CN205168934U - A many rotor crafts for security protection system - Google Patents
A many rotor crafts for security protection system Download PDFInfo
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- CN205168934U CN205168934U CN201520756760.5U CN201520756760U CN205168934U CN 205168934 U CN205168934 U CN 205168934U CN 201520756760 U CN201520756760 U CN 201520756760U CN 205168934 U CN205168934 U CN 205168934U
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- rotor aerocraft
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Abstract
The utility model provides a many rotor crafts for security protection system, this many rotor flying device include that aircraft, orientation module, ultrasonic wave keep away barrier equipment, camera and signal transceiver module, barrier equipment is kept away to orientation module, ultrasonic wave and the camera is fixed on the aircraft, and is connected with signal transceiver module respectively. The utility model is not only simple in structure, the cost of manufacture is low, moreover through this aircraft can enlarge regional security protection area, reduce the control blind area, night the ability of patroling improve greatly.
Description
Technical field
The utility model relates to safety-security area, especially relates to a kind of multi-rotor aerocraft for safety-protection system.
Background technology
Along with the development of industry, factory, the warehouse in modern times are more and more intelligent.Each company is for reduce costs of production and operation further simultaneously, makes unmanned factory to become the trend of future development.And along with the minimizing of personnel amount, the security protection problem that enterprise assets are deposited in plant area, warehouse etc. also more and more highlights.Safety-protection system is related to enterprise's material property and personal security.Current safety-protection system comprises: video monitoring, intrusion alarm, entrance guard management, electronic visiting management, managing caller etc.The security protection of main flow is video monitoring scheme.Undeniable, video monitoring serves very important effect in whole safety-protection system, but it still has it self defect: (1) covers comprehensive, there is monitoring blind area; (2) adopt video frequency pick-up head in a large number, will cost of investment be increased high, especially large enterprise and important warehouse; (3) need hard time maintenance, add operation cost of enterprises.And in security personnel's inspection, even if use electronic patrol system, but still there is leak: (1) Security Personnel is lazy, bore the gap of management rules; (2) go on patrol not according to fixed course; (3) thing of dark place is not easily found night; (4) run into accident, easily personal casualty occurs.
Utility model content
The purpose of this utility model is: for prior art Problems existing, provides a kind of multi-rotor aerocraft for safety-protection system, solves existing monitored control system and there is monitoring blind area, and the problem that investment maintenance cost is high.
The purpose of this utility model is achieved through the following technical solutions:
A kind of multi-rotor aerocraft for safety-protection system, it is characterized in that, this many rotor flight device comprises aircraft, locating module, avoiding obstacles by supersonic wave equipment, pick up camera and signal transmitting and receiving module, described locating module, avoiding obstacles by supersonic wave equipment and pick up camera are fixing on board the aircraft, and respectively with signal transmitting and receiving model calling.
As further technical scheme, described aircraft comprises frame, brushless motor, electricity mediation lithium cell power supply, and brushless motor, electricity mediation lithium cell power supply are fixed in frame, and lithium cell power supply is connected with brushless motor by electricity tune.
As further technical scheme, it is one or more that described locating module comprises in GPS module, Big Dipper locating module and GNSS locating module.
As further technical scheme, described avoiding obstacles by supersonic wave equipment is provided with 6, and being arranged on the sidewall of up, down, left, right, before and after six direction of aircraft respectively, each avoiding obstacles by supersonic wave equipment comprises ultrasonic generator, ultrasonic receiver and sound wave converter.
As further technical scheme, described avoiding obstacles by supersonic wave equipment replaces with infrared obstacle avoidance equipment.
As further technical scheme, described pick up camera is noctovisor.
As further technical scheme, described aircraft also comprises voice module, this voice module and signal transmitting and receiving model calling.
Compared with prior art, the utility model has the following advantages:
(1) not only structure is simple, cost of manufacture is low for the utility model, and by this aircraft can enlarged area security protection area, reduce monitoring blind area;
(2) adopt infrared photography, greatly strengthen night patrol ability;
(3) avoiding obstacles by supersonic wave improves the flight safety of aircraft, reduces unnecessary loss, enhances the ability of indoor patrol simultaneously;
(4) language module can confirm identity, more simple and practical than other technologies such as face recognition technologies, and cost is lower.
