CN107176288A - A kind of energy-saving unmanned plane - Google Patents
A kind of energy-saving unmanned plane Download PDFInfo
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- CN107176288A CN107176288A CN201710376660.3A CN201710376660A CN107176288A CN 107176288 A CN107176288 A CN 107176288A CN 201710376660 A CN201710376660 A CN 201710376660A CN 107176288 A CN107176288 A CN 107176288A
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- 125000006850 spacer group Chemical group 0.000 claims abstract description 8
- 238000012545 processing Methods 0.000 claims description 13
- 230000003321 amplification Effects 0.000 claims description 9
- 238000003199 nucleic acid amplification method Methods 0.000 claims description 9
- 238000005259 measurement Methods 0.000 claims description 8
- 238000001514 detection method Methods 0.000 claims description 7
- 230000001133 acceleration Effects 0.000 claims description 6
- 238000004891 communication Methods 0.000 claims description 5
- 238000013461 design Methods 0.000 abstract description 4
- 238000010276 construction Methods 0.000 abstract description 3
- 239000002699 waste material Substances 0.000 abstract description 2
- 230000002159 abnormal effect Effects 0.000 description 6
- 238000006243 chemical reaction Methods 0.000 description 2
- 230000008450 motivation Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000005498 polishing Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/06—Helicopters with single rotor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/068—Fuselage sections
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/08—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of power plant cooling systems
- B64D33/10—Radiator arrangement
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D43/00—Arrangements or adaptations of instruments
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/02—Arrangements or adaptations of signal or lighting devices
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
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- G—PHYSICS
- G08—SIGNALLING
- G08B—SIGNALLING OR CALLING SYSTEMS; ORDER TELEGRAPHS; ALARM SYSTEMS
- G08B25/00—Alarm systems in which the location of the alarm condition is signalled to a central station, e.g. fire or police telegraphic systems
- G08B25/01—Alarm systems in which the location of the alarm condition is signalled to a central station, e.g. fire or police telegraphic systems characterised by the transmission medium
- G08B25/10—Alarm systems in which the location of the alarm condition is signalled to a central station, e.g. fire or police telegraphic systems characterised by the transmission medium using wireless transmission systems
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
- H02J7/34—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering
- H02J7/35—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering with light sensitive cells
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- General Physics & Mathematics (AREA)
- Physics & Mathematics (AREA)
- Emergency Management (AREA)
- Business, Economics & Management (AREA)
- Computer Networks & Wireless Communication (AREA)
- Radar, Positioning & Navigation (AREA)
- Automation & Control Theory (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Power Engineering (AREA)
- Arrangements For Transmission Of Measured Signals (AREA)
Abstract
The invention discloses a kind of energy-saving unmanned plane, solve prior art radiating have some setbacks, in bad weather circumstances can not early warning in time and waste the energy the problem of.The present invention includes opening up thermovent and ventilating opening in unmanned plane main body, undercarriage, wing and empennage, unmanned plane main body, and unmanned plane body outer wall is fixed with solar panel；Inner chamber is separated into signal acquisition chamber, driving chamber and early warning chamber by the upper spacer and lower clapboard of unmanned plane body lumen, signal acquisition intracavitary sets signal acquisition assembly, closed heat dissipating housing and heat abstractor are fixed with driving chamber, drive motor is set in heat dissipating housing, early warning intracavitary sets prior-warning device, controller for solar, solar storage battery, voltage-stablizer and power panel.The present invention is simple in construction, design science is reasonable, energy-conserving and environment-protective, can effectively remove the heat of engine generation, while the energy early warning in time when running into bad weather, it is ensured that unmanned plane safe flight.
Description
Technical field
The present invention relates to a kind of energy-saving unmanned plane.
