CN207389542U - A kind of new unmanned plane based on remote sensing technology - Google Patents
A kind of new unmanned plane based on remote sensing technology Download PDFInfo
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- CN207389542U CN207389542U CN201721428459.7U CN201721428459U CN207389542U CN 207389542 U CN207389542 U CN 207389542U CN 201721428459 U CN201721428459 U CN 201721428459U CN 207389542 U CN207389542 U CN 207389542U
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- unmanned plane
- remote sensing
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- plane body
- battery
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Abstract
The utility model discloses a kind of new unmanned planes based on remote sensing technology, including unmanned plane body, remote sensing control storehouse is provided on front side of the unmanned plane body, and the one side of unmanned plane body is provided with the first balance wing, opposite side is provided with the second balance wing, the upper surface insertion of the unmanned plane body is provided with loud speaker, and is fixedly connected with connecting rod on rear side of unmanned plane body.The utility model is provided with damping spring, pressure when unmanned plane whereabouts is contacted with ground can enough be buffered, make unmanned slide more steady, there is provided wind speed measurement devices, wind-force size during unmanned plane during flying can be detected, and then resistance when judging unmanned plane during flying, it is controlled convenient for staff, there is provided ultrasonic range finders, the barrier near unmanned plane can be measured, can effectively avoid the problem that colliding during unmanned plane during flying, there is provided radiators, the heat inside battery compartment can be dispersed automatically, extend the service life of accumulator.
Description
Technical field
The utility model is related to unmanned air vehicle technique fields, are specially a kind of new unmanned plane based on remote sensing technology.
Background technology
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and is provided for oneself
The not manned vehicle that presetting apparatus manipulates, unmanned plane is actually the general designation of unmanned vehicle, from technical standpoint
Definition can be divided into：This is several for unmanned helicopter, unmanned fixed-wing aircraft, unmanned multi-rotor aerocraft, unmanned airship, unmanned parasol
Major class, compared with manned aircraft, it has small, low cost, easy to use.
But unmanned plane currently on the market is complicated, and function is single, is not provided with damping spring, it is impossible to it buffers
Pressure when unmanned plane whereabouts is contacted with ground, it is impossible to make unmanned slide more steady, be not provided with LED light and loud speaker,
Birds cannot be driven during unmanned plane during flying, are easily damaged if unmanned plane collides with birds, are not provided with wind speed inspection
Survey device, it is impossible to drag size during unmanned plane during flying is detected, staff's control is not easy to, is not provided with ultrasonic range finder,
The barrier near unmanned plane cannot be measured, it is impossible to effectively avoid, it is impossible to reduce collision during unmanned plane during flying, be not provided with
Radiator, it is impossible to the automatic heat dispersed inside battery compartment, it is impossible to extend the service life of accumulator, be not provided with solar-electricity
Pond plate, it is impossible to convert light energy into electric energy in unmanned plane during flying, it is impossible to realize that unmanned plane has energy saving feature.
Utility model content
The utility model provides a kind of new unmanned plane based on remote sensing technology, can effectively solve in above-mentioned background technology
It is proposed is not provided with damping spring, it is impossible to buffer pressure when unmanned plane whereabouts is contacted with ground, it is impossible to make unmanned slide
It is more steady, it is not provided with LED light and loud speaker, it is impossible to birds are driven during unmanned plane during flying, if unmanned plane and birds
It collides easily impaired, is not provided with wind speed measurement device, it is impossible to detect drag size during unmanned plane during flying, be not easy to work
Personnel control is not provided with ultrasonic range finder, it is impossible to measure the barrier near unmanned plane, it is impossible to effectively avoid, it is impossible to
Collision during unmanned plane during flying is reduced, is not provided with radiator, it is impossible to the automatic heat dispersed inside battery compartment, it is impossible to extend and store
The service life of battery, is not provided with solar panel, it is impossible to convert light energy into electric energy in unmanned plane during flying, it is impossible to real
Existing unmanned plane has the problem of energy saving feature.
