CN206939062U - A kind of energy-saving unmanned plane - Google Patents
A kind of energy-saving unmanned plane Download PDFInfo
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- CN206939062U CN206939062U CN201720589289.4U CN201720589289U CN206939062U CN 206939062 U CN206939062 U CN 206939062U CN 201720589289 U CN201720589289 U CN 201720589289U CN 206939062 U CN206939062 U CN 206939062U
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- unmanned plane
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- 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
Abstract
The utility model discloses a kind of energy-saving unmanned plane, solve the problems, such as prior art radiating have some setbacks, can not early warning in time and the waste energy in bad weather circumstances.The utility model includes unmanned plane main body, undercarriage, wing and empennage, opens up thermovent and ventilating opening in unmanned plane main body, 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 utility model is simple in construction, design science is reasonable, energy-conserving and environment-protective, can effectively remove heat caused by engine, while the timely early warning of energy when running into bad weather, ensure unmanned plane safe flight.
Description
Technical field
It the utility model is related 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 caused heat, it will damage the inside of unmanned plane
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.
Utility model content
The technical problems to be solved in the utility model is：A kind of energy-saving unmanned plane is provided, solves prior art radiating not
It is smooth, 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 in the utility model 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 a pair of ventilating openings, and solar panel is fixed with 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 include data processing module and are respectively connected with the data processing module
Velocity measuring module, height detection module, d GPS locating module, state of flight measurement module and meteorological measurement module；
Prismatic sealed heat dissipating housing and heat abstractor are fixed with the driving chamber, drive motor is provided with the heat dissipating housing,
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 are connected to two oil-way pipe bottoms, cavity that the outer wall of the heat dissipating housing and drive motor surrounds, two
Oil-way pipe and heat abstractor collectively constitute radiating oil return line；
The early warning intracavitary is provided with the controller for solar that is 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 manipulate 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
Form；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 to match
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 utility model has the advantages that：
The utility model is simple in construction, design science is reasonable, energy-conserving and environment-protective, utilizes the solar powered effectively save energy of energy
Source, heat caused by engine, while the timely early warning of energy when running into bad weather can be effectively removed, ensure that unmanned plane flies safely
OK；The utility model sets below heat dissipating housing by setting heat dissipating housing in generation motivation periphery and connects and formed with the heat dissipating housing
The heat abstractor of oil return line, so heat caused by engine fast and effectively can be transferred to heat abstractor and distributed,
Meanwhile upper and lower dividing plate separates driving chamber with signal acquisition chamber and early warning chamber respectively, the heat in driving chamber is effectively prevented to pass
To signal acquisition chamber and early warning chamber, the effective guarantee safety of unmanned plane internal electronic device；The utility model passes through in signal
Signal acquisition assembly is set in acquisition cavity, unmanned plane Velocity Azimuth of itself etc. in flight course can be effectively gathered in real time and join
The information such as information and surrounding environment weather is counted, and the information collected is sent to the early warning of early warning intracavitary effectively in real time
Device carries out conversion comparison, when prior-warning device has compared abnormal signal, can in real time by the abnormal signal wirelessly
The OPS on ground is sent to, wireless receiver carries out early warning, unmanned plane manipulation by coupled alarm in OPS
Bad weather scope is flown away from a manner of reducing flying height etc. further according to warning information manipulation unmanned plane by personnel or stopping of making a return voyage flies
OK, so as to effectively avoiding flight safety accident.
Brief description of the drawings
Fig. 1 is the utility model structure diagram.
Fig. 2 is the utility model side view.
Fig. 3 is that the utility model internal components connect block diagram.
Wherein, it is entitled corresponding to reference：
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 utility model is described in further detail with embodiment for explanation below in conjunction with the accompanying drawings, and mode of the present utility model includes
But it is not limited only to following examples.
Embodiment
As Figure 1-3, a kind of energy-saving unmanned plane provided by the utility model, simple in construction, design science is reasonable, section
Can be environmentally friendly, using the solar powered effectively save energy of energy, heat caused by engine can be effectively removed, and meanwhile it is severe running into
Energy timely early warning during weather, ensures unmanned plane safe flight.This energy-saving unmanned plane includes setting the unmanned plane main body 1 of inner chamber, set
It is used to support the undercarriage 2 of unmanned plane main body 1, the machine located at the top of unmanned plane main body 1 in the bottom of 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 the rear end of unmanned plane main body 1, the unmanned plane main body
Thermovent 4 is being offered at undercarriage 2 on 1, 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
It is provided with number acquisition cavity 8 and is used to gathering unmanned plane during flying status information and weather information and the information collected is real-time in 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；
Prismatic sealed heat dissipating housing 14 and heat abstractor 16 are fixed with the driving chamber 9, is provided with and drives in the heat dissipating housing 14
Dynamic motor 13, the drive shaft of the drive motor 13 pass unmanned plane main body 1 and are 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；
The controller for solar 19 electrically connected with solar panel 18 is provided with the early warning chamber 10, respectively with it is described too
The solar storage battery 20 and voltage-stablizer 21 that positive energy controller 19 electrically connects, 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；The power panel 22 divides
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 utility model sets below heat dissipating housing and connected simultaneously with the heat dissipating housing by setting heat dissipating housing in generation motivation periphery
The heat abstractor of oil return line is formed, so heat caused by engine fast and effectively can be transferred to heat abstractor and given out
Go, 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
Amount reaches signal acquisition chamber and early warning chamber, the effective guarantee safety of unmanned plane internal electronic device；The utility model by
Signal acquisition intracavitary sets signal acquisition assembly, can effectively gather unmanned plane Velocity Azimuth of itself in flight course in real time
Early warning intracavitary is sent to effectively in real time Deng the information such as parameter information and surrounding environment weather, and by the information collected
Prior-warning device carries out conversion comparison, when prior-warning device has compared abnormal signal, in real time can pass through the abnormal signal wireless
Mode is sent to the OPS on ground, and wireless receiver carries out early warning, unmanned plane by coupled alarm in OPS
Operator flies away from bad weather scope or maked a return voyage in a manner of reducing flying height etc. further according to warning information manipulation unmanned plane to stop
Only fly, so as to effectively avoid flight safety accident
The utility model gathers flight information and Weather information is exactly accurate, and the velocity measuring module passes including speed
Sensor and acceleration transducer；The height detection module is baroceptor, and the state of flight measurement module includes magnetic force
Sensor 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 of the filter circuit
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.
