CN205790344U - A kind of unmanned plane beam antenna - Google Patents
A kind of unmanned plane beam antenna Download PDFInfo
- Publication number
- CN205790344U CN205790344U CN201620497382.8U CN201620497382U CN205790344U CN 205790344 U CN205790344 U CN 205790344U CN 201620497382 U CN201620497382 U CN 201620497382U CN 205790344 U CN205790344 U CN 205790344U
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- Prior art keywords
- antenna
- box
- unmanned plane
- beam antenna
- frame
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Abstract
The utility model discloses a kind of unmanned plane beam antenna, including frame, driving means, machine box and beam antenna, described driving means is arranged on four corners of frame；Described driving means includes motor, propeller and anti-collision ring；Described propeller is arranged on motor top by power transmission shaft, and propeller periphery is fixed with anti-collision ring；Described machine box is fixed on frame central authorities, and described beam antenna includes antenna box and signal transmitting and receiving bar；Described signal transmitting and receiving bar is arranged on above antenna box by rotating connector；Horizontal angle sensor, luffing angle sensor and aerial position sensor it is provided with in described antenna box；Being provided with battery and control chip in described machine box, described control chip is electrically connected with driving means, horizontal angle sensor, luffing angle sensor and aerial position sensor respectively.This utility model compact conformation, lightweight, it is simple to carry, processing ease, low in energy consumption, the state of flight of unmanned plane can be apparent from.
Description
Technical field
This utility model relates to unmanned plane equipment technical field, is specially a kind of unmanned plane beam antenna.
Background technology
Unmanned plane enjoyed various countries to favor in the last few years at present, and it can be not only used for battlefield surveillance, gives warning in advance
Etc. military field, more have broad application prospects at civil area.It can carry high-resolution visible ray or red
Outer camera system, can easily enter the area that the mankind cannot arrive at and carry out aerial reconnaissance and aerophotography, can
To be used for carrying out mapping, disaster surveillance etc..
Traditional unmanned plane can not grasp the flight attitude of unmanned plane well, uniquely relies on the top in unmanned plane
Spiral shell instrument ensures not overturning of unmanned plane, and loses unmanned plane good tilt function.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane beam antenna, to solve in above-mentioned background technology
The problem proposed.
For achieving the above object, this utility model following technical scheme of offer: a kind of unmanned plane beam antenna,
Including frame, driving means, machine box and beam antenna, described driving means is arranged on four turnings of frame
Place；Described driving means includes motor, propeller and anti-collision ring；Described propeller is arranged on by power transmission shaft
Motor top, and propeller periphery is fixed with anti-collision ring；Described machine box is fixed on frame central authorities, and on machine box
Side is installed with beam antenna；Described beam antenna includes antenna box and signal transmitting and receiving bar；Described signal is received
Send out bar to be arranged on above antenna box by rotating connector；Be provided with in described antenna box horizontal angle sensor,
Luffing angle sensor and aerial position sensor；Battery and control chip it is provided with in described machine box, described
Control chip senses with driving means, horizontal angle sensor, luffing angle sensor and aerial position respectively
Device is electrically connected with.
Preferably, described frame side is provided with night flight lamp, and night flight lamp is electrically connected with control chip.
Preferably, described driving means is provided with four, and is distributed in frame four turning.
Preferably, described signal transmitting and receiving masthead end is provided with signal enhancing cap.
Preferably, it is installed with undercarriage bottom described frame, and undercarriage is at least provided with two.
Compared with prior art, the beneficial effects of the utility model are: this utility model has compact conformation,
Lightweight, it is easy to carry, processing ease, low in energy consumption, and can feed back unmanned plane constantly by location antenna
State of flight and flying distance, expand the scope of application of unmanned plane.
Accompanying drawing explanation
Fig. 1 is this utility model overall structure figure；
Fig. 2 is utility model works schematic diagram.
In reference: 1-frame；2-driving means；3-machine box；4-beam antenna；5-motor；6-spiral shell
Rotation oar；7-anti-collision ring；8-antenna box；9-signal transmitting and receiving bar；10-rotating connector；11-level angle passes
Sensor；12-luffing angle sensor；13-machine box；14-battery；15-control chip；16-night flight lamp；17-
Signal strengthens cap；18-undercarriage.
