CN205670022U - A kind of unmanned plane dynamical system test platform - Google Patents
A kind of unmanned plane dynamical system test platform Download PDFInfo
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- CN205670022U CN205670022U CN201620555138.2U CN201620555138U CN205670022U CN 205670022 U CN205670022 U CN 205670022U CN 201620555138 U CN201620555138 U CN 201620555138U CN 205670022 U CN205670022 U CN 205670022U
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Abstract
The utility model discloses a kind of unmanned plane dynamical system test platform, relate to unmanned plane field, including test platform, electricity tune it is equipped with on four limits of test platform, the other end that electricity is adjusted is provided with test device, test device includes testboard and test sensor, testboard is provided with motor, electric machine main shaft is provided with propeller, the lower section of test platform is provided with motor, motor is provided with center rod, the top of center rod is provided with slave computer, center rod is provided with the first bull stick in the lower section of slave computer, the centre of center rod is provided with the second bull stick, the end of the first bull stick is provided with thermal imaging system and visible light lens, the end of the second bull stick is provided with survey wind-force module.Loop electrode, electricity can be transferred in row test by this test platform simultaneously.This platform can gather the pulling force of motor, rotating speed, electricity tune electric current, battery life, discharging efficiency；Propeller wind cutting power, the running temperature of each parts；And the operating Vibration Condition of system, overall power.
Description
Technical field
This utility model relates to unmanned plane field, is specifically related to a kind of unmanned plane dynamical system test platform.
Background technology
Current dynamical system testboard is used mostly all kinds of instrument and meters of separation to measure collection data, does not has entirety
Scheme and case study on implementation.During use the most inconvenient, do not have remote collection to control function, measurement data is inaccurate comprehensive, difficult
Think that test job brings substantial data refer.
Native system is unmanned plane dynamical system (battery-electricity tune-motor-propeller) test platform, at burn-in test, assembly
Performance test, etc. aspect have and extensively apply flexibly and effectively, Default Value and debugger routine for unmanned plane provide science complete
The data support in face.
Utility model content
For the deficiencies in the prior art, the purpose of this utility model is to provide a kind of unmanned plane dynamical system test flat
Platform.
This utility model solves the technical problem that and can realize by the following technical solutions: a kind of unmanned plane dynamical system
Test platform, including test platform, four limits of wherein said test platform is equipped with electricity phase modulation even, and the other end that electricity is adjusted is provided with
Connecting rod is connected, and the end of connecting rod is provided with location bar, and the top of location bar is provided with test device, and test device includes testboard and survey
Test sensor in test stand, wherein testboard is provided with motor, and electric machine main shaft is provided with the propeller of connection, tests sensor
Being connected with test platform, the centre of test platform is provided with through hole, through hole be arranged right below motor, motor is provided with
Vertical center rod is connected, and center rod passes through hole, and the top of center rod is provided with slave computer, and slave computer includes wireless data sending mould
Block, remote sensing module, image transmission module, center rod is provided with the first bull stick of level, the centre of center rod in the lower section of slave computer
The second bull stick being provided with level is connected, and the end of the first bull stick is provided with thermal imaging system and visible light lens, and the end of the second bull stick sets
There is survey wind-force module.
Preferably, described motor is provided with protective cover, is provided with arrangements for speed regulation, arrangements for speed regulation and computer in protective cover
It is connected.
Preferably, described test platform is additionally provided with current detection circuit, voltage detecting circuit, decompression voltage regulator, control
Signaling interface processed and collection signaling interface, system power supply input interface.
Preferably, described test sensor includes that Hall element, Temperature Humidity Sensor, pressure transducer pass with gyroscope
Sensor, Hall element and Temperature Humidity Sensor are positioned on testboard, and pressure transducer and gyro sensor are positioned at testboard
Under.
Preferably, described slave computer matches with host computer, and host computer includes the figure matched with described image transmission module
The wireless receiving module matched with described wireless data transmission module as receiver module, image receiver module is connected with video frequency collection card,
Wireless receiving module is connected with serial ports modular converter, and video frequency collection card is connected on computers with serial ports modular converter.
Preferably, described electricity is adjusted upper for three-phase output.
Provide the benefit that: loop electrode, electricity can be transferred in row test by this test platform simultaneously.This platform can gather electricity
The pulling force of machine, rotating speed, electricity adjust electric current, battery life, discharging efficiency；Propeller wind cutting power；And system is operating shakes
Emotionally condition, overall power, the running temperature of each parts.Real time data is measured, feedback, record, and data are automatically integrated or analyze.Far
Process control motor speed, has protective cover, it is ensured that operator safety.Simple in construction, circuit understands, easy to operate.