Accompanying drawing explanation
Fig. 1 is electrical block diagram of the present utility model.
Detailed description of the invention
Below in conjunction with the drawings and specific embodiments, the utility model is described in detail.
Embodiment
The utility model provides a kind of multi-rotor aerocraft, and its structure is shown in Figure 1, mainly comprises aircraft, locating module, avoiding obstacles by supersonic wave equipment, pick up camera and signal transmitting and receiving module.Locating module, avoiding obstacles by supersonic wave equipment and pick up camera are fixing on board the aircraft, and respectively with signal transmitting and receiving model calling.Wherein, avoiding obstacles by supersonic wave equipment is provided with 6, and is arranged on respectively on the sidewall of up, down, left, right, before and after six direction of aircraft, achieves the obstacle detection of 3 axles.Once obstacle be detected on heading, stop automatically moving ahead, carry out in original place unsettled, this obstacle signal can be sent to control center's server of far-end simultaneously.Each avoiding obstacles by supersonic wave equipment comprises ultrasonic generator, ultrasonic receiver and sound wave converter, the acoustic signals that ultrasonic generator sends runs into obstacle and returns, now ultrasonic receiver receives the acoustic signals returned, and sends to control center's server of far-end after converting electric signal to by sound wave converter.Aircraft has automatic mode and manual mode.Under autonomous flight pattern, aircraft, by locating module, realizes presetting route flight.
Aircraft at least will comprise frame, brushless motor, electricity mediation lithium cell power supply.Brushless motor, electricity mediation lithium cell power supply are fixed in frame, and lithium cell power supply is adjusted by electricity and is connected with brushless motor.Aircraft directly can order finished product, and the longitude and latitude M100 of such as large boundary can the aircraft of secondary development, also capable of automatic assembling.
It is one or more that locating module can adopt in GPS module, Big Dipper locating module and GNSS locating module.The present embodiment adopts GPS+ Big Dipper bimodulus locating module, higher than the accuracy rate of general single mode.
Avoiding obstacles by supersonic wave equipment also can be replaced infrared obstacle avoidance equipment.
Pick up camera adopts noctovisor, can not only meet video monitoring on daytime, more can play larger effect at video monitoring at night, and noctovisor volume is little, lightweight.Meanwhile, on the basis of existing noctovisor, also can adopt infrared tracer technique, realize autotrace.
Radio communication device is provided with multiple, and is laid in diverse location, and then can cover whole security protection region.
Aircraft adopts the voice module with microphone and loudspeaker.Voice module can realize speech communication and the identity validation of Security Personnel and target person.
Utilize this multi-rotor aerocraft to form safety-protection system, as shown in Figure 1, this system is primarily of many rotor flight devices, radio communication device and control center's server composition.Many rotor flight devices are mainly used in the graphicinformation of collection site, and are undertaken controlling and data transmission by radio communication device and control center's server.
In order to strengthen the ability in indoor patrol, especially large-scale logistics warehouse, again because the positioning signal of the position fixing systems such as indoor GPS is very weak, so propose higher requirement to the location of aircraft.Simultaneously indoor obstacle can disturb the communication of aircraft.Therefore, these radio communication devices, by laying multiple radio communication device in indoor different location, are set to node by the utility model.These radio communication devices not only can strengthen the communication capacity of control center's server and many rotor flight devices, also can pass through these nodes simultaneously, carry out indoor positioning to many rotor flight devices.Keep away barrier module in conjunction with existing, improve indoor patrol ability further.
Safety-protection system operationally, has two kinds of patterns:
Aircraft automatic mode:
Control center's server sends instruction, and instruction aircraft enters automatic mode.Aircraft is navigated by locating module, flies along the route pre-set.Real-time for video is returned to control center's server by camera simultaneously.Task completes, departure place of automatically flying back.