Background technology
With developing rapidly for unmanned air vehicle technique, its application field is more and more extensive, and unmanned plane is frequent in flight course
The bad weather for being not suitable for flight can be encountered, exceeded when unmanned plane runs into speed of such weather or flight etc. in flight course
During permissible velocity under current environment, it is easy to air crash accident occur, so as to cause unnecessary loss；Unmanned plane is when long
Between flight when, substantial amounts of heat can be produced, if not in time distributed produced heat, it will damage unmanned plane inside
Electronic device, greatly shortens the service life of unmanned plane, and unmanned plane flying for long time needs to expend big energy.
Therefore, setting a energy-saving unmanned plane turns into skilled artisan's technical problem urgently to be resolved hurrily.
The content of the invention
The technical problem to be solved in the present invention is：A kind of energy-saving unmanned plane is provided, solve prior art radiating have some setbacks,
In bad weather circumstances can not early warning in time and waste the energy the problem of.
To achieve the above object, the technical solution adopted by the present invention is as follows：
A kind of energy-saving unmanned plane, including set the unmanned plane main body of inner chamber, be used for branch located at the unmanned plane bottom part body
Support the undercarriage of unmanned plane main body, the wing located at the unmanned plane body top and located at the unmanned plane body rear
For the empennage for keeping unmanned plane main body to balance, thermovent is being offered at undercarriage in the unmanned plane main body, it is described
Unmanned plane main body both sides symmetrically offer and are fixed with solar panel on a pair of ventilating openings, the unmanned plane body outer wall；
The inner chamber of the unmanned plane main body is sequentially provided with upper spacer and lower clapboard, the upper spacer and lower clapboard from top to bottom
By unmanned plane body lumen, side is separated into signal acquisition chamber, driving chamber and early warning chamber, the signal acquisition intracavitary from top to bottom
Provided with what is sent out in real time for collection unmanned plane during flying status information and weather information in real time and by the information collected
Signal acquisition assembly, the signal acquisition assembly includes data processing module and the speed being connected respectively with the data processing module
Spend detection module, height detection module, d GPS locating module, state of flight measurement module and meteorological measurement module；
It is fixed with the driving chamber in prismatic sealed heat dissipating housing and heat abstractor, the heat dissipating housing and is provided with drive motor,
The drive shaft of the drive motor passes unmanned plane main body and is connected with wing, and the heat dissipating housing bottom is communicated with two oil circuits
Pipe, the heat abstractor is connected to two oil-way pipe bottoms, cavity that the outer wall of the heat dissipating housing and drive motor is surrounded, two
Oil-way pipe and heat abstractor collectively constitute radiating oil return line；
The early warning intracavitary is provided with the controller for solar electrically connected with solar panel, respectively with the solar energy control
The solar storage battery and voltage-stablizer of device electrical connection processed, the power panel electrically connected with voltage-stablizer, and filled for the early warning of early warning
Put；The prior-warning device includes the analog-digital converter being connected with data processing module, the ratio being connected with digital analog converter output end
The wireless signal sending module being connected compared with circuit and with comparison circuit, the wireless signal sending module is manipulated with unmanned plane
Interior is connected with the reception of wireless signals module signal connection of alarm；The power panel respectively with d GPS locating module, data
Manage module, analog-digital converter, comparison circuit, wireless signal sending module and drive motor electrical connection.
Further, the velocity measuring module includes velocity sensor and acceleration transducer；The height detection mould
Block is baroceptor, and the state of flight measurement module includes magnetometric sensor and gyroscope, the meteorologic survey module bag
Air velocity transducer, wind transducer and humidity sensor are included, the data processing module is by filter circuit and signal amplification circuit
Constitute；Input termination velocity sensor, acceleration transducer, baroceptor, magnetometric sensor, the gyro of the filter circuit
Instrument, air velocity transducer, the output end of wind transducer and humidity sensor, the output termination signal amplification circuit of filter circuit
Input, the input of the output termination analog-digital converter of signal amplification circuit.
Further, the wireless signal sending module and reception of wireless signals module are mutually matched, and wireless signal
Receiving module receives the wireless signal that wireless signal sending module is sent.