To achieve the above object, the utility model provides following technical solution：It is a kind of based on remote sensing technology it is new nobody
Machine including unmanned plane body, is provided with remote sensing control storehouse, and the one side of unmanned plane body is set on front side of the unmanned plane body
There is the first balance wing, opposite side is provided with the second balance wing, and the upper surface insertion of the unmanned plane body is provided with loud speaker, and
Connecting rod is fixedly connected on rear side of unmanned plane body, the lower end of the unmanned plane body is provided with supporting rod, and unmanned plane sheet
The lower end of body is provided with rear movable pulley close to a side position of supporting rod, and one end of the connecting rod is connected with empennage, the branch
The lower end of strut is provided with damping spring, and the lower end of the damping spring is provided with preceding movable pulley, before first balance wing
Side insertion is provided with LED light, and the one side of the loud speaker is provided with solar cell at the upper end position of unmanned plane body
Plate, the one side of the solar panel are provided with battery compartment, are provided with propeller on rear side of the battery compartment, and battery compartment
Accumulator is internally provided with, the inside of the battery compartment is provided with radiator, and battery compartment at a side position of accumulator
Upper end be provided with battery cabin cap, the junction of the battery cabin cap and battery compartment is provided with shaft, and the upper end of battery cabin cap
Wind speed measurement device is provided with, the remote sensing control storehouse is internally provided with circuit board, and the lower end in remote sensing control storehouse is provided with and takes the photograph
Shadow machine, the circuit board are internally provided with 586-Engine controllers, and the one side of the 586-Engine controllers is provided with
Ultrasonic range finder, and the opposite side of 586-Engine controllers is provided with GPS locator, the one side of the GPS locator is set
It is equipped with wireless transceiver.
As a kind of optimal technical scheme of the utility model, the LED light, wind speed measurement device, loud speaker, radiator,
Ultrasonic range finder, GPS locator, the input terminal of wireless transceiver and video camera passes through circuit board and 586-Engine is controlled
The output point of device is electrically connected, and the input terminal of the 586-Engine controllers and the output terminal of accumulator are electrically connected, described
The output terminal of solar panel and the input terminal of accumulator are electrically connected.
As a kind of optimal technical scheme of the utility model, one end of the battery compartment and battery cabin cap is turned by shaft
Dynamic connection, and the other end of battery compartment and battery cabin cap is bolted to connection.
As a kind of optimal technical scheme of the utility model, the empennage is fixed with unmanned plane body by connecting rod to be connected
It connects, and there are three empennage sets altogether.
As a kind of optimal technical scheme of the utility model, the LED light is provided with ten altogether, and LED light is pacified respectively
Mounted in the front side of the first balance wing and the second balance wing.
Compared with prior art, the beneficial effects of the utility model：
1st, the utility model is provided with damping spring, can enough buffer pressure when unmanned plane whereabouts is contacted with ground, make
Unmanned slide is more steady.
2nd, the utility model be provided with LED light and loud speaker, birds can be driven during unmanned plane during flying, avoid because
Unmanned plane collides the problem of easily impaired with birds.
3rd, the utility model is provided with wind speed measurement device, can detect wind-force size during unmanned plane during flying, and then judge
Resistance during unmanned plane during flying controls convenient for staff.
4th, the utility model is provided with ultrasonic range finder, can measure the barrier near unmanned plane, can be effective
It avoids the problem that colliding during unmanned plane during flying.
5th, the utility model is provided with radiator, can disperse the heat inside battery compartment automatically, extend storage
The service life of battery.
6th, the utility model is provided with solar panel, and electric energy can be converted light energy into unmanned plane during flying, protects
There are enough electric energy when demonstrate,proving unmanned plane during flying, realize that unmanned plane has energy saving feature.