Detailed description of the invention
Below in conjunction with the accompanying drawing in this utility model embodiment, to the technical side in this utility model embodiment
Case is clearly and completely described, it is clear that described embodiment is only that this utility model part is real
Execute example rather than whole embodiments.Based on the embodiment in this utility model, ordinary skill people
The every other embodiment that member is obtained under not making creative work premise, broadly falls into this utility model
The scope of protection.
Refer to Fig. 1-2, a kind of embodiment that this utility model provides: a kind of unmanned plane beam antenna, bag
Including rack 1, driving means 2, machine box 3 and beam antenna 4, driving means 2 is arranged on four of frame 1
Corner；Driving means 2 includes motor 5, propeller 6 and anti-collision ring 7；Propeller 6 is pacified by power transmission shaft
It is contained in motor 5 top, and propeller 6 periphery is fixed with anti-collision ring 7；Machine box 3 is fixed on frame 1 central authorities,
And machine box 3 is fixed above is provided with beam antenna 4；Beam antenna 4 includes antenna box 8 and signal transmitting and receiving bar 9；
Signal transmitting and receiving bar 9 is arranged on above antenna box 8 by rotating connector 10；It is provided with level in antenna box 8
Angular transducer 11, luffing angle sensor 12 and aerial position sensor 13；It is provided with electricity in machine box 3
Pond 14 and control chip 15, control chip 15 respectively with driving means 2, horizontal angle sensor 11, bow
Face upward angular transducer 12 and aerial position sensor 13 is electrically connected with.
It is provided with night flight lamp 16 on frame 1 side, and night flight lamp 16 is electrically connected with control chip 15；Drive
Dynamic device 2 is provided with four, and is distributed in frame 1 four turning；Signal transmitting and receiving bar 9 top is provided with signal
Strengthen cap 17；It is installed with undercarriage 18 bottom frame 1, and undercarriage 18 is at least provided with two.
Operation principle: in utility model works, by the horizontal angle sensor 11 in antenna box 8, bows
Face upward angular transducer 12 and aerial position sensor 13 accurately reflect out unmanned plane during flying state and coordinate,
Power to each equipment by battery 14, receive data by geoceiver, and draw state of flight figure, root
Issue ensuing flight directive accordingly, by control chip 15 interpretive order, control driving means 2 with not
Same speed flight, thus reach the effect of positioning and directing.
It is obvious to a person skilled in the art that this utility model is not limited to the thin of above-mentioned one exemplary embodiment
Joint, and in the case of without departing substantially from spirit or essential attributes of the present utility model, it is possible to concrete with other
Form realizes this utility model.Therefore, no matter from the point of view of which point, embodiment all should be regarded as exemplary
, and be nonrestrictive, scope of the present utility model is limited by claims rather than described above
It is fixed, it is intended that all changes fallen in the implication of equivalency and scope of claim are included at this
In utility model.Should not be considered as limiting involved claim by any reference in claim.
Claims (5)
1. a unmanned plane beam antenna, including frame (1), driving means (2), machine box (3) and orientation
Antenna (4), it is characterised in that: described driving means (2) is arranged on four corners of frame (1)；
Described driving means (2) includes motor (5), propeller (6) and anti-collision ring (7)；Described propeller (6)
It is arranged on motor (5) top by power transmission shaft, and propeller (6) periphery is fixed with anti-collision ring (7)；Institute
State machine box (3) and be fixed on frame (1) central authorities, and machine box (3) is fixed above is provided with beam antenna (4)；
Described beam antenna (4) includes antenna box (8) and signal transmitting and receiving bar (9)；Described signal transmitting and receiving bar (9)
It is arranged on antenna box (8) top by rotating connector (10)；Described antenna box is provided with water in (8)
Flat angular transducer (11), luffing angle sensor (12) and aerial position sensor (13)；Described machine
Be provided with battery (14) and control chip (15) in box (3), described control chip (15) respectively with drive
Dynamic device (2), horizontal angle sensor (11), luffing angle sensor (12) and aerial position sensor
(13) it is electrically connected with.
