CN205381411U - Born alarm device of unmanned aerial vehicle - Google Patents
Born alarm device of unmanned aerial vehicle Download PDFInfo
- Publication number
- CN205381411U CN205381411U CN201620123503.2U CN201620123503U CN205381411U CN 205381411 U CN205381411 U CN 205381411U CN 201620123503 U CN201620123503 U CN 201620123503U CN 205381411 U CN205381411 U CN 205381411U
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- rotating shaft
- born
- movable part
- alarm device
- unmanned plane
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Abstract
The utility model provides a born alarm device of unmanned aerial vehicle, belongs to the unmanned air vehicle technique field. Control panel, vertical location mechanism, alarm indicator and buzzer in including upper cover plate, casing, lower glass cover and arranging the casing in, control panel and the communication of vertical location mechanism set up alarm indicator and buzzer below the vertical location mechanism, and alarm indicator's light passes through glass cover trend of purchasing ground down, the born scope of demonstration unmanned aerial vehicle. The utility model designs a born alarm device of independent unmanned aerial vehicle installs accelerometer and gyroscope in, judge through the unmanned aerial vehicle flight data that accelerometer and gyroscope recorded whether unmanned aerial vehicle is in the state of falling out of control, and when alarm device confirmed that unmanned aerial vehicle is out of control, alarm device sent the buzzing alarm tone and reminds alarm device 0 to notice to built -in LED light source earthward throws the light beam and is used for indicateing the air crash place of estimating, reminds ground personnel to keep away from air crash point.
Description
Technical field
The invention belongs to unmanned air vehicle technique field, particularly relate to a kind of born alarm device of unmanned plane.
Background technology
From monitoring of taking photo by plane, remote sensing mapping, electric inspection process to agricultural plant protection, the use of unmanned plane is more and more universal.Unmanned plane also brings safety problem while being convenient for people to work and life.Unmanned plane causes falling due to unexpected, causes the situation that ground property loss is even hurted sb.'s feelings to happen occasionally.The unmanned plane released at present does not send alarm earthward when falling, with the device reminding the ground staff near the ground that falls to dodge in time.
Summary of the invention
For the technical problem of above-mentioned existence, the present invention provides a kind of born alarm device of unmanned plane, reminds ground staff away from air crash place.
It is an object of the invention to be achieved through the following technical solutions:
The born alarm device of one unmanned plane of the present invention, including upper cover plate, housing, lower-glass cover and be placed in the panel in housing, perpendicular positioning mechanism, alarm lamp and buzzer, panel and the communication of perpendicular positioning mechanism, perpendicular positioning mechanism is arranged below alarm lamp and buzzer, the light of alarm lamp invests ground by lower-glass cover, shows the born scope of unmanned plane.
Further, described perpendicular positioning mechanism includes movable part I, movable part II, rotating shaft I and rotating shaft II, movable part II both sides are respectively through rotating shaft II movable part connecting part I, the axis of rotating shaft I and rotating shaft II is orthogonal and in the same plane, alarm lamp and buzzer are arranged on below movable part II, and movable part I connects housing by two symmetrical rotating shafts I.
Further, described movable part II is eccentric structure, namely the center of gravity of movable part II with its on rotating shaft II axis not on the same line.
Further, described movable part II is groove structure.
Further, described movable part II is groove structure, and its web upper surface is lower than rotating shaft I and rotating shaft II place plane.
Further, described panel and the communication of perpendicular positioning mechanism are to conduct electric current by conductive plate, and movable part I inner wall section that the inner walls section that is connected with panel in perpendicular positioning mechanism rotating shaft I, rotating shaft II, rotating shaft I, rotating shaft I are connected with rotating shaft II, movable part II are installed the two ends of alarm lamp and buzzer and be respectively provided with conductive plate.
Further, described conductive plate is Copper Foil.
Further, described lower-glass cover is hemispherical bell glass.
Further, described upper cover plate is rounded, is provided with and fixes the mounting interface being connected with unmanned plane.