Description of the drawings
Attached drawing is used to provide a further understanding of the present invention, and a part for constitution instruction, with this practicality
New embodiment for explaining the utility model, does not form the limitation to the utility model together.In the accompanying drawings：
Fig. 1 is the structure diagram of the utility model；
Fig. 2 is the mounting structure schematic diagram of the utility model accumulator；
Fig. 3 is the internal structure schematic diagram in the utility model remote sensing control storehouse；
Figure label：1st, unmanned plane body；2nd, remote sensing control storehouse；3rd, supporting rod；4th, damping spring；5th, preceding movable pulley；6、
Movable pulley afterwards；7th, the first balance wing；8th, LED light；9th, empennage；10th, connecting rod；11st, propeller；12nd, wind speed measurement device；13rd, it is electric
Chi Cang；14th, solar panel；15th, the second balance wing；16th, loud speaker；17th, shaft；18th, battery cabin cap；19th, accumulator；
20th, radiator；21st, ultrasonic range finder；22nd, 586-Engine controllers；23rd, GPS locator；24th, wireless transceiver；25、
Circuit board；26th, video camera.
Specific embodiment
The preferred embodiment of the utility model is illustrated below in conjunction with attached drawing, it should be understood that described herein excellent
Embodiment is selected to be only used for describing and explaining the present invention, is not used to limit the utility model.
Embodiment：As shown in Figs. 1-3, the utility model provides a kind of technical solution, a kind of based on the new of remote sensing technology
Unmanned plane, including unmanned plane body 1, the front side of unmanned plane body 1 is provided with remote sensing control storehouse 2, and the one side of unmanned plane body 1
The first balance wing 7 is provided with, opposite side is provided with the second balance wing 15, and the upper surface insertion of unmanned plane body 1, which is provided with, raises one's voice
Device 16, and the rear side of unmanned plane body 1 is fixedly connected with connecting rod 10, the lower end of unmanned plane body 1 is provided with supporting rod 3, and
The lower end of unmanned plane body 1 is provided with rear movable pulley 6 close to a side position of supporting rod 3, and one end of connecting rod 10 is connected with tail
The wing 9, the lower end of supporting rod 3 are provided with damping spring 4, and the lower end of damping spring 4 is provided with preceding movable pulley 5, the first balance wing 7
Front side insertion is provided with LED light 8, and the one side of loud speaker 16 is provided with solar-electricity at the upper end position of unmanned plane body 1
Pond plate 14, the one side of solar panel 14 are provided with battery compartment 13, and the rear side of battery compartment 13 is provided with propeller 11, and battery
Storehouse 13 is internally provided with accumulator 19, and the inside of battery compartment 13 is provided with radiator at a side position of accumulator 19
20, and the upper end of battery compartment 13 is provided with battery cabin cap 18, battery cabin cap 18 and the junction of battery compartment 13 are provided with shaft 17,
And the upper end of battery cabin cap 18 is provided with wind speed measurement device 12, remote sensing control storehouse 2 is internally provided with circuit board 25, and remote sensing control
The lower end in storehouse 2 processed is provided with video camera 26, and circuit board 25 is internally provided with 586-Engine controllers 22,586-Engine controls
The one side of device 22 processed is provided with ultrasonic range finder 21, and the opposite side of 586-Engine controllers 22 is provided with GPS locator
23, the one side of GPS locator 23 is provided with wireless transceiver 24.
Further, LED light 8, wind speed measurement device 12, loud speaker 16, radiator 20, ultrasonic range finder 21, GPS positioning
The input terminal of device 23, wireless transceiver 24 and video camera 26 passes through circuit board 25 and the output point of 586-Engine controllers 22
It is electrically connected, the input terminal of 586-Engine controllers 22 is electrically connected with the output terminal of accumulator 19, solar panel 14
The input terminal of output terminal and accumulator 19 be electrically connected, in order to facilitate the flight of staff's intelligent control unmanned plane, battery
Storehouse 13 and one end of battery cabin cap 18 are rotatablely connected by shaft 17, and battery compartment 13 and the other end of battery cabin cap 18 pass through spiral shell
Bolt is fixedly connected, and staff is facilitated to replace accumulator 19, and empennage 9 is fixedly connected with unmanned plane body 1 by connecting rod 10, and
Empennage 9 keeps unmanned plane smooth flight, LED light 8 is provided with ten altogether, and LED light 8 is separately mounted to there are three setting altogether
The front side of first balance wing 7 and the second balance wing 15, not only increases the beauty of unmanned plane, while also functions to the work for driveing birds
With.
