CN206654197U - Unmanned plane in a kind of Multifunctional air - Google Patents
Unmanned plane in a kind of Multifunctional air Download PDFInfo
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- CN206654197U CN206654197U CN201720122306.3U CN201720122306U CN206654197U CN 206654197 U CN206654197 U CN 206654197U CN 201720122306 U CN201720122306 U CN 201720122306U CN 206654197 U CN206654197 U CN 206654197U
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Abstract
The utility model discloses unmanned plane in a kind of Multifunctional air, including controller, aircraft, and the aircraft includes：Module is investigated, communications relay module, module is thrown, main control module, is connected with the controller by 2.4G Radio Transmission Technologys, and is connected with the investigation module, the communications relay module, the throwing module, for being controlled in real time and data processing；Power plant module, it is connected with investigation module, the communications relay module, the throwing module and the main control module to provide electric energy, also provides for energy needed for the aircraft flight；The throwing module includes：Fixed structure, including first fixed structure and the second fixed structure, second fixed structure are used for fixation and treat object-throwing；Slide construction, it is fixed on the first fixed structure；First track, below the slide construction；Second track, it is connected with first track, object carries out periodicity accelerated motion in second track.
Description
Technical field
It the utility model is related to unmanned plane field, and in particular to unmanned plane in a kind of Multifunctional air.
Background technology
Unmanned plane, it is the not manned aircraft manipulated using radio robot and the presetting apparatus provided for oneself.At present
Unmanned plane using quite varied, is made that very big in terms of agricultural production, mapping and national defence to expanding economy and national defence
Contribution, particularly when carrying out long-range goods and materials and supporting, unmanned plane can be deep into the area that ground staff can not arrive at
Carry out throwing the action such as goods and materials.But the design hommization not enough of traditional unmanned plane on the market now, function is relatively simple, and
And can be disturbed by many external environments, can only realize mostly shooting record function, in the case of dark often because
Light is too dim, and the effect of record can be made to be deteriorated, influence follow-up work.And unmanned plane is when remotely being thrown
The height above sea level that can only be fixed above target area carries out the throwing of goods and materials, can not be in distance objective region farther out local complete
Into the task of throwing, influence goods and materials and throw operating efficiency.
In view of drawbacks described above, the utility model creator obtains this practicality newly finally by prolonged research and practice
Type.
Utility model content
To solve above-mentioned technological deficiency, the technical solution adopted in the utility model is, there is provided nothing in a kind of Multifunctional air
It is man-machine, including a controller, an aircraft, the aircraft include：
One investigation module, for being carried out investigations to mission area surface state；
One communications relay module, for carrying out emergency communication to mission area；
One throws module, for that will treat that object-throwing is thrown in the air；
One main control module, be connected with the controller by 2.4G Radio Transmission Technologys, and with the investigation module, described
Communications relay module, the throwing module are connected, for being controlled in real time and Data Management Analysis；
One power plant module, with investigation module, the communications relay module, the throwing module and the master control mould
Block is connected to provide electric energy, also provides for energy needed for the aircraft flight；
The throwing module includes：
One fixed structure, including first fixed structure and the second fixed structure, second fixed structure are used to fix
Treat object-throwing；
One slide construction, it is fixed on the first fixed structure, is conveyed for treating object-throwing；
One first track, below the slide construction；
One second track, it is connected with first track, treats that object-throwing enters described second through first track
Track, and periodicity accelerated motion is carried out in second track.
Preferably, the center line tracking y of second track is：
Wherein, for line point apart from the radian of the second orbit centre point, e is natural constant centered on x.
Preferably, the investigation module includes varifocal camera, infrared thermography and GPS locator, the control
The angle rotation of the digital zoom of varifocal camera, angle rotation and the infrared thermography described in device remote control processed
Turn, and the switching between the varifocal camera and the infrared thermography, the GPS locator are used to position in real time
And send data to the main control module, the main control module carries out data processing, draw the height in distance objective region with
Horizontal range.
Preferably, second fixed structure is mechanical hook, weight sensor is provided with the mechanical hook, is used for
Detection treats the weight of object-throwing and sends data to the main control module, and the main control module carries out data processing, draws
Treat the acceleration needed for object-throwing.