When prior-warning device of the present utility model compares out abnormal information, timely and effectively the abnormal information can be sent to
Ground control room, the wireless signal sending module and reception of wireless signals module are mutually matched, and reception of wireless signals mould
Block receives the wireless signal that wireless signal sending module is sent；The wireless signal sending module and reception of wireless signals module are
The Beidou communication module and mobile radio telecommunications module to match.
When the warning information transmitted by the utility model prior-warning device is precisely effective, the comparison circuit is by being connected with each other
Latch and comparator form, and the input of comparator and output end are sent with analog-digital converter and wireless signal respectively
Module connects, and associated safety threshold value is prestored in latch during use, comparator is fast in real time by the data message received
Speed compared with secure threshold in latch, when received information exceed secure threshold scope when, pass through in time
Wireless signal sending module sends this to the reception of wireless signals module in ground control room beyond information of secure threshold, together
The alarm that Shi Qidong is connected with reception of wireless signals module realizes early warning, effective and rapid.
Device used in the utility model is existing conventional device, by exquisite combination, effectively realizes that the utility model is fast
Speed radiating and the purpose of real-time early warning, suitable in the art popularization and application.
Above-described embodiment is only one of preferred embodiment of the present utility model, be should not be taken to limit of the present utility model
Protection domain, as long as in body design thought of the present utility model and that mentally makes have no the change of essential meaning or profit
Color, the technical problem that it is solved is still consistent with the utility model, should be included in the scope of protection of the utility model
Within.
Claims (5)
- A kind of 1. 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), it is provided with the signal acquisition chamber (8) and 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) include 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；Prismatic sealed heat dissipating housing (14) and heat abstractor (16) are fixed with the driving chamber (9), is set in the heat dissipating housing (14) 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 the heat abstractor (16) that the outer wall of the heat dissipating housing (14) and drive motor (13) surrounds Collectively constitute radiating oil return line；The controller for solar (19) electrically connected with solar panel (18) is provided with 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 transmission mould being connected with comparison circuit Block, the wireless signal sending module connect 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.
- A kind of 2. 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, accelerate 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.
- A kind of 3. 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.
- A kind of 4. 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 to match.
- A kind of 5. 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 formed, and the input of comparator and output end send mould with analog-digital converter and wireless signal respectively Block connects.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720589289.4U CN206939062U (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 |
|---|---|---|---|
| CN201720589289.4U CN206939062U (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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| CN206939062U true CN206939062U (en) | 2018-01-30 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201720589289.4U Active CN206939062U (en) | 2017-05-25 | 2017-05-25 | A kind of energy-saving unmanned plane |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109491403A (en) * | 2018-11-03 | 2019-03-19 | 上海电力学院 | A kind of collaboration Altitude Long Endurance Unmanned Air Vehicle connection control method |
-
2017
- 2017-05-25 CN CN201720589289.4U patent/CN206939062U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109491403A (en) * | 2018-11-03 | 2019-03-19 | 上海电力学院 | A kind of collaboration Altitude Long Endurance Unmanned Air Vehicle connection control method |
| CN109491403B (en) * | 2018-11-03 | 2021-09-07 | 上海电力学院 | Cooperative high-altitude long-endurance unmanned aerial vehicle connection control method |
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| GR01 | Patent grant | ||
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| TR01 | Transfer of patent right |
Effective date of registration: 20190613 Address after: 215133 Room 218, Yuanyuan Road 959, Yuanhe Street, Xiangcheng District, Suzhou City, Jiangsu Province Patentee after: Suzhou golden entropy Czech Solar Technology Co., Ltd. Address before: 610000 Sichuan Chengdu high tech Zone, Xiaojiahe East Lane 6, 5 Building 1, 2. Patentee before: CHENGDU CHUANTONGDA TECHNOLOGY CO., LTD. |