CN104460682A - Unmanned aerial vehicle with wireless stereo function - Google Patents
Unmanned aerial vehicle with wireless stereo function Download PDFInfo
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- CN104460682A CN104460682A CN201410586066.3A CN201410586066A CN104460682A CN 104460682 A CN104460682 A CN 104460682A CN 201410586066 A CN201410586066 A CN 201410586066A CN 104460682 A CN104460682 A CN 104460682A
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Abstract
The invention relates to an unmanned aerial vehicle with the wireless stereo function. The unmanned aerial vehicle comprises an aerial vehicle body, a power supply module, rotor wing arms, motors, an undercarriage, an unmanned aerial vehicle controller and a wireless stereo system, wherein the power supply module is formed by mutually connecting a charging circuit and a battery capable of being charged repeatedly, the rotor wing arms are fixedly connected with the aerial vehicle body, each motor with one impeller blade is arranged on the corresponding rotor wing arm, the undercarriage is arranged at the bottom of the aerial vehicle body and fixedly connected with the aerial vehicle body, the unmanned aerial vehicle controller is arranged in the body and connected with the motors on the rotor wing arms, and the wireless stereo system is combined with the unmanned aerial vehicle. The unmanned aerial vehicle with the wireless stereo function can fast fly to a certain broadcast height when used, broadcast information in real time to the position below a flight region within the distance range from 300 meters to the farthest voyage of the unmanned aerial vehicle generally according to the used wireless audio transmission mode, and fast and clearly transmit the information and has an excellent information broadcast effect.
Description
Technical field
The present invention relates to a kind of unmanned vehicle, particularly relate to a kind of unmanned vehicle carrying wireless acoustics function.
Background technology
In the occasion that some are special, such as stage or square are performed, or at more corresponding accidents such as earthquake relief, or when evacuating personnel, people often use various loudspeakers to dredge the stream of people, or real-time information is provided, information comparatively is accurately obtained with the personnel in the scene of safeguarding or help disaster area, but under present circumstances when disaster occurs, because the power supply in buildings often also can along with breaking down, therefore information is easily caused to transmit in time, the sound being located at the loudspeaker on the automobile of movement is relatively little, therefore on-the-spot people are caused to obtain tutorial message, thus result in the delay of information, larger loss is caused to the disaster relief, at present along with the more and more maturation of various technology, current many rotor unmanned aircrafts, all there is structure simple, state of flight is stablized and is easy to the feature of manipulation, in addition along with the development of battery technology, the capacity of current battery is increasing, battery standby time is more and more longer, the hang time of many rotor unmanned aircrafts usually can more than several hours, usually with many rotor unmanned aircrafts of more battery, often can hover more than more than 5 hours on specific height, if load and rely on some small-sized low noise fuel electric generators, the aerial hold-up time of many rotor unmanned aircrafts is even longer, the longer stagnant empty hover time, can give unmanned vehicle more feasible applications, if unmanned vehicle and wireless impression are be combined with each other, unmanned vehicle is broadcasted people in high-altitude, just can realize transmitting clearly fast of acoustic information, thus can the order at effective guarantee scene, even if be in the electric high building of stop over, also the information broadcasted can clearly be obtained, it is flurried to cause because information is chaotic.
Summary of the invention
The present invention is to solve above-mentioned technical matters, provides a kind of unmanned vehicle that can carry out broadcasting in high-altitude with wireless sound equipment.
The present invention adopts following technical scheme: should with wireless acoustics function unmanned vehicle, include aircraft body, the supply module be interconnected to constitute with the battery that can repeatedly charge by charging circuit, the rotor arm be fixedly connected with the main body of aircraft, the motor with impeller blade be located on rotor arm, be located at be mutually permanently connected with this aircraft body bottom aircraft body undercarriage, be located in main body and be interconnected formed unmanned aerial vehicle (UAV) control device with the motor on rotor arm, also include the wireless sound system be combined with each other with unmanned vehicle.
Of the present invention with in wireless acoustics function unmanned vehicle, described, described sound system includes the wireless audio reception device be located at ground audio wireless emitter and be located on unmanned vehicle.