Further, the wireless signal sending module and reception of wireless signals module are the Beidou communication module matched
With mobile radio telecommunications module.
Further, the comparison circuit is made up of the latch and comparator being connected with each other, and the input of comparator
End and output end are connected with analog-digital converter and wireless signal sending module respectively.
Compared with prior art, the invention has the advantages that：
The present invention is simple in construction, design science is reasonable, energy-conserving and environment-protective, utilizes the solar powered effectively save energy of energy, energy
The heat of engine generation is effectively removed, while the energy early warning in time when running into bad weather, it is ensured that unmanned plane safe flight；This
Invention connects and formed dissipating for oil return line by setting heat dissipating housing in generation motivation periphery, and being set below heat dissipating housing with the heat dissipating housing
Thermal, so fast and effectively can be transferred to heat abstractor by the heat that engine is produced and distribute, meanwhile, it is upper and lower
Dividing plate separates driving chamber with signal acquisition chamber and early warning chamber respectively, effectively prevents the heat in driving chamber to reach signal acquisition
Chamber and early warning chamber, the effective guarantee safety of unmanned plane internal electronic device；The present invention in signal acquisition intracavitary by setting signal
Gather assembly, effectively can gather in real time unmanned plane in flight course the parameter information such as Velocity Azimuth of itself and around
The information such as ambient weather, and the prior-warning device that the information collected is sent into early warning intracavitary effectively in real time carries out conversion ratio
Compared with when prior-warning device has compared abnormal signal, the abnormal signal can be wirelessly sent to the behaviour on ground in real time
Control wireless receiver in room, OPS and early warning is carried out by coupled alarm, unmanned plane operator is further according to early warning
Information manipulates unmanned plane and flies away from bad weather scope or stopping flight of making a return voyage to reduce the modes such as flying height, so as to effectively keep away
Exempt from flight safety accident.
Brief description of the drawings
Fig. 1 is schematic structural view of the invention.
Fig. 2 is side view of the present invention.
Fig. 3 is that internal components of the present invention connect block diagram.
Wherein, reference is corresponding entitled：
1- unmanned planes main body, 2- undercarriages, 3- empennages, 4- thermovents, 5- ventilating openings, 6- upper spacers, 7- lower clapboards, 8- letters
Number acquisition cavity, 9- driving chambers, 10- early warning chamber, 11- signal acquisitions assembly, 12- wings, 13- drive motors, 14- heat dissipating housings, 15-
Oil-way pipe, 16- heat abstractors, 17- prior-warning devices, 18- solar panels, 19- controller for solar, 20- solar energy power accumulatings
Pond, 21- voltage-stablizers, 22- power panels.
Embodiment
The invention will be further described with embodiment for explanation below in conjunction with the accompanying drawings, and mode of the invention includes but not only limited
In following examples.
