CN107196035A - A kind of rotary plate antenna structure - Google Patents
A kind of rotary plate antenna structure Download PDFInfo
- Publication number
- CN107196035A CN107196035A CN201710324663.2A CN201710324663A CN107196035A CN 107196035 A CN107196035 A CN 107196035A CN 201710324663 A CN201710324663 A CN 201710324663A CN 107196035 A CN107196035 A CN 107196035A
- Authority
- CN
- China
- Prior art keywords
- grades
- steering mechanism
- steering
- antenna structure
- rotary plate
- 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
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Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/08—Means for collapsing antennas or parts thereof
- H01Q1/084—Pivotable antennas
Landscapes
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The invention discloses a kind of rotary plate 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, double treadmill bodies, described pair of treadmill body is rotatable successively, be collapsibly installed on one end of the antenna body mechanism, 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 present invention can effectively strengthen no-manned machine distant control signal intensity；Unmanned plane antenna direction can be changed in time, make unmanned plane all the time within controlled range；Folding storage can be carried out to remote control double flat plate, reduce double slab construction space-consumings.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, more particularly to a kind of unmanned plane antenna structure.
Background technology
Currently, unmanned plane is applied to each field such as civilian, commercial more and more widely, is especially more used for the limit and transports
Move, for being reported every competitive sports, for logistic industry, for shooting before fan and wider market
Scape, as the increasing new things of audient, to ensure safer more reliable, unmanned plane in the wide variety of spring tide of unmanned plane
Antenna has extensive development prospect.
Certainly, the accidents such as weather, cloud and mist, strong wind can be run into during unmanned plane flight in the air, especially to energy for a long time
The unmanned plane of flight, more needs to strengthen the far distance controlled of signal, and can launch/receive unmanned plane during flying direction in time
The Antenna Design of instruction.
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 rotary plate antenna structure, it is intended to solve unmanned plane long-distance flight
When the not enough technical problem turned to control direction not in time of the command range that faces.
To achieve these goals, the invention provides a kind of rotary plate antenna structure：The antenna structure includes I grades
Steering mechanism, II grades of steering mechanism, II grades of steering lock mechanisms, antenna body mechanism, double treadmill bodies, described pair of treadmill body
One end that is rotatable successively, being collapsibly installed on the antenna body mechanism, the other end of the antenna body mechanism and institute
State between one end of II grades of steering mechanism and to be connected by the II grades of steering lock mechanism, the other end of the II grades of steering mechanism
It is connected again with the I grades of steering mechanism.
Further, described pair of treadmill body rotates from 0 ° to 180 °, can rotary folding be completely superposed, coordinate multiple antennas
Use.
Further, the I grades of steering mechanism 1 and II grades of steering mechanism can rotate freely in 90 °.
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 are mainly as follows：
The present invention coordinates the Patcho antenna (referred to as double treadmill bodies) of the rotatable double flat plate of large area by single antenna effectively
Strengthen no-manned machine distant control signal intensity；Unmanned plane antenna direction can be changed in time, make unmanned plane all the time within controlled range；Energy
It is enough that folding storage is carried out to remote control double flat plate, reduce double slab construction space-consumings.
Brief description of the drawings
Fig. 1 is the explosive view of inventive antenna structure.
Fig. 2 is the front elevation of inventive antenna structure.
Fig. 3 is the steering schematic diagram of inventive antenna structure.
Fig. 4 is the rotation schematic diagram of inventive antenna structure (scope is from 0 ° to 180 °).
1：I grades of steering structures；2：II grades of steering mechanism；3：II grades of steering lock mechanisms；4：Antenna body mechanism；5：Double flat
Trigger structure
Embodiment
The embodiment of the antenna structure provided below in conjunction with the accompanying drawings the present invention elaborates.
As Figure 1-4, the rotary plate antenna structure include I grade steering mechanism 1, II grades of steering mechanism 2, II grades turns
To locking mechanism 3, antenna body mechanism 4, double treadmill bodies 5, described pair of treadmill body 5 is rotatable successively, collapsibly install
Pass through II grades between one end of antenna body mechanism 4, one end of the other end and II grade steering mechanism 2 of antenna body mechanism 4
Steering lock mechanism 3 is connected, and the other end of the II grades of steering mechanism 2 is connected with I grades of steering mechanism 1 again.I grades of steering mechanism 1
It can be rotated freely with II grades of steering mechanism 2 in 90 °；II grades of steering lock mechanisms 3 are free to II grades of unlock/lock and turned
To mechanism 2；Folding locking/unlocking mechanism is devised in II grades of steering mechanism 2, the foldable work(of unmanned plane antenna is realized
Energy.
