CN209008855U - A kind of novel high null base station of bispin rotor unmanned plane - Google Patents
A kind of novel high null base station of bispin rotor unmanned plane Download PDFInfo
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- CN209008855U CN209008855U CN201820994083.4U CN201820994083U CN209008855U CN 209008855 U CN209008855 U CN 209008855U CN 201820994083 U CN201820994083 U CN 201820994083U CN 209008855 U CN209008855 U CN 209008855U
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- fuselage
- base station
- rotary wings
- driving motor
- unmanned plane
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Abstract
The utility model discloses a kind of novel high null base station of bispin rotor unmanned plane, it mainly include fuselage, communication base station, control circuit board, first rotary wings group, second rotary wings group, landing aid device and scarer, communication base station is fixedly mounted on the inside of fuselage, control circuit board is electrically connected at the top of communication base station, first rotary wings group is mounted on the upper left side of fuselage, including the first rotary wings, first drive rod, first driving motor and first sliding groove, second rotary wings group is mounted on the upper right side of fuselage, including the second rotary wings, second drive rod, second driving motor and second sliding slot, landing aid device is mounted on the lower section of fuselage, there are two scarer is total, respectively symmetrically it is mounted on the left and right sides of fuselage.In short, the utility model has many advantages, such as that load-carrying is big, adaptability is good, safe and efficient, at low cost.
Description
Technical field
The utility model belongs to wireless communication technique field, is specifically related to a kind of novel high space base of bispin rotor unmanned plane
It stands.
Background technique
UAV is the not manned aircraft manipulated using radio robot and the presetting apparatus provided for oneself,
Or it fully or is intermittently automatically operated by car-mounted computer.Compared with manned aircraft, unmanned plane is often more suitable for
The task of those too " slow-witted, dirty or dangerous ".Unmanned plane press application field, can be divided into it is military with it is civilian.Military aspect, nobody
Machine is divided into reconnaissance plane and target drone.Civilian aspect, unmanned plane+industrial application are that unmanned plane has really just needed；At present take photo by plane, agriculture
Industry, plant protection, miniature self-timer, express transportation, disaster relief, observation wild animal, monitoring infectious disease, mapping, news report, electric power
The application in inspection, the disaster relief, movies-making, manufacture romance etc. field, has greatly expanded the purposes of unmanned plane itself, flourishing state
Family also in actively extension industrial application and develops unmanned air vehicle technique.
In recent years, global operator also expands corresponding research therewith, explores and is suitable for different scenes, inexpensive, easy
The high null base station of deployment.Studying molding high null base station at present includes fire balloon and helium balloon.Wherein fire balloon changes by several generations
It is good, captive fire balloon has had been developed.Captive fire balloon is at low cost, and when lift-off height is to 1000m, coverage area is reachable
40km.But its volume about 6000m3, hang time are only capable of maintaining 6 hours, be only applicable under the weather for being better than small sleet, when lift-off
In the environment of less than 3 grades of surface wind (5 meter per second), less than 5 grades of aerial wind-force (10 meter per second), and 60m is at least needed when lift-off
The headroom place of the smooth of × 60m, periphery without tall and big shelter, needs 20 people of manpower or so.And helium balloon is improved by several generations,
Captive helium ship has had been developed.When captive helium ship lift-off height is to 1000m, coverage area is up to 50km, when stagnant empty
Between can maintain 72 hours.But it possesses the drawbacks of captive hot gas sphere volume causes greatly, and higher cost simultaneously, needs 15,000,000
Left and right, an experimental cost about 200,000.
And unmanned plane has load-carrying big, can be manipulated at a distance, solves under emergency disaster relief scene, personnel or vehicle without
The advantages of scene that method enters, can be low with long-distance remote control progress signal of communication covering takeoff condition, is adapted to adverse circumstances,
So design a kind of novel high null base station of bispin rotor unmanned plane very it is necessary to.
Utility model content
In view of the above problems, the utility model provides a kind of novel high null base station of bispin rotor unmanned plane.