Preferably, being provided with accelerator and acceleration transducer in second track, the accelerator is used to treat
Object-throwing accelerates, and the acceleration transducer is used to detect the acceleration for treating object-throwing and sends data to the master control
Module, the main control module will treat the acceleration of object-throwing, compared with required acceleration, reach required acceleration
Afterwards, then the accelerator stops treating object-throwing acceleration.
Preferably, the investigation module also includes radar life-detection instrument, the radar life-detection instrument is Active Radar
Life-detection instrument, the human body limb fine motion within the aircraft circumference 360m can be detected in open space, obstacle be present
The human body limb fine motion in 15m behind barrier can be detected during thing.
Preferably, the communications relay module includes ultrashort wave u section analog repeaters, touched by the controller frequency difference
Hair, realizes relay function, emergency communication is realized in mission area.
Preferably, the power plant module includes lithium battery and motor, the aircraft also includes horn, set on the horn
Blade is equipped with, the motor is corresponded with the blade and set, and the lithium battery is used for the main control module, the investigation
Module, the communications relay module and the throwing module provide electric energy.
Preferably, first track is the cavity of upper opening, the upper opening extends first level to both sides
Portion and the second horizontal part, the length of second horizontal part are more than the length in the first level portion.
Preferably, the second horizontal part end is provided with baffle plate, the second horizontal part end height is higher than described the
The height of the opposite end of two horizontal part ends.
The beneficial effects of the utility model are compared with the prior art：1, throw module and be provided with the first track and the
Two tracks, the guarantee of the first track treat that object-throwing can smoothly enter the second track, and the center line of the second track is similar to cosine
Function so that treat that object-throwing carries out periodicity accelerated motion in less space so that treat needed for object-throwing acquisition
Acceleration, realize remote accurate throwing；2, unmanned plane includes investigation module, communications relay module and throwing module etc., work(
Can be diversified, and investigate module and be provided with varifocal camera and thermal infrared imager, it can realize remote and night
Investigation, and both can switch in real time.
Brief description of the drawings
In order to illustrate more clearly of the technical scheme in various embodiments of the utility model, institute in being described below to embodiment
The accompanying drawing needed to use is briefly described.
Fig. 1 is the structural representation of the aircraft of unmanned plane in the utility model Multifunctional air；
Fig. 2 is the structural representation of the throwing module of unmanned plane in the utility model Multifunctional air；
Fig. 3 is the functional schematic of unmanned plane in the utility model Multifunctional air；
Embodiment
Below in conjunction with accompanying drawing 1-3, and other technical characteristic above-mentioned to the utility model and advantage are made in more detail
It is bright.
Embodiment one
The utility model provides unmanned plane in a kind of Multifunctional air, including controller 10 and aircraft.
The aircraft includes cabin 1, and horn 2, empennage 3, undercarriage 4, the quantity of the horn 2 is preferably four, institute
Horn 2 is stated to set using axial symmetry.The end of the horn 2 is provided with blade 21, the blade 21 include the first blade with
And second blade, first blade is identical with the structure of second blade, is helical blade, using spiral shape
Blade can effectively avoid the blade 21 from intense shock wave occur in the case where high speed rotates, and improve the efficiency of blade 21.It is described to rise and fall
Frame 4 uses ski type structure, and resistance is small, less demanding to landing place, and such as more smooth ground or meadow can meet to drop
Fall requirement.
The aircraft also includes power plant module 5, investigation module 6, communications relay module 7, throwing module 8 and master control
Module 9.
The main control module 9 is single-chip microcomputer, is arranged in the cabin 1, the single-chip microcomputer respectively with the investigation module
6th, the communications relay module 7, the throwing module 8 and the power plant module 5 are connected, for realizing to the aircraft
The control of each module；The single-chip microcomputer is connected with the controller 10 by 2.4G Radio Transmission Technologys.
The power plant module 5 includes lithium battery 51 and motor 52, the lithium battery 51 be used for the main control module 9,
The investigation module 6, the communications relay module 7 and the throwing module 8 provide electric energy, are arranged in the cabin 1.Institute
State motor 52 and correspond setting with the blade 21, the motor 52 is connected with the blade 21, for providing described fly
The kinetic energy of row device flight.
