CN107193288A - It is a kind of can smooth radiating unmanned plane - Google Patents
It is a kind of can smooth radiating unmanned plane Download PDFInfo
- Publication number
- CN107193288A CN107193288A CN201710408519.7A CN201710408519A CN107193288A CN 107193288 A CN107193288 A CN 107193288A CN 201710408519 A CN201710408519 A CN 201710408519A CN 107193288 A CN107193288 A CN 107193288A
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- chamber
- early warning
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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
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 6
- 230000001133 acceleration Effects 0.000 claims description 6
- 229910052802 copper Inorganic materials 0.000 claims description 6
- 239000010949 copper Substances 0.000 claims description 6
- 238000004891 communication Methods 0.000 claims description 4
- 238000009826 distribution Methods 0.000 claims description 3
- 239000002699 waste material Substances 0.000 abstract description 2
- 230000002159 abnormal effect Effects 0.000 description 6
- 239000000463 material Substances 0.000 description 4
- 238000006243 chemical reaction Methods 0.000 description 3
- 238000013461 design Methods 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000007613 environmental effect Effects 0.000 description 2
- 230000008450 motivation Effects 0.000 description 2
- 238000010030 laminating Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000005498 polishing Methods 0.000 description 1
Classifications
-
- 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
-
- 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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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Emergency Alarm Devices (AREA)
Abstract
The invention discloses it is a kind of can smooth radiating unmanned plane, solve prior art radiating efficiency it is low, 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 thermovent periphery sets deflector, and unmanned plane body outer wall is fixed with solar panel；Unmanned plane body lumen is separated into signal acquisition chamber, driving chamber and early warning chamber by upper spacer and lower clapboard, signal acquisition intracavitary sets signal acquisition assembly, closed heat dissipating housing and heat abstractor are set in driving chamber, heat abstractor includes hollow heat sink and oil guide pipe, circulating pump is set on oil-way pipe, 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.Energy-conserving and environment-protective of the present invention, radiate smooth and efficiency high, 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 it is a kind of can smooth radiating 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, unmanned plane flying for long time needs to expend big energy, and radiates not
It is smooth.
Therefore, set it is a can the unmanned plane of smooth radiating turn into skilled artisan's technology urgently to be resolved hurrily
Problem.
The content of the invention
The technical problem to be solved in the present invention is：There is provided it is a kind of can smooth radiating unmanned plane, solve prior art radiating
Efficiency is low, radiating has some setbacks, can not early warning in time and the problem of the waste energy in bad weather circumstances.
To achieve the above object, the technical solution adopted by the present invention is as follows：
It is a kind of can smooth radiating unmanned plane, including set the unmanned plane main body of inner chamber, located at the unmanned plane bottom part body
For supporting the undercarriage of unmanned plane main body, the wing located at the unmanned plane body top and located at the unmanned owner
Body rear end is used in the empennage for keeping unmanned plane main body to balance, the unmanned plane main body offer radiating at undercarriage
Mouthful, the thermovent periphery is provided with the deflector of the extension on the outside of unmanned plane main body, and the unmanned plane main body both sides are symmetrically opened up
Have and be 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, wherein an oil-way pipe is provided with circulating pump, the heat abstractor is located between a pair of ventilating openings, the heat abstractor
Include the hollow heat sink of more than two pieces parallel equidistant distributions, all hollow heat sinks are parallel to each other and horizontal by two
The oil guide pipe connection set in the hollow heat sink, the bottom of two oil guide pipes is connected with two oil-way pipes respectively, institute
State cavity, two oil-way pipes and heat abstractor that the outer wall of heat dissipating housing and drive motor surrounds and 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, circulating pump and drive motor electrical connection；The ratio
Be made up of compared with circuit the latch and comparator being connected with each other, and comparator input and output end respectively with analog-to-digital conversion
Device and wireless signal sending module 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 hollow heat sink be copper cored slab, the heat dissipating housing be loop configuration, and its inwall with
The outer wall laminating of drive motor.
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 efficiently removed, while the energy early warning in time when running into bad weather, it is ensured that unmanned plane safe flight.
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, heat abstractor is located between a pair of ventilating openings, the heat that quickly smoothly can so produce engine
Amount is transferred to heat abstractor and distributed, meanwhile, upper and lower dividing plate by driving chamber respectively with signal acquisition chamber and early warning chamber every
Open, effectively prevent the heat in driving chamber to reach signal acquisition chamber and early warning chamber, effective guarantee unmanned plane internal electron device
The safety of part；The present invention sets deflector at thermovent makes radiating more smooth, while setting circulating pump on oil-way pipe, can accelerate
The flowing of radiating oil in heat abstractor and heat dissipating housing, so as to improve heat exchange efficiency, and then improves radiating rate, makes radiating more suitable
Freely.
