CN204998781U - Take unmanned aerial vehicle of solar thin film battery - Google Patents
Take unmanned aerial vehicle of solar thin film battery Download PDFInfo
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- CN204998781U CN204998781U CN201520583250.2U CN201520583250U CN204998781U CN 204998781 U CN204998781 U CN 204998781U CN 201520583250 U CN201520583250 U CN 201520583250U CN 204998781 U CN204998781 U CN 204998781U
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Abstract
The utility model relates to a take unmanned aerial vehicle of solar thin film battery, including fuselage, wing and fin, fuselage internally mounted is equipped with battery, the control unit and remote control unit, wing and fin have coated the solar thin film battery, the solar thin film battery passes through the wire and connects in parallel at the positive and negative both ends of battery formation power supply circuit, the control unit includes selecting arrangement, PCB circuit board, wireless communication module, data processing module and sensor, solar thin film battery and battery are connected simultaneously to selecting arrangement's one end, and the other end links to each other with PCB circuit board, wireless communication module and ground basic station wireless connection, wireless communication module and data processing module all set up on PCB circuit board, the sensor includes gravity sensor, three -axis gyroscope and ground magnetic sensor. The utility model discloses, the redundant backup of battery had both been realized, the too big problem of fuselage quality that has caused when having avoided again adopting the double cell among the prior art.
Description
Technical field
The utility model relates to unmanned air vehicle technique field, particularly a kind of unmanned aerial vehicle with solar film battery.
Background technology
Robot airplane, is called for short unmanned plane (UAV), is a kind ofly to be in the equipment of the new concept weapon in developing rapidly, its have maneuverability, reaction fast, unmanned flight, advantage that operation requirements is low.Unmanned plane, by carrying multiclass sensor, can realize image real-time Transmission, high-risk areas detecting function, is that satellite remote sensing and the strong of traditional air remote sensing supplement.At present, the range of use of unmanned plane has widened military affairs, scientific research, civilian three large fields, specifically in electric power, communication, meteorology, agricultural, ocean, exploration, photograph, prevent and reduce natural disasters, Crop Estimation, drug law enforcement anti-smuggling, border patrol, the field application such as public security anti-terrorism be very wide.Wherein, unmanned plane mainly comprises fuselage, power system and some function devices (equipment etc. of such as taking photo by plane).Power system comprises motor and battery, in order to ensure not because battery failures causes air crash, all adopts double cell to carry out backup power supply in a lot of unmanned plane.Existing unmanned plane power system mainly adopts large-capacity battery, when using dual battery system, causing unmanned plane overall weight comparatively large, consuming energy high.
Summary of the invention
The purpose of this utility model is the defect overcoming prior art existence, and provide a kind of structure simple, transformation is convenient, the unmanned aerial vehicle of lightweight band solar film battery.
The technical scheme realizing the utility model object is: a kind of unmanned aerial vehicle with solar film battery, comprise fuselage, wing and empennage, described fuselage interior is installed and is provided with storage battery, control unit and RCU, described wing and empennage are covered with solar film battery, described solar film battery forms power circuit by conductor in parallel at the positive and negative two ends of storage battery, described control unit comprises selecting arrangement, PCB, wireless communication module, data processing module and sensor, one end of described selecting arrangement connects solar film battery and storage battery simultaneously, the other end is connected with PCB, described wireless communication module is connected with ground base station wireless telecommunications, wireless communication module and data processing module are all arranged in PCB, described sensor comprises weight sensor, three-axis gyroscope and geomagnetic sensor.
Power circuit described in technique scheme is parallel with voltage sensor, the input end of the mouth connection control unit of described voltage sensor.
Selecting arrangement described in technique scheme is made up of the branch circuit parallel connection that two are connected by select switch and time delay disconnection relay.
After adopting technique scheme, the utility model has following positive effect:
(1) the utility model, had both achieved the redundancy backup of battery, turn avoid in prior art the problem that the fuselage quality that causes when adopting double cell is excessive.
(2) power circuit of the present utility model is parallel with voltage sensor, the input end of the mouth connection control unit of described voltage sensor.By voltage sensor measuring voltage, feed back to control processor, thus Switching power, extend the flying power of unmanned plane.
