CN107168239A - A kind of rotor Long-Range Surveillance System of variable pitch four - Google Patents
A kind of rotor Long-Range Surveillance System of variable pitch four Download PDFInfo
- Publication number
- CN107168239A CN107168239A CN201710566368.8A CN201710566368A CN107168239A CN 107168239 A CN107168239 A CN 107168239A CN 201710566368 A CN201710566368 A CN 201710566368A CN 107168239 A CN107168239 A CN 107168239A
- Authority
- CN
- China
- Prior art keywords
- module
- control module
- power supply
- electrically connected
- surveillance system
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
Links
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B19/00—Programme-control systems
- G05B19/02—Programme-control systems electric
- G05B19/04—Programme control other than numerical control, i.e. in sequence controllers or logic controllers
- G05B19/05—Programmable logic controllers, e.g. simulating logic interconnections of signals according to ladder diagrams or function charts
- G05B19/058—Safety, monitoring
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B2219/00—Program-control systems
- G05B2219/10—Plc systems
- G05B2219/14—Plc safety
- G05B2219/14006—Safety, monitoring in general
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Studio Devices (AREA)
Abstract
The invention discloses a kind of rotor Long-Range Surveillance System of variable pitch four, including monitor, power supply, first control module and the second control module, first control module is made up of electric machine controller and a signal receiver, second control module is made up of No. two signal receivers and PLC, power supply is fixed with monitor, the first control module and the second control module is electrically connected in power supply, PLC in second control module is electrically connected with temperature detecting module, electric power detection module, insulation monitoring module, motor speed detection module, speech monitoring module, camera and gyro detector, No. two signal receivers, accelerometer and data transmission module, data transmission module signal connects remote terminal.The present invention's is simple in construction, cheap and practical, conveniently detects the various states of power supply and quadrotor, is easy to the normal operation of quadrotor.
Description
Technical field
The present invention relates to a kind of Long-Range Surveillance System, more particularly to a kind of rotor Long-Range Surveillance System of variable pitch four.
Background technology
The technology of fixed-wing formula unmanned plane during flying device comparative maturity, the research of rotary wind type unmanned plane is also simultaneously by comparison
It is insufficient, but rotary wind type unmanned plane has many irreplaceable advantages, and such as VTOL ability, hovering, inverted flight, side fly more
Many flight attitudes.Its middle-size and small-size multi-rotor unmanned aerial vehicle is just more and more being closed as a kind of common rotary aircraft
Note, the study hotspot as recent domestic.
But four traditional rotors are that lift is controlled by changing the rotating speed of rotor, such four rotor can only produce to
On lift, and four rotors can only by change oar speed come control direction change, traditional four rotor also by rotary inertia not
The limitation that can be mutated, it is impossible to carry out good remotely monitor.
The content of the invention
The present invention proposes a kind of rotor Long-Range Surveillance System of variable pitch four, solves prior art quadrotor
Mobility is poor, cruising time is short, noise is big, the problem of can not carry out good remotely monitor, makes the function of quadrotor
More comprehensively, enhanced convenience is used.
In order to solve the above-mentioned technical problem, the invention provides following technical scheme:
A kind of rotor Long-Range Surveillance System of variable pitch four of the present invention, including monitor, power supply, the first control module and the
Two control modules, first control module is made up of electric machine controller and a signal receiver, the second control mould
Block is made up of No. two signal receivers and PLC, and the power supply, the power supply difference are fixed with the monitor
The PLC being electrically connected with first control module and second control module, second control module is electrical
Connect temperature detecting module, electric power detection module, insulation monitoring module, motor speed detection module, speech monitoring module, shooting
Head and gyro detector, No. two signal receivers, accelerometer and data transmission module, the data transmission module signal connection
Remote terminal, the remote station signal connects the motor control in a signal receiver, first control module
Device is electrically connected with a signal receiver and drive module.
As a preferred technical solution of the present invention, multiple connecting holes are fixed with the monitor.
As a preferred technical solution of the present invention, the power supply is electrically connected with solar panel.
As a preferred technical solution of the present invention, the drive module is motor.
Compared with prior art, the beneficial effects of the invention are as follows:The present invention's is simple in construction, cheap, and practicality
By force, by the way that provided with power supply, power supply is electrically connected with solar panel, and convenient in the way of flight, solar panel is to power supply
It is powered, is effectively increased the cruising time of quadrotor machine;By provided with temperature detecting module, electric power detection mould
Block, motor speed detection module, speech monitoring module, camera and gyro detector, temperature detecting module and electric power detection mould
Block conveniently detects the temperature and electricity of power supply, and is transferred to remote terminal progress Power Supply Monitoring, speech monitoring module and shooting
Head conveniently detects volume and landform, and is transferred to remote terminal and is monitored, motor speed detection module and gyro detector
The rotating speed and angular movement state of motor are conveniently detected, and is transferred to remote terminal be monitored, be easy to quadrotor
Normal operation.