Technical solution provided by the utility model is: a kind of novel high null base station of bispin rotor unmanned plane, mainly includes machine
Body, communication base station, control circuit board, the first rotary wings group, the second rotary wings group, landing aid device, scarer and power supply, it is described
Communication base station is fixedly mounted on the inside of fuselage, and the control circuit board is electrically connected at the top of communication base station, and described first
Rotary wings group includes the first rotary wings, the first drive rod, the first driving motor and first sliding groove, and first rotary wings are mounted on
The upper left side of fuselage, first drive rod upper end are fixedly connected with the first rotary wings, the first drive rod lower end and described first
The output shaft of driving motor is fixedly connected, and first driving motor is movably connected in fuselage left side by the first sliding groove
Portion bottom end, the second rotary wings group includes the second rotary wings, the second drive rod, the second driving motor and second sliding slot, described
Second rotary wings are mounted on the upper right side of fuselage, and second drive rod upper end is fixedly connected with the second rotary wings, the second transmission
Bar lower end is fixedly connected with the output shaft of second driving motor, and second driving motor passes through the second sliding slot activity
Be connected to inner bottom on the right side of fuselage, the landing aid device is mounted on the lower section of fuselage, the scarer altogether there are two, respectively
Be symmetrically mounted on the left and right sides of fuselage, the power supply altogether there are two, be separately positioned at left and right sides of communication base station.
Further, the control circuit board is also electrically connected with the first driving motor and the second driving motor, control electricity
Road plate controls the state of flight of unmanned plane by the first driving motor of control and the second driving motor.
Further, the fuselage upper surface middle part is equipped with solar panel, and solar panel connects to power supply, and uses
It charges in power supply.
Further, range sensor has been mounted equidistant in the fuselage side surface, and range sensor can monitor nobody
Object around machine, and judgment object avoids unmanned plane from colliding barrier and crash apart from unmanned plane distance.
Further, the landing aid device is divided into two support frames for being mounted on fuselage lower surface front and rear sides, the branch
Support and fuselage junction are equipped with damper, in unmanned plane landing, since communication base station has constant weight, so damper
The instantaneous pressure generated when can be to avoid unmanned plane landing causes landing aid device damage or communication base station to be collided.
Further, the scarer includes audio wave generator, and audio wave generator can issue what birds can not be resistant to
Sound wave, to be dispersed to the birds attempted close to unmanned plane, it is ensured that unmanned plane safe operation.
The working method of the utility model is: before the use, communication base station debugging being finished and is fixedly mounted on fuselage
Inside is taken off by control circuit board control unmanned plane and reaches designated position, and the first rotary wings group and the second rotary wings group pass through
First driving motor and the second driving motor are slided to adjust unmanned plane during flying direction in first sliding groove and second sliding slot,
The range sensor of unmanned aerial vehicle body side surface can make unmanned plane avoiding barrier, and the scarer of fuselage two sides can pass through sound
Wave producer issues birds and is difficult to the sound wave being resistant to, to disperse the birds attempted close to unmanned plane, in unmanned plane landing, helps
Damper on falling unit can mitigate vibration.
Compared with prior art, the utility model has the beneficial effects that a kind of novel dual rotary provided by the utility model
The high null base station of wing unmanned plane, being particularly suitable for the natural calamities such as earthquake, flood or Large Exhibitions, match, rally activity etc. can lead
The area for causing the communication service in a certain region not to be available in a certain period of time, by using bispin rotor UAV flight
Communication base station is sent to designated position, quickly and efficiently, and solar panel is arranged on unmanned plane, can made by communication base station
Communication base station comes into operation for a long time, is equipped with range sensor, can collide to avoid unmanned plane, is equipped with bird repellent dress
It sets, birds is avoided to damage close to unmanned plane to unmanned plane, meanwhile, unmanned plane can be revolved by the first rotary wings group and second
The collaborative work of rotor group carries out the adjusting of unmanned plane during flying angle.In short, the utility model has, load-carrying is big, adaptability is good,
The advantages that safe and efficient, at low cost.