The operation principle and process for using of the utility model：The lower end of supporting rod 3 is provided with damping spring 4, damping spring 4
Lower end be provided with before movable pulley 5, can enough pressure of buffering unmanned plane whereabouts when being contacted with ground, make unmanned slide more
Steadily, the front side insertion of the first balance wing 7 is provided with LED light 8, and the upper surface insertion of unmanned plane body 1 is provided with loud speaker 16,
By the flicker of LED light 8, sounded the alarm by loud speaker 16, birds can be driven during unmanned plane during flying, avoid because
Unmanned plane collides the problem of easily impaired with birds, and the one side of loud speaker 16 is at the upper end position of unmanned plane body 1
Solar panel 14 is provided with, electric energy can be converted light energy into unmanned plane during flying, ensures have during unmanned plane during flying
Enough electric energy realize that unmanned plane has energy saving feature, and the one side of solar panel 14 is provided with battery compartment 13, battery compartment 13
Rear side be provided with propeller 11, and battery compartment 13 is internally provided with accumulator 19, and the inside of battery compartment 13 is close to accumulator
Radiator 20 is provided at 19 side position, the heat inside battery compartment can be dispersed automatically, extend making for accumulator 19
The upper end in service life, and battery compartment 13 is provided with battery cabin cap 18, the junction of battery cabin cap 18 and battery compartment 13, which is provided with, to be turned
Axis 17, and the upper end of battery cabin cap 18 is provided with wind speed measurement device 12, can detect wind-force size during unmanned plane during flying, and then
Judge resistance during unmanned plane during flying, controlled convenient for staff, remote sensing control storehouse 2 is internally provided with circuit board 25, and distant
The lower end in sensing control storehouse 2 is provided with video camera 26, and circuit board 25 is internally provided with 586-Engine controllers 22,586-
The one side of Engine controllers 22 is provided with ultrasonic range finder 21, can measure the barrier near unmanned plane, can be effective
Avoid the problem that collide during unmanned plane during flying, and the opposite side of 586-Engine controllers 22 is provided with GPS locator
23, staff is facilitated to determine the position of unmanned plane, the one side of GPS locator 23 is provided with wireless transceiver 24, can facilitate
Staff receives and sends signal.
Finally it should be noted that：The foregoing is merely the preferred embodiments of the utility model, are not limited to this reality
With new, although the utility model is described in detail with reference to the foregoing embodiments, come for those skilled in the art
Say, can still modify to the technical solution recorded in foregoing embodiments or to which part technical characteristic into
Row equivalent substitution.Within the spirit and principle of the utility model, any modifications, equivalent replacements and improvements are made, should all
It is included within the scope of protection of this utility model.
Claims (5)
1. a kind of new unmanned plane based on remote sensing technology, including unmanned plane body (1), it is characterised in that：The unmanned plane sheet
Remote sensing control storehouse (2) is provided on front side of body (1), and the one side of unmanned plane body (1) is provided with the first balance wing (7), it is another
Side is provided with the second balance wing (15), and the upper surface insertion of the unmanned plane body (1) is provided with loud speaker (16), and unmanned plane
Connecting rod (10) is fixedly connected on rear side of body (1), the lower end of the unmanned plane body (1) is provided with supporting rod (3), and nothing
The lower end of man-machine body (1) is provided with rear movable pulley (6) close to a side position of supporting rod (3), and the one of the connecting rod (10)
End is connected with empennage (9), and the lower end of the supporting rod (3) is provided with damping spring (4), and the lower end of the damping spring (4) is set
Preceding movable pulley (5) is equipped with, the front side of first balance wing (7), which is embedded in, is provided with LED light (8), and the one of the loud speaker (16)
Side is provided with solar panel (14) at the upper end position of unmanned plane body (1), the solar panel (14)
One side is provided with battery compartment (13), and propeller (11), and the inside of battery compartment (13) are provided on rear side of the battery compartment (13)
Accumulator (19) is provided with, the inside of the battery compartment (13) is provided with radiator at a side position of accumulator (19)
(20), and the upper end of battery compartment (13) is provided with battery cabin cap (18), the battery cabin cap (18) and the connection of battery compartment (13)
Place is provided with shaft (17), and the upper end of battery cabin cap (18) is provided with wind speed measurement device (12), remote sensing control storehouse (2)
Be internally provided with circuit board (25), and the lower end of remote sensing control storehouse (2) is provided with video camera (26), the circuit board (25) it is interior
Portion is provided with 586-Engine controllers (22), and the one side of the 586-Engine controllers (22) is provided with ultrasonic range finder
(21), and the opposite side of 586-Engine controllers (22) is provided with GPS locator (23), and the one of the GPS locator (23)
Side is provided with wireless transceiver (24).