The present invention can effectively gather unmanned plane in real time in flight by setting signal acquisition assembly in signal acquisition intracavitary
During the information such as parameter information and surrounding environment weather such as the Velocity Azimuth of itself, and the information collected is had in real time
The prior-warning device for being sent to effect early warning intracavitary carries out conversion comparison, can be real-time when prior-warning device has compared abnormal signal
The abnormal signal is wirelessly sent to wireless receiver in the OPS on ground, OPS and passes through coupled report
Alert device carries out early warning, and unmanned plane operator manipulates unmanned plane further according to warning information and flies away from evil to reduce the modes such as flying height
Bad weather scope or stopping flight of making a return voyage, so as to be prevented effectively from flight safety accident.
The present invention is matched somebody with somebody by the hollow heat sink for being set as being made up of the copper material of several good heat conductivities by heat abstractor
Upper two oil guide pipes are connected, similarly, and two oil guide pipes are also made of copper material, the inwall of loop configuration heat dissipating housing
Be brought into close contact with drive motor, improve radiating efficiency, be not only simple in structure, and heat conductivility is good, can and its efficiently by heat
Amount sheds；The present invention can continue to keep energy to fill, meet unmanned plane and fly for a long time by converting solar energy into electric energy simultaneously
Row needs, moreover it is possible to the effectively save energy, beneficial to environmental protection.
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 heat abstractor schematic diagram of the present invention.
Fig. 4 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, the hollow heat sinks of 23-, 24- oil guide pipes, 25- deflectors, 26- circulating pumps.
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 1-4, the present invention provide it is a kind of can smooth radiating unmanned plane, simple in construction, design science rationally,
Energy-conserving and environment-protective, using the solar powered effectively save energy of energy, can efficiently remove the heat of engine generation, while running into evil
Energy early warning in time during bad weather, it is ensured that unmanned plane safe flight.Originally can the unmanned plane of smooth radiating include setting the unmanned plane of inner chamber
Main body 1, located at the bottom of unmanned plane main body 1 be used for support the undercarriage 2 of unmanned plane main body 1, located at the unmanned plane main body 1
The wing 12 at top and the empennage 3 for being used to keep unmanned plane main body 1 to balance located at the rear end of unmanned plane main body 1, the nothing
Thermovent 4 is being offered at undercarriage 2 in man-machine main body 1, the periphery of thermovent 4 is provided with to the outside of unmanned plane main body 1
The deflector 25 of extension, the both sides of unmanned plane main body 1 are symmetrically offered on a pair of ventilating openings 5, the outer wall of unmanned plane main body 1
It is fixed with solar panel 18.
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, wherein an oil-way pipe 15 is provided with circulating pump 26, the heat abstractor 16 is located at a pair
Between ventilating opening 5, the heat abstractor 16 includes the hollow heat sink 23 of more than two pieces parallel equidistant distributions, all described hollow
Heat sink 23 is parallel to each other by two and connected transverse to the oil guide pipe 24 that the hollow heat sink 23 is set, and is led described in two
The bottom of oil pipe 24 is connected with two oil-way pipes 15 respectively, cavity that the outer wall of the heat dissipating housing 14 and drive motor 13 is surrounded,
Two oil-way pipes 15 and heat abstractor 16 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, circulating pump 26, with
And drive motor 13 is electrically connected.
The present invention is matched somebody with somebody by the hollow heat sink for being set as being made up of the copper material of several good heat conductivities by heat abstractor
Upper two oil guide pipes are connected, similarly, and two oil guide pipes are also made of copper material, are not only simple in structure, and lead
Hot property is good, can and its efficiently heat shed；The present invention can continue to keep energy by converting solar energy into electric energy simultaneously
Amount is full, unmanned plane flying for long time needs is met, 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, heat abstractor is located between a pair of ventilating openings, the heat that quickly smoothly can so produce engine
Amount is transferred to heat abstractor and distributed, meanwhile, upper and lower dividing plate by driving chamber respectively with signal acquisition chamber and early warning chamber every
Open, effectively prevent the heat in driving chamber to reach signal acquisition chamber and early warning chamber, effective guarantee unmanned plane internal electron device
The safety of part；The present invention sets deflector at thermovent makes radiating more smooth, while setting circulating pump on oil-way pipe, can accelerate
The flowing of radiating oil in heat abstractor and heat dissipating housing, so as to improve heat exchange efficiency, and then improves radiating rate, makes radiating more suitable
Freely.
