CN209023117U - A kind of teaching unmanned plane - Google Patents
A kind of teaching unmanned plane Download PDFInfo
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- CN209023117U CN209023117U CN201821758931.8U CN201821758931U CN209023117U CN 209023117 U CN209023117 U CN 209023117U CN 201821758931 U CN201821758931 U CN 201821758931U CN 209023117 U CN209023117 U CN 209023117U
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- unmanned plane
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- mounting hole
- driving device
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Abstract
The utility model discloses a kind of teaching unmanned plane, including rack, the rack further includes fuselage and horn, and one end of the horn is connect with the fuselage；Power plant module, is set to the other end of the horn and can generate and communicated to connect between flying power control module, with the power plant module by the horn, controls the flight of the unmanned plane.
Description
Technical field
The utility model relates to the technical field of unmanned machine equipment more particularly to a kind of teaching unmanned planes.
Background technique
" unmanned plane " is the abbreviation of " push-button aircraft ", is unmanned, automatic program control flight on a kind of machine
With wireless remotecontrol vectored flight, with the certain task ability of execution, reusable aircraft
Domestic unmanned plane develops in recent years than very fast, and in addition to military use, due to unmanned plane advantage of lower cost, nothing
The advantage that casualties risk, survival ability are strong, mobility is good, easy to use etc., so that unmanned plane is taken pictures in aviation, geology
Measurement, ultra-high-tension power transmission line tour, oil filed pipeline inspection, freeway management, forest fire protection inspection, poison gas prospecting, drug law enforcement and
The civil fields application prospect such as emergency management and rescue, rescue is extremely wide.
Therefore technologically advanced, different properties, widely used various novel unmanned machines continuously emerge.The unmanned plane in China
Development speed is exceedingly fast, and related needs sharply increase, and many productions and equipment are very in short supply using the manipulation talent of unmanned plane unit,
And the mechanism that systematic cultivation unmanned plane control staff is capable of in the country is very rare.
Utility model content
The purpose of this section is to summarize some aspects of the embodiments of the present invention and briefly introduce it is some preferably
Embodiment.It may do a little simplified or be omitted to keep away in this part and the summary of the description of the application and utility model title
The purpose for exempting to make this part, abstract of description and utility model title is fuzzy, and this simplification or omission cannot be used for limitation originally
The range of utility model.
In view of above-mentioned existing problem, the utility model is proposed.
Therefore, the utility model aim is to provide a kind of teaching unmanned plane.
In order to solve the above technical problems, the utility model provides the following technical solutions: a kind of teaching unmanned plane, including machine
Frame, the rack further include fuselage and horn, and one end of the horn is connect with the fuselage；Power plant module is set to described
It the other end of horn and can generate between flying power control module, with the power plant module through the horn communication link
It connects, controls the flight of the unmanned plane.
A kind of preferred embodiment as teaching unmanned plane described in the utility model, in which: the rack further includes connection
End, foot prop and installation end；The connecting pin is set to one end of the horn, and installation corresponding with the fuselage；It is described
Installation end is set to the other end of the horn, and for installing the power plant module, the foot prop is set to the horn
Lower section supports the horn.
A kind of preferred embodiment as teaching unmanned plane described in the utility model, in which: the power plant module further includes
Driving device and blade；The blade is set on the output shaft of the driving device.
A kind of preferred embodiment as teaching unmanned plane described in the utility model, in which: the installation end further includes column
Slot, the first mounting hole, extending column, the second mounting hole；The driving device of top is set in the column slot by described the
One mounting hole is fixed；The extending column is set to the bottom of the column slot, and second mounting hole is arranged on the extending column.
A kind of preferred embodiment as teaching unmanned plane described in the utility model, in which: the installation end further includes solid
Fixed board, the fixed plate further include third mounting hole, third through-hole and the 4th mounting hole；Pass through the third mounting hole and institute
State the corresponding installation of the second mounting hole；The driving device of lower section is installed by the 4th mounting hole.
A kind of preferred embodiment as teaching unmanned plane described in the utility model, in which: the is also set up in the column slot
One through-hole and the second through-hole；The route of the control module is discharged into the horn and by the institute of the first through hole and top
Driving device connection is stated, and is connected by the driving device of second through-hole and lower section.
A kind of preferred embodiment as teaching unmanned plane described in the utility model, in which: the foot prop further includes connection
Block, reinforcement block, support column and support chip；The link block is connect with the horn；The support column and the support chip with
The link block connection, and contradicted after the support chip ends bent with the end of the support column；The reinforcement block with it is described
Link block, support column, support chip three connection.