Embodiment
As Figure 1-3, a kind of energy-saving unmanned plane that the present invention is provided, simple in construction, design science is reasonable, energy-saving ring
Protect, using the solar powered effectively save energy of energy, the heat of engine generation can be effectively removed, while running into bad weather
When can in time early warning, it is ensured that unmanned plane safe flight.This energy-saving unmanned plane includes setting the unmanned plane main body 1 of inner chamber, located at institute
Stating the bottom of unmanned plane main body 1 is used to support the undercarriage 2 of unmanned plane main body 1, the wing located at the top of unmanned plane main body 1
12 and located at the rear end of unmanned plane main body 1 be used for keep unmanned plane main body 1 balance empennage 3, the unmanned plane main body 1
On offering thermovent 4 at the undercarriage 2, the both sides of unmanned plane main body 1 symmetrically offer a pair of ventilating openings 5, described
Solar panel 18 is fixed with the outer wall of unmanned plane main body 1；
The inner chamber of the unmanned plane main body 1 is sequentially provided with upper spacer 6 and lower clapboard 7 from top to bottom, and the upper spacer 6 is with
By the inner chamber of unmanned plane main body 1, side is separated into signal acquisition chamber 8, driving chamber 9 and early warning chamber 10, the letter to dividing plate 7 from top to bottom
Being provided with number acquisition cavity 8 is used to gather unmanned plane during flying status information and weather information in real time and the information collected is real-time
The signal acquisition assembly 11 sent out, the signal acquisition assembly 11 include data processing module and respectively with the data
Manage velocity measuring module, height detection module, d GPS locating module, state of flight measurement module and the meteorologic survey of module connection
Module；
It is fixed with the driving chamber 9 in prismatic sealed heat dissipating housing 14 and heat abstractor 16, the heat dissipating housing 14 provided with drive
Dynamic motor 13, the drive shaft of the drive motor 13 passes unmanned plane main body 1 and is connected with wing 12, the bottom of heat dissipating housing 14
Two oil-way pipes 15 are communicated with, the heat abstractor 16 is connected to two bottoms of oil-way pipe 15, the heat dissipating housing 14 and driving horse
The outer wall cavity, two oil-way pipes 15 and the heat abstractor 16 that surround up to 13 collectively constitute radiating oil return line；
Provided with the controller for solar 19 electrically connected with solar panel 18 in the early warning chamber 10, respectively with it is described too
Solar storage battery 20 and voltage-stablizer 21 that positive energy controller 19 is electrically connected, the power panel 22 electrically connected with voltage-stablizer 21, and
Prior-warning device 17 for early warning；The prior-warning device 17 includes analog-digital converter and the digital-to-analogue being connected with data processing module
The comparison circuit of converter output end connection and the wireless signal sending module being connected with comparison circuit, the wireless signal
Sending module is connected with being connected with the reception of wireless signals module signal of alarm in unmanned plane OPS；22 points of the power panel
Not with d GPS locating module, data processing module, analog-digital converter, comparison circuit, wireless signal sending module and driving horse
Up to 13 electrical connections, by converting solar energy into electric energy, it can continue to keep energy to fill, meet unmanned plane flying for long time need
Will, moreover it is possible to the effectively save energy, beneficial to environmental protection.
The present invention is connected and formed with the heat dissipating housing by setting heat dissipating housing in generation motivation periphery, and being set below heat dissipating housing
The heat abstractor of oil return line, so fast and effectively can be transferred to heat abstractor by the heat that engine is produced and distribute,
Meanwhile, upper and lower dividing plate separates driving chamber with signal acquisition chamber and early warning chamber respectively, effectively prevents the heat in driving chamber to pass
To signal acquisition chamber and early warning chamber, the effective guarantee safety of unmanned plane internal electronic device；The present invention is by signal acquisition
Intracavitary sets signal acquisition assembly, and unmanned plane parameter such as Velocity Azimuth of itself in flight course can be effectively gathered in real time and is believed
Breath and the information such as surrounding environment weather, and the information collected is sent to the prior-warning device of early warning intracavitary effectively in real time
Conversion comparison is carried out, when prior-warning device has compared abnormal signal, in real time can wirelessly be transmitted the abnormal signal
To the OPS on ground, wireless receiver carries out early warning, unmanned plane operator by coupled alarm in OPS
Unmanned plane, which is manipulated, further according to warning information flies away from bad weather scope or stopping flight of making a return voyage to reduce the modes such as flying height, from
And flight safety accident can be prevented effectively from
The present invention gathers flight information and Weather information is exactly accurate, and the velocity measuring module includes velocity sensor
And acceleration transducer；The height detection module is baroceptor, and the state of flight measurement module is sensed including magnetic force
Device and gyroscope, the meteorologic survey module include air velocity transducer, wind transducer and humidity sensor, the data processing
Module is made up of filter circuit and signal amplification circuit；Input termination velocity sensor, the acceleration sensing of the filter circuit
Device, baroceptor, magnetometric sensor, gyroscope, air velocity transducer, the output end of wind transducer and humidity sensor, filter
The input of the output termination signal amplification circuit of wave circuit, the input of the output termination analog-digital converter of signal amplification circuit
End.