The invention have the benefit that
1. the present invention devises the born warning devices of independent unmanned plane, accelerometer and gyroscope are installed in warning devices, take into account, by acceleration, the unmanned plane during flying data that gyroscope records and judge whether unmanned plane is in fall condition out of control, when warning devices confirms that unmanned plane is out of control, warning devices sends buzzing alarming sound and reminds ground staff to note, and built-in LED light source projecting beam earthward is for indicating the air crash place of expectation, remind ground staff away from air crash point.
2. the present invention can be manually booted by remote controller, it is possible to starts voluntarily when unmanned plane is born.
Even if 3. the present invention exists swing situation in unmanned plane drop event, unmanned plane still can be accurately indicated to fall place.
Accompanying drawing explanation
Fig. 1 is the structural representation of the present invention.
Fig. 2 is conductivity principle schematic diagram of the present invention.
Fig. 3 is the perpendicular positioning structural scheme of mechanism in Fig. 1.
Fig. 4 is perpendicular positioning mechanism of the present invention attachment structure schematic diagram.
In figure: 1. upper cover plate, 2. panel, 3. housing, 4. conductive plate, 5. perpendicular positioning mechanism, 51. movable parts I, 52. movable parts II, 53. rotating shafts I, 54. rotating shafts II, 55. webs, 6. lower-glass
Cover, 7. alarm lamp, 8. buzzer.
Detailed description of the invention
Describe the present invention below in conjunction with drawings and Examples.
Embodiment: as shown in Figure 1, the born alarm device of one unmanned plane of the present invention, including upper cover plate 1, housing 3, lower-glass cover 6 and be placed in the panel 2 in housing 3, perpendicular positioning mechanism 5, alarm lamp 7 and buzzer 8, panel 2 and perpendicular positioning mechanism 5 communication, perpendicular positioning mechanism 5 is arranged below alarm lamp 7 and buzzer 8, the light of alarm lamp 7 invests ground by lower-glass cover 6, shows the born scope of unmanned plane.
As shown in Figure 3, described perpendicular positioning mechanism 5 includes movable part I 51, movable part II 52, rotating shaft I 53 and rotating shaft II 54, movable part II 52 both sides are respectively through rotating shaft II 54 movable part connecting part I 51, alarm lamp 7 and buzzer 8 are arranged on below movable part II 52, and movable part I 51 connects housing 3 by two symmetrical rotating shafts I 53.
Described movable part II 52 is eccentric structure, namely the center of gravity of movable part II 52 with its on rotating shaft II 54 axis not on the same line.
Described movable part II 52 is groove structure.
Web 55 upper surface of described movable part II 52 is lower than rotating shaft I 53 and rotating shaft II 54 place plane.
As shown in Figure 2, described panel 2 and perpendicular positioning mechanism 5 communication are to conduct electric current by conductive plate, and the two ends of movable part I 52 inner wall section, movable part II 52 installation alarm lamp 7 and buzzer 8 that housing 3 inner wall section that is connected with panel 2 in perpendicular positioning mechanism rotating shaft I 53, rotating shaft II 54, rotating shaft I 53, rotating shaft I 53 are connected with rotating shaft II 54 are respectively provided with conductive plate.Described conductive plate is Copper Foil.
Described lower-glass cover 6 is hemispherical bell glass, makes device internal element be isolated from the outside.Described upper cover plate 1 is rounded, which is provided with and fixes the mounting interface being connected with unmanned plane.The coalition shape of hemisphere and cylinder is formed after the whole device combination of the present invention.It is integral that housing 3 threadeds formation with upper cover plate 1.Panel 2 mounting platform and current conduction plate mounting groove is had in housing 3.
Panel 2 of the present invention is provided with acceleration gyroscope, 2.4G wireless module, main control chip and battery.Panel 2 can receive the wireless signal that remote controller sends.When unmanned plane is out of control fall time, transmit a signal to panel 2 by ground remote controller, panel 2 is handled and is opened alarm lamp 7 and the switch of buzzer 8, alarm lamp 7 and buzzer 8 and start working.But the unmanned plane during flying data that panel 2 also oneself gathers, analyze again and judge whether unmanned plane is in fall condition out of control, when judging that unmanned plane is for fall condition out of control, manipulation is opened alarm lamp 7 and the switch of buzzer 8, alarm lamp 7 and buzzer 8 and is started working by panel 2.Panel 2 is provided with battery for element on panel.