A kind of preferred embodiment as teaching unmanned plane described in the utility model, in which: the unmanned plane further includes letter
Number receiving module and power module, the signal receiving module receive the signal that controlling terminal issues and are simultaneously transmitted to the control mould
Analysis is handled in block, is finally responded by the power plant module and flare maneuver occurs；The power module provides power supply.
A kind of preferred embodiment as teaching unmanned plane described in the utility model, in which: further include being set to the religion
The airborne task device on unmanned plane is learned, the task device includes video camera, sensor etc..
Detailed description of the invention
It, below will be to required in embodiment description in order to illustrate more clearly of the technical solution of the utility model embodiment
The attached drawing used is briefly described, it should be apparent that, the accompanying drawings in the following description is only some implementations of the utility model
Example, for those of ordinary skill in the art, without any creative labor, can also be according to these attached drawings
Obtain other attached drawings.Wherein:
Fig. 1 is the overall structure diagram of teaching unmanned plane described in the first embodiment of utility model；
Fig. 2 is the overall structure diagram of rack in teaching unmanned plane described in the first embodiment of utility model；
Fig. 3 is the overall structure diagram of installation end in teaching unmanned plane described in second of embodiment of utility model；
Fig. 4 is the overall structure diagram of foot prop in teaching unmanned plane described in second of embodiment of utility model；
Fig. 5 is the local explosion structure diagram of teaching unmanned plane described in second of embodiment of utility model.
Specific embodiment
It is attached below with reference to specification to keep the above objects, features, and advantages of the utility model more obvious and easy to understand
Figure is described in detail specific embodiment of the present utility model, it is clear that described embodiment is one of the utility model
Point embodiment, rather than whole embodiments.Based on the embodiments of the present invention, ordinary people in the field is not making wound
Every other embodiment obtained under the premise of the property made labour, all should belong to the range of the protection of the utility model.
Many details are explained in the following description in order to fully understand the utility model, but this is practical new
Type can also be implemented using other than the one described here other way, and those skilled in the art can be without prejudice to this reality
With doing similar popularization in the case where novel intension, therefore the utility model is not limited by the specific embodiments disclosed below.
Secondly, " one embodiment " or " embodiment " referred to herein, which refers to, may be included at least one reality of the utility model
A particular feature, structure, or characteristic in existing mode." in one embodiment " that different places occur in the present specification is not
The same embodiment is referred both to, nor the individual or selective embodiment mutually exclusive with other embodiments.
Thirdly, the utility model combination schematic diagram is described in detail, when the utility model embodiment is described in detail, for just
In explanation, indicate that the sectional view of device architecture can disobey general proportion and make partial enlargement, and the schematic diagram is example,
The range of the utility model protection should not be limited herein.In addition, the three-dimensional of length, width and depth should be included in actual fabrication
Bulk.
Simultaneously in the description of the present invention, it should be noted that the instructions such as " upper and lower, inner and outer " in term
Orientation or positional relationship is to be based on the orientation or positional relationship shown in the drawings, and is merely for convenience of description the utility model and simplification
Description, rather than the device or element of indication or suggestion meaning must have a particular orientation, constructed and grasped with specific orientation
Make, therefore should not be understood as limiting the present invention.In addition, term " first, second or third " is used for description purposes only,
It is not understood to indicate or imply relative importance.
In the utility model unless otherwise clearly defined and limited, term " installation is connected, connection " should do broad sense reason
Solution, such as: may be a fixed connection, be detachably connected or integral type connection；It equally can be mechanical connection, electrical connection or direct
Connection, can also indirectly connected through an intermediary, the connection being also possible to inside two elements.For the common skill of this field
For art personnel, the concrete meaning of above-mentioned term in the present invention can be understood with concrete condition.
Embodiment 1
Signal referring to Fig.1~2 illustrates the overall structure diagram for unmanned plane of imparting knowledge to students described in the present embodiment, should
Unmanned plane includes rack 100, power plant module 200 and control module 300, and rack 100 is for carrying power plant module 200 and control
Module 300, power plant module 200 generates the power of unmanned plane during flying, and control module 300 then controls the speed of flight, posture etc..