The investigation module 6 includes varifocal camera 61, infrared thermography 62, radar life-detection instrument 62, GPS
Locator 64, the varifocal camera 61 can realize the investigation of different distance by regulating and controlling the focal length of camera, pass through institute
Stating infrared thermography 62 can realize that night search is investigated.Varifocal camera 61 described in the remote control of controller 10
Digital zoom, the angle spinfunction of angle spinfunction and the infrared thermography 62, and described varifocal take the photograph
As the switching between first 61 and the infrared thermography 62.The radar life-detection instrument 62 detects for active radar life
Instrument, the Active Radar survey meter are that it leads in the life detection equipment of one using Radar Technology, biomedical engineering technology
The principle of reflection of electromagnetic wave is utilized to be made, by detecting the various fine motions caused by human life activity, from these fine motions
Breathed, heartbeat for information about, whether there is life so as to recognize.Active Radar life-detection instrument energy in open space
The human body limb fine motion within the aircraft circumference 360m is enough detected, building reinforced concrete wall, steel casement door, tree can be penetrated
The barriers such as wood, the human body limb fine motion in 15m behind barrier can be detected when barrier be present, to life entity target
Reaction time is no more than 30 seconds, quick detection vital sign, is raced against time for rescue.The GPS locator 64 can be right in real time
The aircraft is positioned, when discovery needs to rescue object, the location information sent by the GPS locator 64, energy
Enough quick carry out are rescued.
The communications relay module 7 includes ultrashort wave u sections analog repeater 71, is triggered by the frequency difference of controller 10,
Relay function is realized, is set up using the high-altitude of unmanned plane to realize the ultrashort wave relay forwarding function in complicated landform environment, from
And realize in mission area, emergency communication, it is ensured that People's Armed Police communicates unimpeded in the tasks carrying of particular surroundings.
The throwing module 8 is located in the cabin 1, including first fixed structure 81, slide construction 82, the second fixed knot
Structure 83, the first track 84, the second track 85.In the present embodiment, it is preferred that the first fixed structure 81 is fix bar, institute
It is slide rail to state slide construction 82, and second fixed structure 83 is mechanical hook.The fix bar upper surface is fixedly installed on institute
The top of cabin 1 is stated, the fix bar lower surface is fixedly connected with the slide rail, and multiple machineries are provided with the slide rail
Hook, object are placed on the slide rail by the mechanical hook, are transmitted by controller 10 to the single-chip microcomputer and are thrown life
Order, the mechanical hook enter line slip along the slide rail, when the mechanical hook reaches consolidating for the top of the first track 84
Determine opening position, the hook portion of the mechanical hook rotates so that object enters second track 85 by first track 84,
First track 84 is the cavity of upper opening, and the upper opening extends first level portion 841 and second to both sides
Horizontal part 842, the length of second horizontal part 842 are much larger than the length in the first level portion 841.Second horizontal part
842 ends are provided with baffle plate, and second horizontal part 842 is located at the lower section of hanging object, accordingly even when hanging object is not
Reaching and just inadvertently fallen off at the upper opening of first track 84, the setting of second horizontal part 842 can also accept object,
And the baffle plate being capable of motion of the blocking object to opposite direction so that object eventually enters into second track 85.Further,
Height at the end stop of second horizontal part 842 can be slightly above the height of the opposite end of the end of the second horizontal part 842
Degree so that the object in second horizontal part 842 that drops can enter second track 85 faster.First track
841st, the setting of the first level portion 841 and second horizontal part 842 causes the aircraft even in high-speed flight
Or in the case of jolting, object being capable of the stable and accurate initiating terminal into second track 85.Second track
85 ends are connected with slot, and object is entered outside the cabin 1 by the slot.The center line rail of second track 85
Mark y is：
Wherein, centered on x line point apart from the central point of the second track 85 (center line and water of second track 85
Square to center line intersection point) radian, e is natural constant.