When the prior-warning device of the present invention compares out abnormal information, the abnormal information timely and effectively can be sent to ground
OPS, the wireless signal sending module and reception of wireless signals module are mutually matched, and reception of wireless signals module connects
Receive the wireless signal that wireless signal sending module is sent；The wireless signal sending module and reception of wireless signals module are phase
The Beidou communication module and mobile radio telecommunications module matched somebody with somebody.
When the warning information transmitted by prior-warning device of the present invention is precisely effective, the comparison circuit is by the latch that is connected with each other
Device and comparator are constituted, and the input and output end of comparator connect with analog-digital converter and wireless signal sending module respectively
Connect, prestore associated safety threshold values when using in latch, comparator by the data message received it is real-time with
Safe threshold is compared in latch, when received information exceeds the scope of safe threshold, passes through wireless communication in time
Number sending module sends this to the reception of wireless signals module in ground control room beyond information of safe threshold, starts simultaneously
The alarm being connected with reception of wireless signals module realizes early warning, effective and rapid.
Device of the invention used is existing conventional device, by exquisite combination, effectively realization quick heat radiating of the present invention and
The purpose of real-time early warning, suitable in the art popularization and application.
Above-described embodiment is only one of the preferred embodiment of the present invention, should not be taken to limit the protection model of the present invention
Enclose, as long as the present invention body design thought and mentally make have no the change of essential meaning or polishing, it is solved
Technical problem it is still consistent with the present invention, should be included in protection scope of the present invention within.
Claims (5)
1. a kind of energy-saving unmanned plane, it is characterised in that：Including setting the unmanned plane main body (1) of inner chamber, located at the unmanned owner
Body (1) bottom is used to support the undercarriage (2) of unmanned plane main body (1), the wing at the top of the unmanned plane main body (1)
(12) and located at unmanned plane main body (1) rear end be used for keep unmanned plane main body (1) balance empennage (3), it is described nobody
Thermovent (4) is being offered close to undercarriage (2) place on owner's body (1), unmanned plane main body (1) both sides symmetrically offer one
To ventilating opening (5), solar panel (18) is fixed with unmanned plane main body (1) outer wall；
The inner chamber of the unmanned plane main body (1) is sequentially provided with upper spacer (6) and lower clapboard (7), the upper spacer (6) from top to bottom
By unmanned plane main body (1) inner chamber, side is separated into signal acquisition chamber (8), driving chamber (9) and early warning from top to bottom with lower clapboard (7)
Chamber (10), being provided with the signal acquisition chamber (8) is used to gathering unmanned plane during flying status information and weather information in real time and by institute
The signal acquisition assembly (11) that the information collected is sent out in real time, the signal acquisition assembly (11) includes data processing mould
Block and the velocity measuring module being connected respectively with the data processing module, height detection module, d GPS locating module, flight shape
State measurement module and meteorological measurement module；
It is fixed with prismatic sealed heat dissipating housing (14) and heat abstractor (16), the heat dissipating housing (14) and sets in the driving chamber (9)
There is drive motor (13), the drive shaft of the drive motor (13) passes unmanned plane main body (1) and is connected with wing (12), described
Heat dissipating housing (14) bottom is communicated with two oil-way pipes (15), and the heat abstractor (16) is connected to two oil-way pipe (15) bottoms,
Cavity, two oil-way pipes (15) and heat abstractor (16) that the outer wall of the heat dissipating housing (14) and drive motor (13) is surrounded
Collectively constitute radiating oil return line；
Provided with the controller for solar (19) electrically connected with solar panel (18) in the early warning chamber (10), respectively with it is described
The solar storage battery (20) and voltage-stablizer (21) of controller for solar (19) electrical connection, the power supply electrically connected with voltage-stablizer (21)
Plate (22), and the prior-warning device (17) for early warning；The prior-warning device (17) includes the mould being connected with data processing module
Number converter, the comparison circuit being connected with digital analog converter output end and the wireless signal being connected with comparison circuit send mould
Block, the wireless signal sending module connects with being connected with the reception of wireless signals module signal of alarm in unmanned plane OPS
Connect；The power panel (22) respectively with d GPS locating module, data processing module, analog-digital converter, comparison circuit, wireless signal
Sending module and drive motor (13) electrical connection.
