterised in that the I grades of steering mechanism has 90 ° of steering
Ability.
4. antenna structure according to claim 1 and 2, it is characterised in that when I grades of steering mechanism's deficiency is used,
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 and 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 and 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 |
|---|---|---|---|
| CN201710027294.0A CN106711606A (en) | 2017-01-13 | 2017-01-13 | Unmanned aerial vehicle signal enhancement antenna structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710027294.0A CN106711606A (en) | 2017-01-13 | 2017-01-13 | Unmanned aerial vehicle signal enhancement antenna structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106711606A true CN106711606A (en) | 2017-05-24 |
Family
ID=58907403
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710027294.0A Pending CN106711606A (en) | 2017-01-13 | 2017-01-13 | Unmanned aerial vehicle signal enhancement antenna structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106711606A (en) |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102956987A (en) * | 2011-08-31 | 2013-03-06 | 深圳光启高等理工研究院 | Signal enhancing structure and mobile multimedia broadcasting device |
| KR101424493B1 (en) * | 2014-02-26 | 2014-08-01 | 김현주 | DMB(Digital Multimedia Broadcasting) antenna |
| CN204315727U (en) * | 2014-12-31 | 2015-05-06 | 河北科技大学 | A kind of Navigation of Pilotless Aircraft antenna |
| CN104901894A (en) * | 2015-06-16 | 2015-09-09 | 四川分享微联科技有限公司 | Intelligent wireless network router |
| KR20160000541U (en) * | 2014-08-06 | 2016-02-16 | 백범석 | Antenna type camera that can be detachable to the mobile phone |
| CN205211913U (en) * | 2015-11-13 | 2016-05-04 | 中国人民解放军国防科学技术大学 | Collapsible syllogic quick assembly disassembly antenna frame |
| CN105789824A (en) * | 2016-04-05 | 2016-07-20 | 北京小米移动软件有限公司 | Remote control, antenna device of remote control and axial limiting structure thereof |
| CN205790344U (en) * | 2016-05-26 | 2016-12-07 | 深圳市根通通信技术有限公司 | A kind of unmanned plane beam antenna |
| CN206412478U (en) * | 2017-01-13 | 2017-08-15 | 深圳市天鼎微波科技有限公司 | A kind of unmanned plane signal enhancing antenna structure |
-
2017
- 2017-01-13 CN CN201710027294.0A patent/CN106711606A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102956987A (en) * | 2011-08-31 | 2013-03-06 | 深圳光启高等理工研究院 | Signal enhancing structure and mobile multimedia broadcasting device |
| KR101424493B1 (en) * | 2014-02-26 | 2014-08-01 | 김현주 | DMB(Digital Multimedia Broadcasting) antenna |
| KR20160000541U (en) * | 2014-08-06 | 2016-02-16 | 백범석 | Antenna type camera that can be detachable to the mobile phone |
| CN204315727U (en) * | 2014-12-31 | 2015-05-06 | 河北科技大学 | A kind of Navigation of Pilotless Aircraft antenna |
| CN104901894A (en) * | 2015-06-16 | 2015-09-09 | 四川分享微联科技有限公司 | Intelligent wireless network router |
| CN205211913U (en) * | 2015-11-13 | 2016-05-04 | 中国人民解放军国防科学技术大学 | Collapsible syllogic quick assembly disassembly antenna frame |
| CN105789824A (en) * | 2016-04-05 | 2016-07-20 | 北京小米移动软件有限公司 | Remote control, antenna device of remote control and axial limiting structure thereof |
| CN205790344U (en) * | 2016-05-26 | 2016-12-07 | 深圳市根通通信技术有限公司 | A kind of unmanned plane beam antenna |
| CN206412478U (en) * | 2017-01-13 | 2017-08-15 | 深圳市天鼎微波科技有限公司 | A kind of unmanned plane signal enhancing antenna structure |
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