The present invention can effectively gather unmanned plane in real time in flight by setting signal acquisition assembly in signal acquisition intracavitary
During the information such as parameter information and surrounding environment weather such as the Velocity Azimuth of itself, and the information collected is had in real time
The prior-warning device for being sent to effect early warning intracavitary carries out conversion comparison, can be real-time when prior-warning device has compared abnormal signal
The abnormal signal is wirelessly sent to wireless receiver in the OPS on ground, OPS and passes through coupled report
Alert device carries out early warning, and unmanned plane operator manipulates unmanned plane further according to warning information and flies away from evil to reduce the modes such as flying height
Bad weather scope or stopping flight of making a return voyage, so as to be prevented effectively from flight safety accident
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. it is a kind of can smooth radiating unmanned plane, it is characterised in that：Including setting the unmanned plane main body (1) of inner chamber, located at the nothing
Man-machine main body (1) bottom is used to support the undercarriage (2) of unmanned plane main body (1), the machine at the top of the unmanned plane main body (1)
The wing (12) and the empennage (3) for being used to keep unmanned plane main body (1) to balance located at unmanned plane main body (1) rear end, the nothing
Thermovent (4) is being offered close to undercarriage (2) place on man-machine main body (1), thermovent (4) periphery is provided with to unmanned owner
The deflector (25) of extension on the outside of body (1), unmanned plane main body (1) both sides symmetrically offer a pair of ventilating openings (5), the nothing
Solar panel (18) is fixed with man-machine 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), wherein an oil-way pipe (15) is provided with circulating pump (26), institute
Heat abstractor (16) is stated between a pair of ventilating openings (5), the heat abstractor (16) includes more than two pieces parallel equidistant distributions
Hollow heat sink (23), all hollow heat sinks (23) are parallel to each other by two and transverse to the hollow heat sink
(23) oil guide pipe (24) connection set, the bottom of two oil guide pipes (24) is connected with two oil-way pipes (15) respectively, institute
State cavity, two oil-way pipes (15) and heat abstractor (16) that the outer wall of heat dissipating housing (14) and drive motor (13) surrounds altogether
With composition 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, circulating pump (26) and drive motor (13) electrical connection；The comparison circuit is by the latch and ratio that are connected with each other
Constituted compared with device, and the input and output end of comparator are connected with analog-digital converter and wireless signal sending module respectively.
2. it is according to claim 1 it is a kind of can smooth radiating unmanned plane, it is characterised in that：The velocity measuring module bag
Include velocity sensor and acceleration transducer；The height detection module is baroceptor, the state of flight measurement module
Including magnetometric sensor and gyroscope, the meteorologic survey module includes air velocity transducer, wind transducer and humidity sensor,
The data processing module is made up of filter circuit and signal amplification circuit；The input termination velocity pick-up of the filter circuit
Device, acceleration transducer, baroceptor, magnetometric sensor, gyroscope, air velocity transducer, wind transducer and humidity sensor
The output end of device, the input of the output termination signal amplification circuit of filter circuit, the output termination modulus of signal amplification circuit
The input of converter.
3. it is according to claim 2 it is a kind of can smooth radiating unmanned plane, it is characterised in that：The wireless signal sends mould
Block and reception of wireless signals module are mutually matched, and reception of wireless signals module receives the nothing that wireless signal sending module is sent
Line signal.
4. it is according to claim 3 it is a kind of can smooth radiating unmanned plane, it is characterised in that：The wireless signal sends mould
Block and reception of wireless signals module are the Beidou communication module and mobile radio telecommunications module matched.
5. it is according to claim 4 it is a kind of can smooth radiating unmanned plane, it is characterised in that：The hollow heat sink (23)
For copper cored slab, the heat dissipating housing (14) is loop configuration, and its inwall is fitted with the outer wall of drive motor (13).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710408519.7A CN107193288A (en) | 2017-06-02 | 2017-06-02 | It is a kind of can smooth radiating unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710408519.7A CN107193288A (en) | 2017-06-02 | 2017-06-02 | It is a kind of can smooth radiating unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107193288A true CN107193288A (en) | 2017-09-22 |
Family
ID=59877038
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710408519.7A Pending CN107193288A (en) | 2017-06-02 | 2017-06-02 | It is a kind of can smooth radiating unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107193288A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108454868A (en) * | 2018-03-23 | 2018-08-28 | 中科灵动航空科技成都有限公司 | A kind of rotor wing unmanned aerial vehicle protective cover |
| CN112710097A (en) * | 2020-12-28 | 2021-04-27 | 北京航空航天大学 | Solar unmanned aerial vehicle refrigerating system |
-
2017
- 2017-06-02 CN CN201710408519.7A patent/CN107193288A/en active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108454868A (en) * | 2018-03-23 | 2018-08-28 | 中科灵动航空科技成都有限公司 | A kind of rotor wing unmanned aerial vehicle protective cover |
| CN112710097A (en) * | 2020-12-28 | 2021-04-27 | 北京航空航天大学 | Solar unmanned aerial vehicle refrigerating system |
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