2. a kind of energy-saving unmanned plane according to claim 1, it is characterised in that：The velocity measuring module includes speed
Sensor and acceleration transducer；The height detection module is baroceptor, and the state of flight measurement module includes magnetic
Force snesor and gyroscope, the meteorologic survey module include air velocity transducer, wind transducer and humidity sensor, the number
It is made up of according to processing module filter circuit and signal amplification circuit；The input termination velocity sensor of the filter circuit, acceleration
Spend the output of sensor, baroceptor, magnetometric sensor, gyroscope, air velocity transducer, wind transducer and humidity sensor
End, the input of the output termination signal amplification circuit of filter circuit, the output termination analog-digital converter of signal amplification circuit
Input.
3. a kind of energy-saving unmanned plane according to claim 2, it is characterised in that：The wireless signal sending module and nothing
Line signal receiving module is mutually matched, and reception of wireless signals module receives the wireless communication that wireless signal sending module is sent
Number.
4. a kind of energy-saving unmanned plane according to claim 3, it is characterised in that：The wireless signal sending module and nothing
Line signal receiving module is the Beidou communication module and mobile radio telecommunications module matched.
5. a kind of energy-saving unmanned plane according to claim 4, it is characterised in that：The comparison circuit is by being connected with each other
Latch and comparator are constituted, and the input and output end of comparator send mould with analog-digital converter and wireless signal respectively
Block is connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710376660.3A CN107176288A (en) | 2017-05-25 | 2017-05-25 | A kind of energy-saving unmanned plane |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710376660.3A CN107176288A (en) | 2017-05-25 | 2017-05-25 | A kind of energy-saving unmanned plane |
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| Publication Number | Publication Date |
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| CN107176288A true CN107176288A (en) | 2017-09-19 |
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ID=59832260
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| Application Number | Title | Priority Date | Filing Date |
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| CN201710376660.3A Pending CN107176288A (en) | 2017-05-25 | 2017-05-25 | A kind of energy-saving unmanned plane |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108039766A (en) * | 2017-12-23 | 2018-05-15 | 王艺臻 | A kind of electric power system of unmanned plane |
| CN111060654A (en) * | 2019-12-25 | 2020-04-24 | 电子科技大学成都学院 | Unmanned aerial vehicle atmospheric pollution real-time supervision early warning platform based on digital twin |
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| CN205854488U (en) * | 2016-08-03 | 2017-01-04 | 泛洲科技（北京）有限公司 | A kind of solar energy charging type unmanned plane |
| CN206144655U (en) * | 2016-10-26 | 2017-05-03 | 天津曙光天成科技有限公司 | Many rotor unmanned aerial vehicle engine cooling device and many rotor unmanned aerial vehicle |
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| CN205366072U (en) * | 2015-12-31 | 2016-07-06 | 天津御遨航空科技发展有限公司 | Unmanned aerial vehicle |
| CN205403847U (en) * | 2016-03-02 | 2016-07-27 | 成都翼比特自动化设备有限公司 | A early warning device for unmanned aerial vehicle |
| CN205854488U (en) * | 2016-08-03 | 2017-01-04 | 泛洲科技（北京）有限公司 | A kind of solar energy charging type unmanned plane |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108039766A (en) * | 2017-12-23 | 2018-05-15 | 王艺臻 | A kind of electric power system of unmanned plane |
| CN111060654A (en) * | 2019-12-25 | 2020-04-24 | 电子科技大学成都学院 | Unmanned aerial vehicle atmospheric pollution real-time supervision early warning platform based on digital twin |
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