Detailed description of the invention
Fig. 1 is the overall structure diagram of the utility model；
Fig. 2 is the utility model range sensor position view；
Fig. 3 is the system block diagram of the utility model；
Fig. 4 is the circuit diagram of the utility model.
Wherein, 1- fuselage, 2- communication base station, 3- control circuit board, the first rotary wings of 4- group, the first rotary wings of 41-, 42-
First drive rod, the first driving motor of 43-, 44- first sliding groove, the second rotary wings of 5- group, the second rotary wings of 51-, 52- second are passed
Lever, the second driving motor of 53-, 54- second sliding slot, 6- landing aid device, 61- support frame, 62- damper, 7- scarer,
71- audio wave generator, 8- solar panel, 9- range sensor, 10- power supply.
Specific embodiment
For convenient for the understanding to technical solutions of the utility model, 1-3 and specific embodiment are practical to this with reference to the accompanying drawing
Novel to be further explained explanation, embodiment does not constitute the restriction to scope of protection of the utility model.
As shown in Figure 1, a kind of novel high null base station of bispin rotor unmanned plane, mainly includes fuselage 1, communication base station 2, control
Circuit board 3, the first rotary wings group 4, the second rotary wings group 5, landing aid device 6, scarer 7 and power supply 10, communication base station 2 are fixed
It is mounted on the inside of fuselage 1, control circuit board 3 is electrically connected at the top of communication base station 2, and control circuit board 3 is also driven with first
Dynamic motor 43 and the second driving motor 53 are electrically connected, the first rotary wings group 4 include the first rotary wings 41, the first drive rod 42,
First driving motor 43 and first sliding groove 44, the first rotary wings 41 are mounted on the upper left side of fuselage 1,42 upper end of the first drive rod with
First rotary wings 41 are fixedly connected, and 42 lower end of the first drive rod is fixedly connected with the output shaft of the first driving motor 43, and first drives
Dynamic motor 43 is movably connected in 1 left side inner bottom of fuselage by first sliding groove 44, and the second rotary wings group 5 includes the second rotary wings
51, the second drive rod 52, the second driving motor 53 and second sliding slot 54, the second rotary wings 51 are mounted on the upper right side of fuselage 1, the
Two drive rods, 52 upper end is fixedly connected with the second rotary wings 51, the output shaft of 52 lower end of the second drive rod and the second driving motor 53
It is fixedly connected, the second driving motor 53 is movably connected in 1 right side inner bottom of fuselage by second sliding slot 54, and landing aid device 6 is pacified
Mounted in the lower section of fuselage 1, landing aid device 6 is divided to be mounted on two support frames 61 of 1 lower surface front and rear sides of fuselage, support frame 61
It is equipped with damper 62 with 1 junction of fuselage, scarer 7 is respectively symmetrically mounted on the left and right sides of fuselage 1 there are two being total to, and drives
Bird device 7 includes audio wave generator 71, and 1 upper surface middle part of fuselage is equipped with solar panel 8, as shown in Fig. 2, 1 side table of fuselage
Face has been mounted equidistant range sensor 9, power supply 10 altogether there are two, be separately positioned on 2 left and right sides of communication base station, solar battery
Plate 8 is connect with power supply 10, for charging to power supply 10.
The working method of the present embodiment are as follows: before the use, the debugging of communication base station 2 is finished and is fixedly mounted on fuselage 1
Inside is taken off by the control unmanned plane of control circuit board 3 and reaches designated position, and the first rotary wings group 4 and the second rotary wings group 5 are logical
It crosses the first driving motor 43 and the second driving motor 53 is slided in first sliding groove 44 and second sliding slot 54 to adjust nobody
Machine heading, the range sensor 9 of 1 side surface of unmanned aerial vehicle body can make unmanned plane avoiding barrier, the drive of 1 two sides of fuselage
Bird device 7 can issue birds by audio wave generator 71 and be difficult to the sound wave being resistant to, so that the birds attempted close to unmanned plane are dispersed,
In unmanned plane landing, the damper 61 on landing aid device 6 can mitigate vibration.