Of the present invention with in wireless acoustics function unmanned vehicle, the audio wireless transmitter unit that described ANTENN AUDIO emitter includes power supply and is connected with power supply, this wireless transmitting unit is provided with the audio emission input connector connecting audio frequency input.
Of the present invention with in wireless acoustics function unmanned vehicle, described wireless audio reception device comprises and connects audio wireless receiving element successively, for expanding power amplifier unit and the loudspeaker of sound, and described radio receiving unit is connected with described supply module.
Of the present invention with in wireless acoustics function unmanned vehicle, described wireless sound system includes with the GSM receiver module of GSM card, for expanding power amplifier unit and the loudspeaker of sound, and described GSM receiver module and described supply module are interconnected, described loudspeaker is arranged at the bottom of unmanned vehicle main body cover, corresponding GSM transmitter unit is the GSM transmitter module with GSM card, and this GSM transmitter module is provided with the GSM audio connector connecting audio frequency input.
Useful effect: owing to have employed above-mentioned technical scheme, of the present invention with wireless acoustics function unmanned vehicle, certain height can be flown to fast in use, usually according to the mode of wireless audio frequency transmission function used, in 300 meters of scopes to unmanned plane voyage farthest, information broadcasting is carried out in real time to below flight range, therefore can convey a message clearly fast, no matter be in skyscraper or under the physical features environment of other complexity, can be notified everyone fast, ensure that there is good information broadcasting effect.
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the invention will be further described.
Fig. 1, main TV structure figure for a kind of embodiment of the present invention;
Fig. 2, theory diagram for a kind of embodiment of the present invention;
Fig. 3, theory diagram for another kind of embodiment of the present invention.
Embodiment
Please refer to Fig. 1, shown in Fig. 2 and Fig. 3, for the present invention is with the structural representation of a kind of embodiment of wireless acoustics function unmanned vehicle, should with wireless acoustics function unmanned vehicle, comprise aircraft body 1, the supply module be interconnected to constitute with the battery that can repeatedly charge by charging circuit, the rotor arm be fixedly connected with the main body of aircraft, be located at the motor with impeller blade on rotor arm, be located at the undercarriage be mutually permanently connected with this aircraft body bottom aircraft body, be located in main body and be interconnected formed unmanned aerial vehicle (UAV) control device with the motor on rotor arm, also include the wireless sound system be combined with each other with unmanned vehicle.
Further, described, described sound system includes the wireless audio reception device be located at ground audio wireless emitter and be located on unmanned vehicle.
Further, the audio wireless transmitter unit that described ANTENN AUDIO emitter includes power supply and is connected with power supply, this wireless transmitting unit is provided with the audio emission input connector connecting audio frequency input.
Further, described wireless audio reception device comprises and connects audio wireless receiving element successively, for expanding power amplifier unit and the loudspeaker 2 of sound, and described radio receiving unit is connected with described supply module.
Further, described wireless sound system includes with the GSM receiver module of GSM card, for expanding power amplifier unit and the loudspeaker of sound, and described GSM receiver module and described supply module are interconnected, described loudspeaker is arranged at the bottom of unmanned vehicle main body cover, corresponding GSM transmitter unit is the GSM transmitter module with GSM card, and this GSM transmitter module is provided with the GSM audio connector connecting audio frequency input.Owing to have employed above-mentioned technical scheme, of the present invention with wireless acoustics function unmanned vehicle, certain height can be flown to fast in use, usually according to the mode of used wireless audio frequency transmission function, can in 300 meters of scopes to unmanned plane voyage farthest, information broadcasting is carried out in real time to below flight range, therefore can convey a message clearly fast, no matter be in high-rise or under the physical features environment of other various complexity, can be notified everyone fast, ensure the effect with good information broadcasting.
Claims (5)
1. with wireless acoustics function unmanned vehicle, include aircraft body, the supply module be interconnected to constitute with the battery that can repeatedly charge by charging circuit, the rotor arm be fixedly connected with the main body of aircraft, the motor with impeller blade be located on rotor arm, be located at be mutually permanently connected with this aircraft body bottom aircraft body undercarriage, be located in main body and be interconnected formed unmanned aerial vehicle (UAV) control device with the motor on rotor arm, it is characterized in that: also include the wireless sound system be combined with each other with unmanned vehicle.