If avoiding obstacles by supersonic wave equipment detects obstacle in way, aircraft halts automatically, enters floating state.And situation is informed control center's server.M/C is carried out by the Security Personnel of control center.When finding a suspect, Security Personnel controls aircraft and enters floating state, and is engaged in the dialogue by voice module and a suspect, confirms the other side's identity.Run into emergency case, as electricity deficiency, communication disruption, cannot the situation such as normal flight, aircraft lands slowly, and is reported to the police by control center's server.During automatic mode, manual mode can be switched in any case.
Aircraft manual mode:
State of flight, flight path and aerial mission is controlled completely by operating personal.
The foregoing is only preferred embodiment of the present utility model; not in order to limit the utility model; it should be pointed out that all do within spirit of the present utility model and principle any amendment, equivalent to replace and improvement etc., all should be included within protection domain of the present utility model.
Claims (7)
1. the multi-rotor aerocraft for safety-protection system, it is characterized in that, this many rotor flight device comprises aircraft, locating module, avoiding obstacles by supersonic wave equipment, pick up camera and signal transmitting and receiving module, described locating module, avoiding obstacles by supersonic wave equipment and pick up camera are fixing on board the aircraft, and respectively with signal transmitting and receiving model calling.
2. the multi-rotor aerocraft for safety-protection system according to claim 1, it is characterized in that, described aircraft comprises frame, brushless motor, electricity mediation lithium cell power supply, and brushless motor, electricity mediation lithium cell power supply are fixed in frame, and lithium cell power supply is connected with brushless motor by electricity tune.
3. the multi-rotor aerocraft for safety-protection system according to claim 1, is characterized in that, it is one or more that described locating module comprises in GPS module, Big Dipper locating module and GNSS locating module.
4. the multi-rotor aerocraft for safety-protection system according to claim 1, it is characterized in that, described avoiding obstacles by supersonic wave equipment is provided with 6, and being arranged on the sidewall of up, down, left, right, before and after six direction of aircraft respectively, each avoiding obstacles by supersonic wave equipment comprises ultrasonic generator, ultrasonic receiver and sound wave converter.
5. the multi-rotor aerocraft for safety-protection system according to claim 1, is characterized in that, described avoiding obstacles by supersonic wave equipment replaces with infrared obstacle avoidance equipment.
6. the multi-rotor aerocraft for safety-protection system according to claim 1, is characterized in that, described pick up camera is noctovisor.
7. the multi-rotor aerocraft for safety-protection system according to claim 1, is characterized in that, described aircraft also comprises voice module, this voice module and signal transmitting and receiving model calling.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520756760.5U CN205168934U (en) | 2015-09-28 | 2015-09-28 | A many rotor crafts for security protection system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520756760.5U CN205168934U (en) | 2015-09-28 | 2015-09-28 | A many rotor crafts for security protection system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205168934U true CN205168934U (en) | 2016-04-20 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520756760.5U Expired - Fee Related CN205168934U (en) | 2015-09-28 | 2015-09-28 | A many rotor crafts for security protection system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205168934U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106708080A (en) * | 2017-03-16 | 2017-05-24 | 江西师范大学 | Cloud control-based automatic express delivery system employing unmanned aerial vehicle |
| CN113226024A (en) * | 2019-01-16 | 2021-08-06 | 株式会社尼罗沃克 | Unmanned aerial vehicle system, unmanned aerial vehicle, moving body, partition member, control method for unmanned aerial vehicle system, and unmanned aerial vehicle system control program |
-
2015
- 2015-09-28 CN CN201520756760.5U patent/CN205168934U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106708080A (en) * | 2017-03-16 | 2017-05-24 | 江西师范大学 | Cloud control-based automatic express delivery system employing unmanned aerial vehicle |
| CN113226024A (en) * | 2019-01-16 | 2021-08-06 | 株式会社尼罗沃克 | Unmanned aerial vehicle system, unmanned aerial vehicle, moving body, partition member, control method for unmanned aerial vehicle system, and unmanned aerial vehicle system control program |
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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: 20160420 Termination date: 20170928 |