Finally, it should be noted that above embodiments are only to illustrate the technical solution of the utility model, rather than its limitations；
Although the utility model is described in detail with reference to the foregoing embodiments, those skilled in the art should understand that:
It can still modify to technical solution documented by previous embodiment, or be equal to part of technical characteristic
Replacement；And these are modified or replaceed, the utility model embodiment technical solution that it does not separate the essence of the corresponding technical solution
Spirit and scope.
Claims (5)
1. a kind of novel high null base station of bispin rotor unmanned plane, which is characterized in that mainly include fuselage (1), communication base station (2),
Control circuit board (3), the first rotary wings group (4), the second rotary wings group (5), landing aid device (6), scarer (7) and power supply
(10), the communication base station (2) is fixedly mounted on the inside of fuselage (1), and the control circuit board (3) is electrically connected at communication base
It stands the top of (2), the first rotary wings group (4) includes the first rotary wings (41), the first drive rod (42), the first driving motor
(43) and first sliding groove (44), first rotary wings (41) are mounted on the upper left side of fuselage (1), first drive rod (42)
Upper end is fixedly connected with the first rotary wings (41), the output shaft of the first drive rod (42) lower end and first driving motor (43)
It is fixedly connected, first driving motor (43) is movably connected in inner bottom on the left of fuselage (1) by the first sliding groove (44)
End, the second rotary wings group (5) include the second rotary wings (51), the second drive rod (52), the second driving motor (53) and the
Two sliding slots (54), second rotary wings (51) are mounted on the upper right side of fuselage (1), the second drive rod (52) upper end and the
Two rotary wings (51) are fixedly connected, and the output shaft of the second drive rod (52) lower end and second driving motor (53) is fixed to be connected
It connects, second driving motor (53) is movably connected in inner bottom on the right side of fuselage (1) by the second sliding slot (54), described
Landing aid device (6) is mounted on the lower section of fuselage (1), and the scarer (7) is respectively symmetrically mounted on fuselage (1) there are two being total to
The left and right sides, the power supply (10) altogether there are two, be separately positioned at left and right sides of communication base station (2).
2. a kind of novel high null base station of bispin rotor unmanned plane according to claim 1, which is characterized in that the control electricity
Road plate (3) is also electrically connected with the first driving motor (43) and the second driving motor (53).
3. a kind of novel high null base station of bispin rotor unmanned plane according to claim 1, which is characterized in that the fuselage
(1) upper surface middle part is equipped with solar panel (8), and the solar panel (8) and power supply (10) are electrically connected.
4. a kind of novel high null base station of bispin rotor unmanned plane according to claim 1, which is characterized in that described that drop is helped to fill
It sets (6) and is divided into two support frames (61) for being mounted on fuselage (1) lower surface front and rear sides, support frame as described above (61) and fuselage (1)
Junction is equipped with damper (62).
5. a kind of novel high null base station of bispin rotor unmanned plane according to claim 1, which is characterized in that the bird repellent dress
Setting (7) includes audio wave generator (71).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820994083.4U CN209008855U (en) | 2018-06-26 | 2018-06-26 | A kind of novel high null base station of bispin rotor unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820994083.4U CN209008855U (en) | 2018-06-26 | 2018-06-26 | A kind of novel high null base station of bispin rotor unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209008855U true CN209008855U (en) | 2019-06-21 |
Family
ID=66828041
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820994083.4U Expired - Fee Related CN209008855U (en) | 2018-06-26 | 2018-06-26 | A kind of novel high null base station of bispin rotor unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209008855U (en) |
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2018
- 2018-06-26 CN CN201820994083.4U patent/CN209008855U/en not_active Expired - Fee Related
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190621 Termination date: 20210626 |