Alarm lamp 7 and buzzer 8 are arranged in vertical orientation mechanism 5, as shown in Figure 4.When vertical orientation mechanism 5 is capable of unmanned plane random swing, the light beam that alarm lamp 7 is launched is straight down always.Vertical orientation mechanism 5 operation principle is as described below: as it is shown on figure 3, vertical orientation mechanism 5 by two movable parts and and two rotating shafts form, movable part I 51, in annular, is arranged on housing 3 sidewall by rotating shaft I 53, can be I 53 freely rotatable around the shaft；Movable part II 52 is arranged on movable part I 51 by rotating shaft II 54, can be II 54 freely rotatable around the shaft；The axis of rotating shaft I 53 and rotating shaft II 54 is orthogonal and in the same plane；Movable part II 52 is bathtub construction, and two flanges of bathtub construction are used for connection rotating shaft II 54, and the web 55 of flute profile, as the mounting platform of functional unit, is used for installing alarm lamp 7 and buzzer 8；Corrugation web 55 (i.e. the mounting platform of the functional unit) upper surface of movable part II 52 is lower than rotating shaft I 53 and rotating shaft II 54 place plane；When there is certain specific rotation in housing, under gravity, movable part I 51 I 53 turns an angle around the shaft, movable part II 52 II 54 turns an angle around the shaft, twice rotation couple, it is ensured that the alarm lamp 7 being arranged on movable part II 52 corrugation web 55 bottom surface can automatically keep vertically downward towards.
The current conducting path of the present invention is: battery=on panel > Copper Foil conductive plate=in housing sidewall > rotating shaft I 53 Copper Foil conductive plate=> Copper Foil conductive plate=on movable part I 51 > Copper Foil conductive plate=in rotating shaft II 54 > Copper Foil conductive plate=on movable part 2 > alarm lamp and buzzer, this conducting path realizes the function that fixing parts are powered to movable part, avoid the freely-movable of wire influence movable part simultaneously, simple for structure.
Claims (9)
1. the born alarm device of unmanned plane, it is characterized in that: include upper cover plate, housing, lower-glass cover and the panel being placed in housing, perpendicular positioning mechanism, alarm lamp and buzzer, panel and the communication of perpendicular positioning mechanism, perpendicular positioning mechanism is arranged below alarm lamp and buzzer, the light of alarm lamp invests ground by lower-glass cover, shows the born scope of unmanned plane.
2. the born alarm device of unmanned plane according to claim 1, it is characterized in that: described perpendicular positioning mechanism includes movable part I, movable part II, rotating shaft I and rotating shaft II, movable part II both sides are respectively through rotating shaft II movable part connecting part I, the axis of rotating shaft I and rotating shaft II is orthogonal and in the same plane, alarm lamp and buzzer are arranged on below movable part II, and movable part I connects housing by two symmetrical rotating shafts I.
3. the born alarm device of unmanned plane according to claim 2, it is characterised in that: described movable part II is eccentric structure, namely the center of gravity of movable part II with its on rotating shaft II axis not on the same line.
4. the born alarm device of unmanned plane according to claim 3, it is characterised in that: described movable part II is groove structure.
5. the born alarm device of unmanned plane according to claim 4, it is characterised in that: described movable part II is groove structure, and its web upper surface is lower than rotating shaft I and rotating shaft II place plane.
6. the born alarm device of unmanned plane according to claim 1 or claim 2, it is characterized in that: described panel and the communication of perpendicular positioning mechanism are to conduct electric current by conductive plate, movable part I inner wall section that the inner walls section that is connected with panel in perpendicular positioning mechanism rotating shaft I, rotating shaft II, rotating shaft I, rotating shaft I are connected with rotating shaft II, movable part II are installed the two ends of alarm lamp and buzzer and are respectively provided with conductive plate.
7. the born alarm device of unmanned plane according to claim 6, it is characterised in that: described conductive plate is Copper Foil.