Brief description of the drawings
Accompanying drawing is used for providing a further understanding of the present invention, and constitutes a part for specification, the reality with the present invention
Applying example is used to explain the present invention together, is not construed as limiting the invention.In the accompanying drawings:
Fig. 1 is the monitor structural representation of the present invention;
Fig. 2 is the modular structure schematic diagram of the present invention;
Fig. 3 is the modular structure schematic diagram of the first control module of the present invention;
Fig. 4 is the modular structure schematic diagram of the second control module of the present invention;
In figure:1st, monitor;2nd, power supply;3rd, temperature detecting module;4th, electric power detection module;5th, insulation monitoring module;6、
Motor speed detection module;7th, speech monitoring module;8th, camera;9th, gyro detector;10th, data transmission module;11st, it is long-range
Terminal;12nd, the first control module;13rd, drive module;14th, the second control module;15th, accelerometer;16th, No. two signals are received
Device;17th, PLC;18th, electric machine controller;19th, a signal receiver.
Embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete
Site preparation is described, it is clear that described embodiment is only a part of embodiment of the invention, rather than whole embodiments, is based on
Embodiment in the present invention, it is every other that those of ordinary skill in the art are obtained under the premise of creative work is not made
Embodiment, belongs to the scope of protection of the invention.
Fig. 1-4 are referred to, the present invention discloses a kind of technical scheme:A kind of rotor Long-Range Surveillance System of variable pitch four, bag
Monitor 1, power supply 2, the first control module 12 and the second control module 14 are included, the first control module 12 is by electric machine controller 18
Constitute, the second control module 14 is made up of No. two signal receivers 16 and PLC 17, supervise with a signal receiver 19
Power supply 2 is fixed with control device 1, the first control module 12 and the second control module 14, the second control is electrically connected in power supply 2
PLC 17 in module 14 is electrically connected with temperature detecting module 3, electric power detection module 4, insulation monitoring module 5, motor and turned
Fast detection module 6, speech monitoring module 7, camera 8 and gyro detector 9, No. two signal receivers 16, the and of accelerometer 15
Data transmission module 10, the signal of data transmission module 10 connection remote terminal 11, the signal of remote terminal 11 connects a signal and connect
The electric machine controller 18 received in device 19, the first control module 12 is electrically connected with a signal receiver 19 and drive module 13.Prison
Multiple connecting holes are fixed with control device 1.Power supply 2 is electrically connected with solar panel.Drive module 13 is motor.
In use, by the way that provided with power supply, power supply is electrically connected with solar panel, convenient in the way of flight, solar energy
Cell panel is powered to power supply, is effectively increased the cruising time of quadrotor machine;By provided with temperature detection mould
Block, electric power detection module, motor speed detection module, speech monitoring module, camera and gyro detector, temperature detecting module
The temperature and electricity of power supply are conveniently detected with electric power detection module, and is transferred to remote terminal progress Power Supply Monitoring, voice prison
Survey module and camera conveniently detects volume and landform, and be transferred to remote terminal and be monitored, motor speed detection module
The rotating speed and angular movement state of motor are conveniently detected with gyro detector, and is transferred to remote terminal be monitored, be easy to four
The normal operation of rotor craft.
Finally it should be noted that:The preferred embodiments of the present invention are the foregoing is only, are not intended to limit the invention,
Although the present invention is described in detail with reference to the foregoing embodiments, for those skilled in the art, it still may be used
To be modified to the technical scheme described in foregoing embodiments, or equivalent substitution is carried out to which part technical characteristic,
Within the spirit and principles of the invention, any modification, equivalent substitution and improvements made etc., should be included in the present invention's
Within protection domain.
Claims (4)
1. a kind of rotor Long-Range Surveillance System of variable pitch four, including monitor (1), power supply (2), the first control module (12) and
Second control module (14), it is characterised in that first control module (12) is by electric machine controller (18) and a signal
Receiver (19) is constituted, and second control module (14) is made up of No. two signal receivers (16) and PLC (17),
The power supply (2) is fixed with the monitor (1), first control module is electrically connected in the power supply (2)
(12) and second control module (14), the PLC (17) in second control module (14) is electrically connected with temperature
Detection module (3), electric power detection module (4), insulation monitoring module (5), motor speed detection module (6), speech monitoring module
(7), camera (8) and gyro detector (9), No. two signal receivers (16), accelerometer (15) and data transmission module
(10), data transmission module (10) the signal connection remote terminal (11), remote terminal (11) the signal connection described one
Electric machine controller (18) in number signal receiver (19), first control module (12) is electrically connected with a signal receiver
And drive module (13) (19).