A kind of unmanned plane beam antenna the most according to claim 1, it is characterised in that: described frame (1)
It is provided with night flight lamp (16) on side, and night flight lamp (16) is electrically connected with control chip (15).
A kind of unmanned plane beam antenna the most according to claim 1, it is characterised in that: described driving fills
Put (2) and be provided with four, and be distributed in frame (1) four turning.
A kind of unmanned plane beam antenna the most according to claim 1, it is characterised in that: described signal is received
Send out bar (9) top and signal enhancing cap (17) is installed.
A kind of unmanned plane beam antenna the most according to claim 1, it is characterised in that: described frame (1)
Bottom is installed with undercarriage (18), and undercarriage (18) is at least provided with two.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620497382.8U CN205790344U (en) | 2016-05-26 | 2016-05-26 | A kind of unmanned plane beam antenna |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620497382.8U CN205790344U (en) | 2016-05-26 | 2016-05-26 | A kind of unmanned plane beam antenna |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205790344U true CN205790344U (en) | 2016-12-07 |
Family
ID=57408394
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620497382.8U Expired - Fee Related CN205790344U (en) | 2016-05-26 | 2016-05-26 | A kind of unmanned plane beam antenna |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205790344U (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106314782A (en) * | 2016-10-22 | 2017-01-11 | 钟贵洪 | Remote control aerial camera |
| 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 |
| CN108232410A (en) * | 2017-12-28 | 2018-06-29 | 广州亿航智能技术有限公司 | A kind of aerial radiation direction regulator of unmanned plane |
| CN108615346A (en) * | 2017-05-05 | 2018-10-02 | 品尼高维斯塔有限责任公司 | Relay UAV system |
| CN108674677A (en) * | 2018-05-28 | 2018-10-19 | 河南农贝得农业科技有限公司 | A kind of dismountable unmanned plane anticollision damping device |
| EP3453615A4 (en) * | 2017-07-10 | 2019-03-20 | Autel Robotics Co., Ltd. | Antenna and unmanned aerial vehicle |
| US10707572B2 (en) | 2017-07-10 | 2020-07-07 | Autel Robotics Co., Ltd. | Antenna and unmanned aerial vehicle |
| CN114455085A (en) * | 2022-03-18 | 2022-05-10 | 成都科洛威尔科技有限公司 | Pitot tube heating alarm unit of general aircraft |
-
2016
- 2016-05-26 CN CN201620497382.8U patent/CN205790344U/en not_active Expired - Fee Related
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106314782A (en) * | 2016-10-22 | 2017-01-11 | 钟贵洪 | Remote control aerial camera |
| 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 |
| CN108615346A (en) * | 2017-05-05 | 2018-10-02 | 品尼高维斯塔有限责任公司 | Relay UAV system |
| CN108615346B (en) * | 2017-05-05 | 2021-12-24 | 上海峰飞航空科技有限公司 | Relay unmanned aerial vehicle system |
| EP3453615A4 (en) * | 2017-07-10 | 2019-03-20 | Autel Robotics Co., Ltd. | Antenna and unmanned aerial vehicle |
| US10707572B2 (en) | 2017-07-10 | 2020-07-07 | Autel Robotics Co., Ltd. | Antenna and unmanned aerial vehicle |
| CN108232410A (en) * | 2017-12-28 | 2018-06-29 | 广州亿航智能技术有限公司 | A kind of aerial radiation direction regulator of unmanned plane |
| CN108232410B (en) * | 2017-12-28 | 2021-06-25 | 广州亿航智能技术有限公司 | Antenna radiation direction regulator of unmanned aerial vehicle |
| CN108674677A (en) * | 2018-05-28 | 2018-10-19 | 河南农贝得农业科技有限公司 | A kind of dismountable unmanned plane anticollision damping device |
| CN114455085A (en) * | 2022-03-18 | 2022-05-10 | 成都科洛威尔科技有限公司 | Pitot tube heating alarm unit of general aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| 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: 20161207 Termination date: 20210526 |