Dual platen on individual antenna, which can be realized from 0 ° to 180 °, to be rotated, and rotary folding is completely superposed, and coordinates multiple antennas
Use, its signal receiving area can be greatly increased for the remote control of multiple antennas.
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,
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 is simply provided preferred embodiment, is not intended to limit the invention for the present invention, right
For those skilled in the art, the present invention can have various modifications and variations.Within the spirit and principles of the invention,
Any modification, equivalent substitution and improvements made etc., should be included in the scope of the protection.
Claims (6)
1. a kind of rotary plate antenna structure, the antenna structure includes I grades of steering mechanism, II grades of steering mechanism, II grades of steerings
Locking mechanism, antenna body mechanism, double treadmill bodies, described pair of treadmill body is rotatable successively, be collapsibly installed on described
Pass through institute between one end of one end of antenna body mechanism, the other end of the antenna body mechanism and the II grades of steering mechanism
II grades of steering lock mechanism connections are stated, the other end of the II grades of steering mechanism is connected with the I grades of steering mechanism again.
2. rotary plate antenna structure according to claim 1, it is characterised in that described pair of treadmill body is from 0 ° to 180 °
Rotation, can rotary folding be completely superposed, coordinate multiple antennas use.
3. rotary plate antenna structure according to claim 1 or 2, it is characterised in that the I grades of steering mechanism 1 and II
Level steering mechanism can rotate freely in 90 °.
4. rotary plate antenna structure according to claim 1 or 2, it is characterised in that when the I grades of steering mechanism 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. rotary plate antenna structure according to claim 1 or 2, it is characterised in that the remote control of the I grades of steering mechanism
Device has corresponding steering blind area when turning to, and the I grades of steering mechanism and the II grades of steering mechanism use cooperatively.
6. rotary plate antenna structure according to claim 1 or 2, it is characterised in that the II grades of steering lock mechanism
The activity of the II grades of steering mechanism can be subjected to lock locking/unlocking according to the actual requirements.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710324663.2A CN107196035A (en) | 2017-05-09 | 2017-05-09 | A kind of rotary plate antenna structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710324663.2A CN107196035A (en) | 2017-05-09 | 2017-05-09 | A kind of rotary plate antenna structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107196035A true CN107196035A (en) | 2017-09-22 |
Family
ID=59873848
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710324663.2A Pending CN107196035A (en) | 2017-05-09 | 2017-05-09 | A kind of rotary plate antenna structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107196035A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2019095770A1 (en) * | 2017-11-17 | 2019-05-23 | 深圳市道通智能航空技术有限公司 | Antenna device, and remote controller and unmanned aerial vehicle assembly having same |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201682042U (en) * | 2010-03-12 | 2010-12-22 | 深圳市海生机房技术有限公司 | Folded antenna |
| CN102931487A (en) * | 2012-11-26 | 2013-02-13 | 江苏联海通信技术有限公司 | Rotatable billboard type beautifying antenna |
| 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 |
| CN105742780A (en) * | 2016-04-25 | 2016-07-06 | 东莞思谷数字技术有限公司 | Radio frequency identification (RFID) flexible bending type adjustable antenna |
-
2017
- 2017-05-09 CN CN201710324663.2A patent/CN107196035A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201682042U (en) * | 2010-03-12 | 2010-12-22 | 深圳市海生机房技术有限公司 | Folded antenna |
| CN102931487A (en) * | 2012-11-26 | 2013-02-13 | 江苏联海通信技术有限公司 | Rotatable billboard type beautifying antenna |
| 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 |
| CN105742780A (en) * | 2016-04-25 | 2016-07-06 | 东莞思谷数字技术有限公司 | Radio frequency identification (RFID) flexible bending type adjustable antenna |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2019095770A1 (en) * | 2017-11-17 | 2019-05-23 | 深圳市道通智能航空技术有限公司 | Antenna device, and remote controller and unmanned aerial vehicle assembly having same |
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