Specifically, rack 100, rack 100 further includes fuselage 101 and horn 102, and one end of horn 102 is connect with fuselage 101；Power
Module 200 is set to the other end of horn 102 and can generate flying power；Between control module 300, with power plant module 200
It is communicated to connect by horn 102, controls the flight of unmanned plane.Unmanned plane is a kind of power airflight for not carrying operator
Device, wherein power plant module 200 uses air force to provide required lift for aircraft, can fly or remotely guide automatically,
Referring to fig. 1, the present embodiment uses quadrotor power mode, is to be turned by adjusting four motor speeds to change rotor
Speed, realizes the variation of lift, to control posture and the position of aircraft, and power plant module 200 further includes 201 He of driving device
Blade 202；Blade 202 is set on the output shaft of driving device 201, and driving device 201 is the electricity of quadrotor in the present embodiment
Machine, the output axis connection of blade 202 and motor, for the stability of flight, the driving device 201 is using upper and lower longitudinally asymmetric
Setting constitutes one group of rotor.Further, rack 100 further includes connecting pin 103, foot prop 104 and installation end 105；Connecting pin
103 are set to one end of horn 102, and installation corresponding with fuselage 101；Installation end 105 is set to the other end of horn 102,
And for installing power plant module 200, foot prop 104 is set to the lower section of horn 102, supports horn 102.Those skilled in the art herein
Understandable to be, referring in the prior art, the connecting pin 103 of 102 both ends of horn setting and the mode of installation end 105 can join
It is realized according to the prior art, such as integral type injection molding, welding or the mounting means for using punching bolt etc., therefore foot prop 104
Mounting means the present embodiment also similarly.Control module 300 is the core control devices of unmanned plane, is equivalent to the big of unmanned plane
Brain, if the important symbol of general aviation model is different from equipped with control system and unmanned plane；Control module 300 includes real-time
It acquires the Flight Condition Data of each sensor measurement, receive being sent by ground control station up channel for radio measurement and control terminal transmission
The control command and data come, are computed processing, export control instruction to executing agency, realize to flight moulds various in unmanned plane
The control of state and management and control to task device；Simultaneously by the status data of unmanned plane and engine, airborne power supply system,
The working status parameter of task device is real-time transmitted to airborne radio data terminal, sends back ground through radio downlink channel
Tracking telemetry and command station completes the flight control of unmanned plane.
For the ease of the understanding of those skilled in the art, it is also necessary to which explanation, motor is referring to existing skill in the present embodiment
In art, the control of control module 300 is realized by signal, is finally executed by power plant module 200 namely motor executes, by different letters
Number it is converted into the power of electric signal, certainly further includes the speed regulator with motor phase separation, again to control the revolving speed of motor
Referred to as electricity is adjusted, and effect is control motor speed.Further, the present embodiment unmanned plane further includes 400 He of signal receiving module
Power module 500, signal receiving module 400 receive the signal that controlling terminal issues and are transmitted in control module 300 at analysis
Reason is finally responded by power plant module 200 and flare maneuver occurs；Power module 500 provides power supply.But and for complete unmanned plane
For system, it should include also necessarily electrical connection, navigation positioning system, servo driving module etc., can refer to
The prior art is realized, does not enumerate explanation herein, stresses the connection between each modular structure in the present embodiment, rather than entirely control
System realization, those skilled in the art can refer to the prior art realization.
Embodiment 2
Referring to Fig. 3~5 signal, with one embodiment the difference is that: installation end 105 further include column slot 105a,
First mounting hole 105b, extending column 105c, the second mounting hole 105d, as one of the present embodiment preferred embodiment, to installation
End 105 improves.Specifically, the unmanned plane includes rack 100, power plant module 200 and control module 300, rack 100 is used
In carrying power plant module 200 and control module 300, power plant module 200 generates the power of unmanned plane during flying, and control module 300
Then control speed, the posture etc. of flight.Specifically, rack 100, rack 100 further includes fuselage 101 and horn 102, horn 102
One end connect with fuselage 101；Power plant module 200 is set to the other end of horn 102 and can generate flying power；Control
It is communicated to connect between module 300, with power plant module 200 by horn 102, controls the flight of unmanned plane.Unmanned plane is not carry
A kind of power airborne aircraft of operator, wherein power plant module 200 uses air force to provide required liter for aircraft
Power can fly automatically or remotely guide, and referring to fig. 1, it is to pass through adjusting that the present embodiment, which uses quadrotor power mode,
Four motor speeds change variable rotor speed, realize the variation of lift, to control posture and the position of aircraft, and power mould
Block 200 further includes driving device 201 and blade 202；Blade 202 is set on the output shaft of driving device 201, the present embodiment
Middle driving device 201 is the motor of quadrotor, the output axis connection of blade 202 and motor, for the stability of flight, the driving
Device 201 constitutes one group of rotor using upper and lower longitudinally asymmetric setting.Further, rack 100 further includes connecting pin 103, foot prop
104 and installation end 105；Connecting pin 103 is set to one end of horn 102, and installation corresponding with fuselage 101；Installation end 105
It is set to the other end of horn 102, and for installing power plant module 200, foot prop 104 is set to the lower section of horn 102, support
Horn 102.Those skilled in the art are understandable herein is, referring in the prior art, the connecting pin 103 of 102 both ends of horn setting
It can refer to the prior art with the mode of installation end 105 to realize, such as integral type injection molding, welding or the peace using punching bolt
Dress mode etc., thus the mounting means of foot prop 104 the present embodiment also similarly.Control module 300 is the core control of unmanned plane
Device is equivalent to the brain of unmanned plane, if the important mark of general aviation model is different from equipped with control system and unmanned plane
Will；Control module 300 includes the Flight Condition Data for acquiring each sensor measurement in real time, receives radio measurement and control terminal transmission
The control command and data sent by ground control station up channel, are computed processing, export control instruction to executing agency, in fact
The now control to model of flight various in unmanned plane and management and control to task device；Simultaneously by the status data of unmanned plane
And engine, airborne power supply system, the working status parameter of task device are real-time transmitted to airborne radio data terminal, through nothing
Line electricity down channel sends back ground control station, completes the flight control of unmanned plane.