2. a kind of new unmanned plane based on remote sensing technology according to claim 1, it is characterised in that：The LED light
(8), wind speed measurement device (12), loud speaker (16), radiator (20), ultrasonic range finder (21), GPS locator (23), wireless
The input terminal of transceiver (24) and video camera (26) passes through circuit board (25) and the output point of 586-Engine controllers (22)
Be electrically connected, the input terminals of the 586-Engine controllers (22) and the output terminal of accumulator (19) are electrically connected, it is described too
The output terminal of positive energy solar panel (14) is electrically connected with the input terminal of accumulator (19).
3. a kind of new unmanned plane based on remote sensing technology according to claim 1, it is characterised in that：The battery compartment
(13) it is rotatablely connected with one end of battery cabin cap (18) by shaft (17), and battery compartment (13) and battery cabin cap (18) is another
End is bolted to connection.
4. a kind of new unmanned plane based on remote sensing technology according to claim 1, it is characterised in that：The empennage (9)
It is fixedly connected with unmanned plane body (1) by connecting rod (10), and there are three the common settings of empennage (9).
5. a kind of new unmanned plane based on remote sensing technology according to claim 1, it is characterised in that：The LED light (8)
Ten are provided with altogether, and LED light (8) is separately mounted to the front side of the first balance wing (7) and the second balance wing (15).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721428459.7U CN207389542U (en) | 2017-11-01 | 2017-11-01 | A kind of new unmanned plane based on remote sensing technology |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721428459.7U CN207389542U (en) | 2017-11-01 | 2017-11-01 | A kind of new unmanned plane based on remote sensing technology |
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| Publication Number | Publication Date |
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| CN207389542U true CN207389542U (en) | 2018-05-22 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721428459.7U Expired - Fee Related CN207389542U (en) | 2017-11-01 | 2017-11-01 | A kind of new unmanned plane based on remote sensing technology |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108839794A (en) * | 2018-06-01 | 2018-11-20 | 芜湖超源力工业设计有限公司 | A kind of unmanned plane of perfect heat-dissipating |
| CN109374531A (en) * | 2018-11-09 | 2019-02-22 | 浙江海洋大学 | Sea area spilled oil monitoring device based on remote sensing |
| CN109533324A (en) * | 2019-01-21 | 2019-03-29 | 宁波大学 | Butterfly multifunctional bionic robot |
| CN109911191A (en) * | 2019-04-16 | 2019-06-21 | 无锡森孚软件有限公司 | A kind of telemetry station with fixed point flight function |
-
2017
- 2017-11-01 CN CN201721428459.7U patent/CN207389542U/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108839794A (en) * | 2018-06-01 | 2018-11-20 | 芜湖超源力工业设计有限公司 | A kind of unmanned plane of perfect heat-dissipating |
| CN109374531A (en) * | 2018-11-09 | 2019-02-22 | 浙江海洋大学 | Sea area spilled oil monitoring device based on remote sensing |
| CN109533324A (en) * | 2019-01-21 | 2019-03-29 | 宁波大学 | Butterfly multifunctional bionic robot |
| CN109533324B (en) * | 2019-01-21 | 2022-05-03 | 宁波大学 | Butterfly-shaped bionic multifunctional robot |
| CN109911191A (en) * | 2019-04-16 | 2019-06-21 | 无锡森孚软件有限公司 | A kind of telemetry station with fixed point flight function |
| CN109911191B (en) * | 2019-04-16 | 2022-12-27 | 无锡森孚软件有限公司 | Telemetry station with fixed-point flight function |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180522 Termination date: 20181101 |
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| CF01 | Termination of patent right due to non-payment of annual fee |