8. the born alarm device of unmanned plane according to claim 1, it is characterised in that: described lower-glass cover is hemispherical bell glass.
9. the born alarm device of unmanned plane according to claim 1, it is characterised in that: described upper cover plate is rounded, is provided with and fixes the mounting interface being connected with unmanned plane.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620123503.2U CN205381411U (en) | 2016-02-17 | 2016-02-17 | Born alarm device of unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620123503.2U CN205381411U (en) | 2016-02-17 | 2016-02-17 | Born alarm device of unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205381411U true CN205381411U (en) | 2016-07-13 |
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ID=56350525
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620123503.2U Expired - Fee Related CN205381411U (en) | 2016-02-17 | 2016-02-17 | Born alarm device of unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205381411U (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107063755A (en) * | 2017-05-29 | 2017-08-18 | 四川沃洛佳科技有限公司 | A kind of unmanned plane water sampling method |
| WO2018059017A1 (en) * | 2016-09-29 | 2018-04-05 | 上海华测导航技术股份有限公司 | Anti-fall protection and anti-loss apparatus for unmanned aerial vehicle |
| WO2018076467A1 (en) * | 2016-10-31 | 2018-05-03 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle and alarm system thereof |
| CN109683164A (en) * | 2019-01-25 | 2019-04-26 | 西南科技大学 | A kind of unmanned plane based on flying quality falls Activity recognition method |
| CN109754548A (en) * | 2018-12-24 | 2019-05-14 | 天津航天中为数据系统科技有限公司 | A kind of unmanned plane locator tracing system with removable acousto-optic cigarette alarm |
| CN110546071A (en) * | 2018-12-26 | 2019-12-06 | 乐天株式会社 | Unmanned aerial vehicle, reporter, flight vehicle, and reporter release device |
| WO2021043331A1 (en) * | 2019-09-03 | 2021-03-11 | 深圳市道通智能航空技术有限公司 | Aircraft alarm method and device, and aircraft |
| CN112700617A (en) * | 2020-12-21 | 2021-04-23 | 北京二郎神科技有限公司 | Aircraft early warning method and device, electronic equipment and readable storage medium |
-
2016
- 2016-02-17 CN CN201620123503.2U patent/CN205381411U/en not_active Expired - Fee Related
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018059017A1 (en) * | 2016-09-29 | 2018-04-05 | 上海华测导航技术股份有限公司 | Anti-fall protection and anti-loss apparatus for unmanned aerial vehicle |
| CN107884777A (en) * | 2016-09-29 | 2018-04-06 | 上海华测导航技术股份有限公司 | A kind of shatter-resistant protection and loss prevention device for unmanned plane |
| WO2018076467A1 (en) * | 2016-10-31 | 2018-05-03 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle and alarm system thereof |
| CN107063755A (en) * | 2017-05-29 | 2017-08-18 | 四川沃洛佳科技有限公司 | A kind of unmanned plane water sampling method |
| CN107063755B (en) * | 2017-05-29 | 2023-05-05 | 四川沃洛佳科技有限公司 | Unmanned aerial vehicle water sample collection method |
| CN109754548A (en) * | 2018-12-24 | 2019-05-14 | 天津航天中为数据系统科技有限公司 | A kind of unmanned plane locator tracing system with removable acousto-optic cigarette alarm |
| CN110546071A (en) * | 2018-12-26 | 2019-12-06 | 乐天株式会社 | Unmanned aerial vehicle, reporter, flight vehicle, and reporter release device |
| CN109683164A (en) * | 2019-01-25 | 2019-04-26 | 西南科技大学 | A kind of unmanned plane based on flying quality falls Activity recognition method |
| WO2021043331A1 (en) * | 2019-09-03 | 2021-03-11 | 深圳市道通智能航空技术有限公司 | Aircraft alarm method and device, and aircraft |
| CN112700617A (en) * | 2020-12-21 | 2021-04-23 | 北京二郎神科技有限公司 | Aircraft early warning method and device, electronic equipment and readable storage medium |
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Legal Events
| Date | Code | Title | Description |
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| 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: 20160713 Termination date: 20190217 |