For the ease of the understanding of those skilled in the art, it is also necessary to which explanation, motor is referring to existing skill in the present embodiment
In art, the control of control module 300 is realized by signal, is finally executed by power plant module 200 namely motor executes, by different letters
Number it is converted into the power of electric signal, certainly further includes the speed regulator with motor phase separation, again to control the revolving speed of motor
Referred to as electricity is adjusted, and effect is control motor speed.Further, the present embodiment unmanned plane further includes 400 He of signal receiving module
Power module 500, signal receiving module 400 receive the signal that controlling terminal issues and are transmitted in control module 300 at analysis
Reason is finally responded by power plant module 200 and flare maneuver occurs；Power module 500 provides power supply.But and for complete unmanned plane
For system, it should include also necessarily electrical connection, navigation positioning system, servo driving module etc., can refer to
The prior art is realized, does not enumerate explanation herein, stresses the connection between each modular structure in the present embodiment, rather than entirely control
System realization, those skilled in the art can refer to the prior art realization.
Further more specifically, the driving device 201 for being set to top is set in column slot 105a through the first installation
Hole 105b is fixed；Extending column 105c is set to the bottom of column slot 105a, and the second mounting hole 105d is arranged on extending column 105c.
Installation end 105 further includes fixed plate 105e, and fixed plate 105e further includes third mounting hole 105e-1, third through-hole
105e-2 and the 4th mounting hole 105e-3；Pass through third mounting hole 105e-1 installation corresponding with the second mounting hole 105d；Lower section
Driving device 201 installed by the 4th mounting hole 105e-3.First through hole 105f and second is also set up in column slot 105a
Through-hole 105g；The route of control module 300 is discharged into the driving device 201 in horn 102 and passing through first through hole 105f and top
Connection, and connected by the driving device 201 of the second through-hole 105g and lower section.Foot prop 104 further includes link block 104a, reinforcement block
104b, support column 104c and support chip 104d；Link block 104a is connect with horn 102；Support column 104c and support chip 104d
It connect with link block 104a, and is contradicted after support chip 104d ends bent with the end of support column 104c；Reinforcement block 104b with
Link block 104a, support column 104c, support chip 104d three connection.
Based on process above-mentioned, that the driving device 201 of upper and lower is installed are as follows: first will be by the electrical of power plant module 200
Route is discharged into horn 102, then is pierced by the driving device 201 that access is located above by first through hole 105f；Likewise, line
The second through-hole of Lu Kejing 105g, which enters in third through-hole 105e-2, to be accessed in underlying driving device 201, so realizes electricity
Gas connection.Further, 201 bottom of driving device of top be set to the first mounting hole 105b for bolt hole, the side of working as
Driving device 201 when being put into column slot 105a, the first mounting hole 105b is fixed；The driving device 201 of lower section is led to again
It crosses the 4th mounting hole 105e-3 and fixed plate 105e to be installed, after being installed, passes through third mounting hole 105e-1 and second
The installation of fixed plate 105e and 105 bottom of installation end, so completion upper and lower are realized in bolt cooperation between mounting hole 105d
Driving device 201 install.