The center line tracking of second track 85 is similar to cosine curve, has cyclically-varying trend, each cycle
All there is crest segment and paddy section accordingly, be provided with acceleration transducer in each crest segment, acceleration is provided with each paddy section
Device, weight sensor is provided with the mechanical hook 83, the weight of hanging object and institute is sent data to for detecting
Single-chip microcomputer is stated, based on the real-time positioning of the GPS locator 64, the single-chip microcomputer carries out data processing, calculates distance and throws mesh
Mark the height and horizontal range in region.The aircraft is additionally provided with air velocity transducer, and data are carried out for the single-chip microcomputer
The influence of wind speed is considered during processing, in air-drop, object is broadly divided into inertia motion stage and freely falling body stage, will be certainly
After the horizontal range that can be advanced by the falling bodies stage deducts, the single-chip microcomputer is based on horizontal range and altitude information continues
Calculate, obtain the acceleration needed for object so that object can be thrown into target area under required acceleration.Object is in institute
State the second track 85 and carry out periodicity accelerated motion, the accelerator is used to accelerate object, the acceleration transducer
The acceleration of object-throwing is treated for detecting and sends data to the single-chip microcomputer, the single-chip microcomputer will treat adding for object-throwing
Speed is compared with required acceleration, and after object reaches required acceleration, the accelerator no longer enters to object
Row accelerates.
In the prior art, it is necessary to be thrown specifying above target, in reality when air-drop by unmanned plane
Due to the reason such as weather or artificial conflict so that need throwing objective area to be difficult to approach so that air-drop can not be carried out.This reality
With new by setting the first track 84 so that need dropped object smoothly to enter second track 85, second track
85 track, which is set, reaching a larger acceleration after second track 85 after dropped object so that long distance
Become possible to from air-drop.Second track 85 has periodic crest segment and paddy section, in less space so that object
Can periodically it be moved, the single-chip microcomputer is calculated by data obtains accurate required acceleration magnitude, second rail
Road 85 causes object to carry out periodicity acceleration in the presence of accelerator and is finally reached required acceleration so that object energy
It is enough to carry out remote accurate throwing.Can be smart at a distance by progress such as police pinking bullet, rescue ropes by the throwing module 8
Really throw.
In the utility model Multifunctional air unmanned plane be provided with it is described investigation module 6, the communications relay module 7 and
Described throwing module 8 etc., functional diversities, can be carried out investigations, rescue, and goods and materials are launched etc., and the investigation module 6 is provided with
The varifocal camera 61 and the thermal infrared imager 62, the investigation at night can be easy to investigating apart from real-time monitoring
Work, and both can switch in real time；The throwing module 8 is provided with first track 84 and second track 85, institute
State the first track 84 to ensure to treat that object-throwing can smoothly enter second track 85, the center line of second track 85 is near
It is similar to cosine function so that treat that object-throwing carries out periodicity accelerated motion in less space so that treat that object-throwing obtains
Acceleration necessarily is obtained, realizes remote accurate throwing.
Preferred embodiment of the present utility model is the foregoing is only, is merely illustrative for the utility model, and
It is nonrestrictive.Those skilled in the art understanding, can be to it in the spirit and scope that the utility model claims are limited
Many changes are carried out, are changed, in addition it is equivalent, but fall within the scope of protection of the utility model.
Claims (10)
1. unmanned plane in a kind of Multifunctional air, including a controller, an aircraft, it is characterised in that the aircraft includes：
One investigation module, for being carried out investigations to mission area surface state；
One communications relay module, for carrying out emergency communication to mission area；
One throws module, for that will treat that object-throwing is thrown in the air；
One main control module, it is connected with the controller by 2.4G Radio Transmission Technologys, and module, the communication is investigated with described
Trunk module, the throwing module are connected, for being controlled in real time and Data Management Analysis；
One power plant module, with investigation module, the communications relay module, the throwing module and the main control module phase
Connection also provides for energy needed for the aircraft flight to provide electric energy；
The throwing module includes：
One fixed structure, including first fixed structure and the second fixed structure, second fixed structure, which is used for fixation, to be waited to throw
Throw object；
One slide construction, it is fixed on the first fixed structure, is conveyed for treating object-throwing；
One first track, below the slide construction；
One second track, it is connected with first track, treats that object-throwing enters second track through first track,
And periodicity accelerated motion is carried out in second track.
2. unmanned plane in Multifunctional air as claimed in claim 1, it is characterised in that the center line tracking y of second track
For：
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Wherein, for line point apart from the radian of the second orbit centre point, e is natural constant centered on x.
3. unmanned plane in Multifunctional air as claimed in claim 1 or 2, it is characterised in that the investigation module includes varifocal
Camera, infrared thermography and GPS locator, the numeral change of varifocal camera described in the controller remote control
Burnt, angle rotation and the angle rotation of the infrared thermography, and the varifocal camera and the infrared heat into
As the switching between instrument, the GPS locator is used to position in real time and send data to the main control module, the master control mould
Block carries out data processing, draws the height and horizontal range in distance objective region.
4. unmanned plane in Multifunctional air as claimed in claim 3, it is characterised in that second fixed structure is hung for machinery
Hook, weight sensor is provided with the mechanical hook, the weight of object-throwing is treated for detecting and is sent data to described
Main control module, the main control module carry out data processing, draw the acceleration treated needed for object-throwing.
5. unmanned plane in Multifunctional air as claimed in claim 4, it is characterised in that be provided with accelerator in second track
And acceleration transducer, the accelerator are used to treat object-throwing acceleration, the acceleration transducer is used to detect to wait to throw
To throw the acceleration of object and send data to the main control module, the main control module will treat the acceleration of object-throwing, with
Required acceleration is compared, and after reaching required acceleration, then the accelerator stops treating object-throwing acceleration.
6. unmanned plane in Multifunctional air as claimed in claim 3, it is characterised in that the investigation module also includes radar life
Survey meter, the radar life-detection instrument are active radar life-detection instrument, and the aircraft can be detected in open space
Human body limb fine motion within circumference 360m, the human body limb that can be detected behind barrier in 15m when barrier be present are micro-
It is dynamic.
7. unmanned plane in Multifunctional air as claimed in claim 6, it is characterised in that the communications relay module includes ultrashort wave
U section analog repeaters, triggered by the controller frequency difference, realize relay function, emergency communication is realized in mission area.
8. unmanned plane in Multifunctional air as claimed in claim 5, it is characterised in that the power plant module includes lithium battery and electricity
Machine, the aircraft also include horn, and blade is provided with the horn, and the motor is corresponded with the blade and set,
The lithium battery is used to carry to the main control module, the investigation module, the communications relay module and the throwing module
Power supply energy.
9. unmanned plane in Multifunctional air as claimed in claim 3, it is characterised in that first track is the sky of upper opening
Chamber, the upper opening extend first level portion and the second horizontal part to both sides, and the length of second horizontal part is more than
The length in the first level portion.
10. unmanned plane in Multifunctional air as claimed in claim 9, it is characterised in that the second horizontal part end is provided with
Baffle plate, height of the second horizontal part end height higher than the opposite end of the second horizontal part end.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720122306.3U CN206654197U (en) | 2017-02-10 | 2017-02-10 | Unmanned plane in a kind of Multifunctional air |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720122306.3U CN206654197U (en) | 2017-02-10 | 2017-02-10 | Unmanned plane in a kind of Multifunctional air |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206654197U true CN206654197U (en) | 2017-11-21 |
Family
ID=60314077
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720122306.3U Expired - Fee Related CN206654197U (en) | 2017-02-10 | 2017-02-10 | Unmanned plane in a kind of Multifunctional air |
Country Status (1)
| Country | Link |
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| CN (1) | CN206654197U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108668257A (en) * | 2018-04-28 | 2018-10-16 | 中国人民解放军陆军工程大学 | Distributed unmanned aerial vehicle postman difference relay trajectory optimization method |
| CN110941284A (en) * | 2019-11-20 | 2020-03-31 | 黄锦山 | Relay network deployment method based on unmanned aerial vehicle and ground station equipment |
| CN112386832A (en) * | 2020-12-01 | 2021-02-23 | 安徽信息工程学院 | Fire rescue unmanned aerial vehicle |
-
2017
- 2017-02-10 CN CN201720122306.3U patent/CN206654197U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108668257A (en) * | 2018-04-28 | 2018-10-16 | 中国人民解放军陆军工程大学 | Distributed unmanned aerial vehicle postman difference relay trajectory optimization method |
| CN110941284A (en) * | 2019-11-20 | 2020-03-31 | 黄锦山 | Relay network deployment method based on unmanned aerial vehicle and ground station equipment |
| CN112386832A (en) * | 2020-12-01 | 2021-02-23 | 安徽信息工程学院 | Fire rescue unmanned aerial vehicle |
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