2. a kind of rotor Long-Range Surveillance System of variable pitch four according to claim 1, it is characterised in that the monitor
(1) multiple connecting holes are fixed with.
3. a kind of rotor Long-Range Surveillance System of variable pitch four according to claim 1, it is characterised in that the power supply
(2) it is electrically connected with solar panel.
4. a kind of rotor Long-Range Surveillance System of variable pitch four according to claim 1, it is characterised in that the driving mould
Block (13) is motor.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201710566368.8A CN107168239A (en) | 2017-07-12 | 2017-07-12 | A kind of rotor Long-Range Surveillance System of variable pitch four |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201710566368.8A CN107168239A (en) | 2017-07-12 | 2017-07-12 | A kind of rotor Long-Range Surveillance System of variable pitch four |
Publications (1)
Publication Number | Publication Date |
---|---|
CN107168239A true CN107168239A (en) | 2017-09-15 |
Family
ID=59823940
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201710566368.8A Withdrawn CN107168239A (en) | 2017-07-12 | 2017-07-12 | A kind of rotor Long-Range Surveillance System of variable pitch four |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN107168239A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108313313A (en) * | 2018-01-26 | 2018-07-24 | 重庆邮电大学 | Unmanned plane failure response system |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN206410742U (en) * | 2017-02-12 | 2017-08-15 | 滨州学院 | A kind of rotor Long-Range Surveillance System of variable pitch four |
-
2017
- 2017-07-12 CN CN201710566368.8A patent/CN107168239A/en not_active Withdrawn
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN206410742U (en) * | 2017-02-12 | 2017-08-15 | 滨州学院 | A kind of rotor Long-Range Surveillance System of variable pitch four |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108313313A (en) * | 2018-01-26 | 2018-07-24 | 重庆邮电大学 | Unmanned plane failure response system |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN202080435U (en) | Ranked dual-rotor vertically-lifted unmanned aerial vehicle (UAV) | |
CN204055195U (en) | A kind of six rotor diving aircraft | |
CN102126554A (en) | Unmanned air vehicle with multiple rotary wings in plane-symmetry layout | |
CN103359283A (en) | High-reliability unmanned aerial vehicle with tilt rotors | |
CN203876983U (en) | Spherical flight device | |
CN108146608B (en) | A composite aerostat with vector thrust rotor and inflatable airbag | |
CN106347651A (en) | Columnar and coaxial double-propeller miniature unmanned aerial vehicle | |
CN110481769A (en) | Unmanned flight's device based on coaxial double-rotary wing | |
CN201151485Y (en) | Coaxial counter-rotating flying saucer | |
CN109592024A (en) | A kind of Intelligent unattended machine | |
CN108706097A (en) | A kind of captive rotor flying robot with double-manipulator | |
CN114379777B (en) | Tilting rotor unmanned aerial vehicle structure and working method thereof | |
CN101811572A (en) | Coaxial-inversion birotor eight-rotary wing aircraft | |
CN103345255A (en) | Quad-rotor aerial photography positioning unmanned aerial vehicle | |
CN203405734U (en) | Quadrotor aerial photography positioning unmanned aerial vehicle | |
CN104176249B (en) | A kind of non co axial anti-oar many rotors unmanned gyroplane | |
CN107168239A (en) | A kind of rotor Long-Range Surveillance System of variable pitch four | |
CN206410742U (en) | A kind of rotor Long-Range Surveillance System of variable pitch four | |
CN207759016U (en) | A kind of vertical take-off and landing drone electrical system | |
CN206331305U (en) | Electricity tune, unmanned plane and its control system | |
CN104494817A (en) | Four-rotor unmanned aerial vehicle | |
CN210175106U (en) | Multi-direction locking folding mechanism of unmanned aerial vehicle wing | |
CN210133283U (en) | Combined type aircraft | |
CN204642143U (en) | Propeller arrangement, vector propulsion system and aircraft | |
CN206719537U (en) | A kind of safety-type unmanned plane |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
WW01 | Invention patent application withdrawn after publication | ||
WW01 | Invention patent application withdrawn after publication |
Application publication date: 20170915 |