It should be noted that above embodiments are merely intended for describing the technical solutions of the present application, but not for limiting the present application, although reference
The utility model is described in detail in preferred embodiment, those skilled in the art should understand that, it can be to this reality
It is modified or replaced equivalently with novel technical solution, without departing from the spirit and scope of the technical scheme of the present invention,
It should all cover in the scope of the claims of the utility model.
Claims (9)
1. a kind of teaching unmanned plane, it is characterised in that: including,
Rack (100), the rack (100) further include fuselage (101) and horn (102), one end of the horn (102) and institute
State fuselage (101) connection；
Power plant module (200) is set to the other end of the horn (102) and can generate flying power；
It is communicated to connect between control module (300), with the power plant module (200) by the horn (102), controls the nothing
Man-machine flight.
2. as described in claim 1 teaching unmanned plane, it is characterised in that: the rack (100) further include connecting pin (103),
Foot prop (104) and installation end (105)；
The connecting pin (103) is set to one end of the horn (102), and installation corresponding with the fuselage (101)；It is described
Installation end (105) is set to the other end of the horn (102), and for installing the power plant module (200), the foot prop
(104) it is set to the lower section of the horn (102), supports the horn (102).
3. teaching unmanned plane as claimed in claim 2, it is characterised in that: the power plant module (200) further includes driving device
(201) and blade (202)；The blade (202) is set on the output shaft of the driving device (201).
4. teaching unmanned plane as claimed in claim 3, it is characterised in that: the installation end (105) further includes column slot (105a), the
One mounting hole (105b), extending column (105c), the second mounting hole (105d)；
The driving device (201) of top is set to solid by first mounting hole (105b) in the column slot (105a)
It is fixed；The extending column (105c) is set to the bottom of the column slot (105a), and described is arranged on the extending column (105c)
Two mounting holes (105d).
5. teaching unmanned plane as claimed in claim 4, it is characterised in that: the installation end (105) further includes fixed plate (105e),
The fixed plate (105e) further includes third mounting hole (105e-1), third through-hole (105e-2) and the 4th mounting hole (105e-
3)；
Third mounting hole (105e-1) installation corresponding with the second mounting hole (105d)；The driving device of lower section
(201) it is installed by the 4th mounting hole (105e-3) with the fixed plate (105e).
6. unmanned plane of imparting knowledge to students as described in claim 4 or 5, it is characterised in that: also set up first through hole in the column slot (105a)
(105f) and the second through-hole (105g)；
The route of the control module (300) is discharged into the horn (102) and by the first through hole (105f) and top
The driving device (201) connection, and pass through the driving device (201) of second through-hole (105g) and lower section company
It connects.
7. claim 2,4 or 5 it is any as described in impart knowledge to students unmanned plane, it is characterised in that: the foot prop (104) further includes link block
(104a), reinforcement block (104b), support column (104c) and support chip (104d)；
The link block (104a) connect with the horn (102)；The support column (104c) and the support chip (104d) are equal
It connect with the link block (104a), and is supported after the support chip (104d) ends bent with the end of the support column (104c)
Touching；The reinforcement block (104b) connect with the link block (104a), support column (104c), support chip (104d) three.
8. teaching unmanned plane as claimed in claim 7, it is characterised in that: the unmanned plane further includes signal receiving module (400)
With power module (500), the signal receiving module (400) receives the signal that controlling terminal issues and is transmitted to the control mould
Analysis is handled in block (300), is finally responded by the power plant module (200) and flare maneuver occurs；The power module (500) mentions
Power supply source.
9. as claimed in claim 8 teaching unmanned plane, it is characterised in that: further include be set to it is described teaching unmanned plane on it is airborne
Task device, the task device include video camera, sensor, measuring device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821758931.8U CN209023117U (en) | 2018-10-29 | 2018-10-29 | A kind of teaching unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821758931.8U CN209023117U (en) | 2018-10-29 | 2018-10-29 | A kind of teaching unmanned plane |
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| Publication Number | Publication Date |
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| CN209023117U true CN209023117U (en) | 2019-06-25 |
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ID=66907536
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| CN201821758931.8U Active CN209023117U (en) | 2018-10-29 | 2018-10-29 | A kind of teaching unmanned plane |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110703801A (en) * | 2019-10-30 | 2020-01-17 | 上海歌尔泰克机器人有限公司 | Unmanned aerial vehicle simulation method, device and equipment and storage medium |
-
2018
- 2018-10-29 CN CN201821758931.8U patent/CN209023117U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110703801A (en) * | 2019-10-30 | 2020-01-17 | 上海歌尔泰克机器人有限公司 | Unmanned aerial vehicle simulation method, device and equipment and storage medium |
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