2. as claimed in claim 1 with wireless acoustics function unmanned vehicle, it is characterized in that: described, described sound system includes the wireless audio reception device is located at ground audio wireless emitter and is located on unmanned vehicle.
3. as claimed in claim 2 with wireless acoustics function unmanned vehicle, it is characterized in that: the audio wireless transmitter unit that described ANTENN AUDIO emitter includes power supply and is connected with power supply, this wireless transmitting unit is provided with the audio emission input connector connecting audio frequency input.
4. as claimed in claim 2 with wireless acoustics function unmanned vehicle, it is characterized in that: described wireless audio reception device comprises and connects audio wireless receiving element successively, for expanding power amplifier unit and the loudspeaker of sound, and described radio receiving unit is connected with described supply module.
5. as claimed in claim 1 with wireless acoustics function unmanned vehicle, it is characterized in that: described wireless sound system includes with the GSM receiver module of GSM card, for expanding power amplifier unit and the loudspeaker of sound, and described GSM receiver module and described supply module are interconnected, described loudspeaker is arranged at the bottom of unmanned vehicle main body cover, corresponding GSM transmitter unit is the GSM transmitter module with GSM card, and this GSM transmitter module is provided with the GSM audio connector connecting audio frequency input.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410586066.3A CN104460682A (en) | 2014-10-29 | 2014-10-29 | Unmanned aerial vehicle with wireless stereo function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410586066.3A CN104460682A (en) | 2014-10-29 | 2014-10-29 | Unmanned aerial vehicle with wireless stereo function |
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| CN104460682A true CN104460682A (en) | 2015-03-25 |
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| CN201410586066.3A Pending CN104460682A (en) | 2014-10-29 | 2014-10-29 | Unmanned aerial vehicle with wireless stereo function |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2016154868A1 (en) * | 2015-03-31 | 2016-10-06 | 深圳市大疆创新科技有限公司 | Flight system, aircraft, sound apparatus and sound processing method |
| WO2019241970A1 (en) * | 2018-06-21 | 2019-12-26 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle speaker control method and device |
| WO2020135528A1 (en) * | 2018-12-25 | 2020-07-02 | 深圳市道通智能航空技术有限公司 | Unmanned aircraft, voice system thereof, and voice interaction method |
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| CN103592947A (en) * | 2013-11-19 | 2014-02-19 | 华南农业大学 | Farm-oriented aerial vehicle safe operation flight monitoring device and control algorithm thereof |
| CN103941745A (en) * | 2014-03-07 | 2014-07-23 | 国家电网公司 | Movable substation and working method for unmanned aerial vehicle electric transmission line inspection |
| CN203896342U (en) * | 2014-06-10 | 2014-10-22 | 中孚航空科技（天津）有限公司 | System for calling in the air on electric unmanned helicopter |
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| CN1929335A (en) * | 2006-05-25 | 2007-03-14 | 中国人民解放军空军工程大学 | Unmanned Aerial Vehicle Control System Based on Cellular Mobile Communication |
| CN201138840Y (en) * | 2008-06-20 | 2008-10-22 | 王利龙 | Unmanned aircraft for patrol |
| CN201904789U (en) * | 2010-12-29 | 2011-07-20 | 西安上尚机电有限公司 | Radio broadcasting system |
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| CN103941745A (en) * | 2014-03-07 | 2014-07-23 | 国家电网公司 | Movable substation and working method for unmanned aerial vehicle electric transmission line inspection |
| CN203896342U (en) * | 2014-06-10 | 2014-10-22 | 中孚航空科技（天津）有限公司 | System for calling in the air on electric unmanned helicopter |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| WO2016154868A1 (en) * | 2015-03-31 | 2016-10-06 | 深圳市大疆创新科技有限公司 | Flight system, aircraft, sound apparatus and sound processing method |
| WO2019241970A1 (en) * | 2018-06-21 | 2019-12-26 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle speaker control method and device |
| WO2020135528A1 (en) * | 2018-12-25 | 2020-07-02 | 深圳市道通智能航空技术有限公司 | Unmanned aircraft, voice system thereof, and voice interaction method |
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Application publication date: 20150325 |