Accompanying drawing explanation
In order to make content of the present utility model more easily be clearly understood, below according to specific embodiment also by reference to the accompanying drawings, the utility model is described in further detail, wherein
Fig. 1 is structural representation of the present utility model;
Fig. 2 is schematic diagram of the present utility model;
Attached number in the figure is: fuselage 1, wing 2, empennage 3, storage battery 4, control unit 5, RCU 6, solar film battery 7, selecting arrangement 8, PCB 9, wireless communication module 10, data processing module 11, sensor 12, ground base station 13, voltage sensor 14, select switch 15, time delay disconnect relay 16.
Detailed description of the invention
(embodiment 1)
See Fig. 1, the utility model comprises fuselage 1, wing 2 and empennage 3, fuselage 1 inside is installed and is provided with storage battery 4, control unit 5 and RCU 6, wing 2 and empennage 3 are covered with solar film battery 7, solar film battery 7 forms power circuit by conductor in parallel at the positive and negative two ends of storage battery 4, control unit 5 comprises selecting arrangement 8, PCB 9, wireless communication module 10, data processing module 11 and sensor 12, one end of selecting arrangement 8 connects solar film battery 7 and storage battery 4 simultaneously, the other end is connected with PCB 9, wireless communication module 10 is connected with ground base station 13 wireless telecommunications, wireless communication module 10 and data processing module 11 are all arranged in PCB 9, sensor 12 comprises weight sensor, three-axis gyroscope and geomagnetic sensor.
Power circuit is parallel with voltage sensor 14, the input end of the mouth connection control unit 5 of voltage sensor 14.
Selecting arrangement 8 is made up of the branch circuit parallel connection that two are connected by select switch 15 and time delay disconnection relay 16.
Above-described specific embodiment; the purpose of this utility model, technical scheme and beneficial effect are further described; be understood that; the foregoing is only specific embodiment of the utility model; be not limited to the utility model; all within spirit of the present utility model and principle, any amendment made, equivalent replacement, improvement etc., all should be included within protection domain of the present utility model.
Claims (3)
1. the unmanned aerial vehicle with solar film battery, comprise fuselage (1), wing (2) and empennage (3), described fuselage (1) inside is installed and is provided with storage battery (4), control unit (5) and RCU (6), it is characterized in that: described wing (2) and empennage (3) are covered with solar film battery (7), described solar film battery (7) forms power circuit by conductor in parallel at the positive and negative two ends of storage battery (4), described control unit (5) comprises selecting arrangement (8), PCB (9), wireless communication module (10), data processing module (11) and sensor (12), one end of described selecting arrangement (8) connects solar film battery (7) and storage battery (4) simultaneously, the other end is connected with PCB (9), described wireless communication module (10) is connected with ground base station (13) wireless telecommunications, wireless communication module (10) and data processing module (11) are all arranged in PCB (9), described sensor (12) comprises weight sensor, three-axis gyroscope and geomagnetic sensor.
2. the unmanned aerial vehicle of band solar film battery according to claim 1, it is characterized in that: described power circuit is parallel with voltage sensor (14), the input end of the mouth connection control unit (5) of described voltage sensor (14).
3. the unmanned aerial vehicle of band solar film battery according to claim 1, is characterized in that: described selecting arrangement (8) is made up of the branch circuit parallel connection that two are connected by select switch (15) and time delay disconnection relay (16).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520583250.2U CN204998781U (en) | 2015-08-06 | 2015-08-06 | Take unmanned aerial vehicle of solar thin film battery |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520583250.2U CN204998781U (en) | 2015-08-06 | 2015-08-06 | Take unmanned aerial vehicle of solar thin film battery |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204998781U true CN204998781U (en) | 2016-01-27 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520583250.2U Active CN204998781U (en) | 2015-08-06 | 2015-08-06 | Take unmanned aerial vehicle of solar thin film battery |
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| Country | Link |
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| CN (1) | CN204998781U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2022132008A (en) * | 2021-02-26 | 2022-09-07 | 均 石井 | Battery for hybrid-type electric airplane |
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2015
- 2015-08-06 CN CN201520583250.2U patent/CN204998781U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2022132008A (en) * | 2021-02-26 | 2022-09-07 | 均 石井 | Battery for hybrid-type electric airplane |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |