CN209492705U - A kind of electronic fixed-wing unmanned plane of novel agricultural remote sensing - Google Patents
A kind of electronic fixed-wing unmanned plane of novel agricultural remote sensing Download PDFInfo
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- CN209492705U CN209492705U CN201920047120.5U CN201920047120U CN209492705U CN 209492705 U CN209492705 U CN 209492705U CN 201920047120 U CN201920047120 U CN 201920047120U CN 209492705 U CN209492705 U CN 209492705U
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- unmanned plane
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Abstract
The utility model discloses a kind of electronic fixed-wing unmanned planes of novel agricultural remote sensing, including body, dynamical system, avionics system, ground control system and mission payload system；The body is fixed wing structure, faster than what multi-rotor unmanned aerial vehicle flew, winged is long, and single-coverage area is big, operating efficiency is high, meanwhile influenced than multi-rotor unmanned aerial vehicle by weather, environment it is smaller, can carry out for a long time, the monitoring of multifrequency time, furthermore, the technology relative maturity of fixed-wing unmanned plane, reliability and safety are relatively high, and maintenance, running cost are lower；The dynamical system uses high-energy battery as power source, will not generate pollution to environment in use, meanwhile, influenced by height above sea level it is smaller while easy to operate, it is easy to maintain, further improve operating efficiency；The mission payload system includes multiple-task equipment, can acquire a variety of data of target area simultaneously, is more conducive to improving operating efficiency.
Description
Technical field
The utility model relates to air vehicle technique fields, and in particular to a kind of novel agricultural remote sensing with electronic fixed-wing nobody
Machine.
Background technique
Unmanned plane have the characteristics that it is motor-driven quickly, use cost is low, maintenance is using simple, therefore at home and abroad extensively
It is employed.But up to the present, because of the limitation of technology, unmanned plane does not obtain comprehensive application in actual use.
Unmanned plane currently on the market is mostly multi-rotor unmanned aerial vehicle absolutely, is all usually using multiple rotors in symmetrically setting
Meter cannot be by wind although such design flexibility with higher, overall structure simultaneously do not meet traditional aerodynamics
The lift and thrust that power generates.Meanwhile that there is also power wastes is big, load-carrying is small, flying speed is slow and continuous for multi-rotor unmanned aerial vehicle
Boat apart from it is short the deficiencies of, operating efficiency is lower in agricultural remote sensing.
Except multi-rotor unmanned aerial vehicle, also there are many traditional fixed-wing unmanned planes on the market, but these are fixed
Wing unmanned plane is mostly to use gasoline as power source.Although this unmanned plane can solve many of multi-rotor unmanned aerial vehicle
Defect, but that there is also engine vibrations is big, is influenced the problems such as serious, Operation and Maintenance is complicated, waste oil pollution by height above sea level, and uncomfortable
Agricultural remote sensing is closed to use.
So how to design a kind of unmanned plane that novel suitable agricultural remote sensing uses, become what we currently to be solved
Problem.
Utility model content
In view of this, the purpose of this utility model is to provide a kind of electronic fixed-wing unmanned plane of novel agricultural remote sensing,
To improve the efficiency of agricultural remote sensing operation.
The utility model is solved the above problems by following technological means: a kind of novel agricultural remote sensing with electronic fixed-wing without
It is man-machine, including body, dynamical system, avionics system, ground control system and mission payload system；The body include fuselage,
Wing, tail pipe, empennage and parachute, the wing are locked by bolt again after being inserted into back by fixation hole, institute
It is locked again by bolt after stating tail pipe insertion fuselage afterbody, the empennage is locked in tail pipe rear portion by self-locking mechanism；Institute
Stating dynamical system includes high-energy battery, the mechanical, electrical reconciliation propeller of electricity, and the high-energy battery is electrically connected with motor, and the electricity is mechanical, electrical
It is sequentially connected between reconciliation propeller；The avionics system is connect with ground control system signal.
Further, the wing includes left Duan Yiti, middle section wing body and right Duan Yiti, the left section of wing body and right Duan Yiti
Respectively by self-locking mechanism interlocking in the left and right ends of middle section wing body.
Further, the avionics system includes flight control modules, GPS module, power management module and body communication mould
Block.
Further, the ground control system includes ground control station and ground communication module, the ground communication module
It is connect with body communication module signal.
Further, the mission payload system includes the mission payload power supply electricly connected, mission payload control and task
Equipment.
Further, the task device includes Visible Light Camera, multispectral camera and thermal infrared imager.
Further, the mission payload storehouse for accommodating mission payload system is provided on the fuselage.
Further, multiple data acquisition window mouths are provided on the fuselage.
Further, the fore-body is provided with the battery compartment for accommodating high-energy battery, and the mechanical, electrical reconciliation propeller of electricity is equal
It is mounted in the wing body of middle section, outside motor is equipped with pod.
Further, parachute storehouse is provided on the fuselage.
The utility model has the beneficial effects that
1, it is equipped with multiple-task equipment simultaneously, a variety of data of target area can be acquired simultaneously.
2, use high-energy battery as power source, pollution will not be generated to environment in use.
3, use motor as propulsion system, smaller while easy to operate, maintenance side is influenced by height above sea level
Just.
4, fixed-wing unmanned plane is faster than what multi-rotor unmanned aerial vehicle flew, and winged is long, and single-coverage area is big, and operating efficiency is high.
5, fixed-wing unmanned plane is influenced than multi-rotor unmanned aerial vehicle by weather, environment smaller, can carry out long-time, multifrequency
Secondary monitoring.
6, the technology relative maturity of fixed-wing unmanned plane, reliability and safety are relatively high, and maintenance, running cost are lower.
Detailed description of the invention
The utility model is further described with reference to the accompanying drawings and examples.
Fig. 1 is the perspective view of the utility model；
Fig. 2 is the left view of the utility model；
Fig. 3 is the bottom view of the utility model；
Fig. 4 is the top view of the utility model；
Fig. 5 is the system structure diagram of the utility model；
Fig. 6 is the operation schematic diagram of the utility model.
In figure: the left Duan Yiti of 1-1--；The middle section 1-2-- wing body；The right Duan Yiti of 1-3--；2-- fuselage；2-1-- battery compartment；2-
2-- mission payload storehouse；2-3-- parachute storehouse；3-- tail pipe；4-- empennage；5-- parachute；6-- data acquisition window mouth；7-- high energy
Battery；8-- motor；9-- electricity tune；10-- propeller；11-- ground control station；12-- ground communication module.
Specific embodiment
For the ease of understanding the utility model, below in conjunction with Figure of description and preferred embodiment to the utility model
Work more comprehensively, meticulously describes, but the protection scope of the utility model is not limited to embodiment in detail below.
Embodiment 1
Such as Fig. 1-6, the electronic fixed-wing unmanned plane of the novel agricultural remote sensing, including body, dynamical system, avionics system
System, ground control system and mission payload system.The body includes fuselage 2, wing, tail pipe 3, empennage 4 and parachute 5；Institute
The front for stating fuselage 2 is provided with battery compartment 2-1, and the rear portion of fuselage 2 is provided with the parachute storehouse 2-3 for accommodating parachute；The machine
The wing includes left section of wing body 1-1, middle section wing body 1-2 and right section of wing body 1-3, and the left section of wing body 1-1 and right section of wing body 1-3 lead to respectively
Self-locking mechanism interlocking is crossed in the left and right ends of middle section wing body 1-2, wing passes through again after being inserted into back entirely through fixation hole
Bolt is locked；It is locked again by bolt after the tail pipe insertion fuselage afterbody, the empennage is locked by self-locking mechanism
It is scheduled on tail pipe rear portion；The parachute is arranged in parachute storehouse.The dynamical system includes high-energy battery 7, motor 8, electricity tune 9
With propeller 10, the high-energy battery is electrically connected with motor, and high-energy battery is contained in battery compartment, the mechanical, electrical reconciliation spiral shell of electricity
It being sequentially connected between rotation paddle, propeller rotational is driven by motor, the mechanical, electrical reconciliation propeller of electricity is installed in the wing body of middle section,
Outside motor is equipped with pod, so as to rapid cooling.The avionics system includes flight control modules, GPS module, power supply pipe
Manage module and body communication module, the ground control system includes ground control station 11 and ground communication module 12, describedly
Face communication module is connect with body communication module signal.GPS module can acquire the unmanned plane institute provided by GPS satellite in real time
The three dimensional local information (longitude, dimension, height) at place；Flight control modules are according to the task route imported in advance or in real time, control
Unmanned plane processed, which is arranged under the accurate positioning of GPS module according to task course line, to fly；Body communication module is then by aerial nobody
Machine is connected with ground control station, and the parameters such as the speed of unmanned plane, height, coordinate, three shaft angle degree are passed back to ground control in real time
System station, can also be by the operation real-time delivery of the ground handling operator received to flight control modules.In ground control system,
Ground control station is connected with ground communication module；Ground staff can monitor the flight of unmanned plane in real time by ground control station
State, it is necessary to when state of flight or route can be corrected immediately.The mission payload system includes times electricly connected
Business load power supply, mission payload controls and task device, and the mission payload storehouse 2- for accommodating mission payload system is provided on fuselage
2, the task device includes Visible Light Camera, multispectral camera and thermal infrared imager.
The specific implementation of the utility model the following steps are included:
1) before unmanned plane carries out operation, unmanned plane each section should comprehensively be checked；
2) after inspection is errorless, unmanned plane is given to carry out power on operation, GPS module automatically begins to carry out satellite positioning；
3) after the completion of positioning, ground handling operator is by ground control station editor task route, and editor is after the completion by logical
Letter module is uploaded to the flight control modules of unmanned plane；
4) after the completion of course line uploads, can carry out takeoff operational: the motor being fixed on wing starts to start, on motor
Propeller rotates, and generates thrust backward；Unmanned plane main body uses bullet under the action of airfoil lift and motor thrust
The mode for penetrating or sliding race is gone up to the air flight；
5) after unmanned plane takes off, flight control modules control unmanned plane and spiral in takeoff point according to the setting of takeoff pattern
And hoisting depth, until reaching operation flight height；
6) after reaching operation flight height, flight control modules are switched to task course line, control unmanned plane according to setting
Task course line and specified air speed carry out Mission Operations flight；
7) after reaching specified region, the task device that flight control modules control is carried carries out data acquisition；
8) after fulfiling assignment, flight control modules are switched to course back, and control unmanned plane returns to the overhead of takeoff point
It spirals and reduces height；
9) after the completion of confirmation task, ground handling operator is controlled unmanned plane and is dropped in a manner of sliding race or parachuting
It falls.
In conclusion the novel agricultural remote sensing of the application electronic fixed-wing unmanned plane, including body, dynamical system, boat
Electric system, ground control system and mission payload system；The body is fixed wing structure, faster than what multi-rotor unmanned aerial vehicle flew,
Winged is long, and single-coverage area is big, and operating efficiency is high, meanwhile, influenced than multi-rotor unmanned aerial vehicle by weather, environment it is smaller, can
To carry out the secondary monitoring of long-time, multifrequency, furthermore, the technology relative maturity of fixed-wing unmanned plane, reliability and safety are compared
Height, maintenance, running cost are lower；The dynamical system uses high-energy battery as power source, will not be right in use
Environment generate pollution, meanwhile, influenced by height above sea level it is smaller while easy to operate, it is easy to maintain, further improve work
Industry efficiency；The mission payload system includes multiple-task equipment, can acquire a variety of data of target area simultaneously, advantageously
In raising operating efficiency.
Embodiment 2
The present embodiment difference from example 1 is that: multiple data acquisition window mouths 6 are provided on fuselage, each
Data acquisition window mouth corresponds to different task devices, then can pass in and out and acquire to a variety of data simultaneously, substantially increase data and adopt
Collect efficiency and operating efficiency.
Finally, it is stated that above embodiments are merely intended for describing the technical solutions of the present application, but not for limiting the present application, although ginseng
The utility model is described in detail according to preferred embodiment, those skilled in the art should understand that, it can be to this
The technical solution of utility model is modified or replaced equivalently, without departing from the objective and model of technical solutions of the utility model
It encloses, should all cover in the scope of the claims of the utility model.
Claims (10)
1. a kind of electronic fixed-wing unmanned plane of novel agricultural remote sensing, it is characterised in that: including body, dynamical system, avionics system
System, ground control system and mission payload system；The body includes fuselage, wing, tail pipe, empennage and parachute, the machine
The wing is locked by bolt again after being inserted into back by fixation hole, passes through bolt again after the tail pipe insertion fuselage afterbody
It is locked, the empennage is locked in tail pipe rear portion by self-locking mechanism；The dynamical system include high-energy battery, electricity it is mechanical, electrical
Reconciliation propeller, the high-energy battery are electrically connected with motor, are sequentially connected between the mechanical, electrical reconciliation propeller of electricity；The boat
Electric system is connect with ground control system signal.
2. the electronic fixed-wing unmanned plane of novel agricultural remote sensing according to claim 1, it is characterised in that: the wing packet
Left Duan Yiti, middle section wing body and right Duan Yiti are included, the left section of wing body and right section of wing body pass through self-locking mechanism interlocking in respectively
The left and right ends of Duan Yiti.
3. the electronic fixed-wing unmanned plane of novel agricultural remote sensing according to claim 2, it is characterised in that: the avionics system
System includes flight control modules, GPS module, power management module and body communication module.
4. the electronic fixed-wing unmanned plane of novel agricultural remote sensing according to claim 3, it is characterised in that: the ground control
System processed includes ground control station and ground communication module, and the ground communication module is connect with body communication module signal.
5. the electronic fixed-wing unmanned plane of novel agricultural remote sensing according to claim 4, it is characterised in that: the task carries
G system includes the mission payload power supply electricly connected, mission payload control and task device.
6. the electronic fixed-wing unmanned plane of novel agricultural remote sensing according to claim 5, it is characterised in that: the task is set
Standby includes Visible Light Camera, multispectral camera and thermal infrared imager.
7. the electronic fixed-wing unmanned plane of novel agricultural remote sensing according to claim 6, it is characterised in that: on the fuselage
It is provided with the mission payload storehouse for accommodating mission payload system.
8. the electronic fixed-wing unmanned plane of novel agricultural remote sensing according to claim 7, it is characterised in that: on the fuselage
It is provided with multiple data acquisition window mouths.
9. the electronic fixed-wing unmanned plane of novel agricultural remote sensing according to claim 2, it is characterised in that: before the fuselage
Portion is provided with the battery compartment for accommodating high-energy battery, and the mechanical, electrical reconciliation propeller of electricity is installed in the wing body of middle section, outside motor
Pod is installed.
10. novel agricultural remote sensing described in -9 any one is existed with electronic fixed-wing unmanned plane, feature according to claim 1
In: parachute storehouse is provided on the fuselage.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920047120.5U CN209492705U (en) | 2019-01-11 | 2019-01-11 | A kind of electronic fixed-wing unmanned plane of novel agricultural remote sensing |
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| CN201920047120.5U CN209492705U (en) | 2019-01-11 | 2019-01-11 | A kind of electronic fixed-wing unmanned plane of novel agricultural remote sensing |
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| CN209492705U true CN209492705U (en) | 2019-10-15 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109625268A (en) * | 2019-01-11 | 2019-04-16 | 北京云影飞扬科技有限公司 | A kind of electronic fixed-wing unmanned plane of novel agricultural remote sensing |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109625268A (en) * | 2019-01-11 | 2019-04-16 | 北京云影飞扬科技有限公司 | A kind of electronic fixed-wing unmanned plane of novel agricultural remote sensing |
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| TR01 | Transfer of patent right |
Effective date of registration: 20220406 Address after: 100195 Room 301, 3 / F, building 5, zone 4, Xishan Creative Park, Haidian District, Beijing Patentee after: Aerospace Hongtu Information Technology Co.,Ltd. Address before: 101399 Room 501, 5 / F, 101, building 3, courtyard 11, Tengren Road, Niulanshan Town, Shunyi District, Beijing Patentee before: BEIJING YUNYING TECHNOLOGY Co.,Ltd. |