Accompanying drawing explanation
Fig. 1 is the structural representation of this utility model a kind of unmanned plane dynamical system test platform；
Fig. 2 is the top view of the test platform of this utility model a kind of unmanned plane dynamical system test platform；
Fig. 3 is the structural representation of the test device of this utility model a kind of unmanned plane dynamical system test platform；
Fig. 4 is the circuit block diagram of this utility model a kind of unmanned plane dynamical system test platform；
Wherein 1, test platform；2, through hole；3, motor；4, protective cover；5, center rod；6, the first bull stick；7, second
Bull stick；8, slave computer；9, thermal imaging system；10, it is seen that light camera lens；11, survey wind-force module；12, connecting rod；13, position bar；14, test
Device；15, testboard；16, electricity is adjusted；17, motor；18, propeller；19, Hall element；20, pressure transducer；21, gyro
Instrument sensor；22, current detection circuit；23, voltage detecting circuit；24, decompression voltage regulator；25, control signal interface and adopting
Collection signaling interface；26, system power supply input interface.
Detailed description of the invention
Describe preferred implementation of the present utility model below in conjunction with the accompanying drawings in detail.
Fig. 1, Fig. 2, Fig. 3 and Fig. 4 show the specific embodiment party of this utility model a kind of unmanned plane dynamical system test platform
Formula: a kind of unmanned plane dynamical system test platform, including test platform 1, four limits of wherein said test platform 1 is equipped with electricity
Adjusting 16 to be connected, it is connected that electricity adjusts the other end of 16 to be provided with connecting rod 12, and the end of connecting rod 12 is provided with location bar 13, the top of location bar 13
Being provided with test device 14, test device 14 includes testboard 15 and the test sensor on testboard 15, wherein on testboard 15
Being provided with motor 17, motor 17 main shaft is provided with the propeller 18 of connection, and test sensor is connected with test platform 1, test platform 1
Centre be provided with through hole 2, through hole 2 be arranged right below motor 3, motor 3 is provided with vertical center rod 5 and is connected,
Center rod 5 is through through hole 2, and the top of center rod 5 is provided with slave computer 8, and slave computer 8 includes wireless data transmission module, remote sensing module, figure
As transport module, center rod 5 is provided with the first bull stick 6 of level in the lower section of slave computer 8, and the centre of center rod 5 is provided with level
Second bull stick 7 is connected, and the end of the first bull stick 6 is provided with thermal imaging system 9 and visible light lens 10, and the end of the second bull stick 7 is provided with survey
Wind-force module 11.
It should be noted that described motor 3 is provided with protective cover 4, be provided with arrangements for speed regulation in protective cover 4, speed governing fills
Put and be connected with computer.Current detection circuit 22, voltage detecting circuit 23, lowering and stabilizing blood pressure electricity it is additionally provided with on described test platform 1
Road 24, control signal interface and collection signaling interface 25, system power supply input interface 26.Described test sensor includes that Hall passes
Sensor 19, Temperature Humidity Sensor, pressure transducer 20 and gyro sensor 21, Hall element 19 and Temperature Humidity Sensor position
On testboard 15, pressure transducer 20 and gyro sensor 21 are positioned at testboard 15 times.Described slave computer 8 and host computer phase
Coordinating, host computer includes what the image receiver module matched with described image transmission module and described wireless data transmission module matched
Wireless receiving module, image receiver module is connected with video frequency collection card, and wireless receiving module is connected with serial ports modular converter, video
Capture card is connected on computers with serial ports modular converter.Described electricity is adjusted and is exported for three-phase on 16.
This test platform 1 uses single shaft plane to control thermal infrared imager 9, it is seen that light camera lens 10 pitch orientation rotates so that it is
The temperature conditions of the energy each parts of recording.Use Hall element 19 measure motor 17 rotating speed, lever away from measure motor 17 pulling force,
Temperature Humidity Sensor knows ambient temperature and humidity, and the wind-force size below propeller 18 blade measured by anemobiagraph, and gyroscope measurement is shaken
Emotionally condition.This test platform 1 can use computer remote monitoring motor 17, electricity to adjust the operating temperature (thermal map storage) of 16, host computer
Software design patterns platform parameters, and record each sensor and go back on one's word data, to mate " throttle stroke ".During the electric discharge of recordable lower battery
Between, and can all kinds of measurement data of superposition on a timeline.Abnormal alarm and report, when motor 17 electricity adjusts 16 temperature to exceed agreed
During safety value, report to the police；When the anti-electrical anomaly of battery, when electricity reaches protection value, it is automatically stopped motor 17 and tests.Can simultaneously test loop
Motor 17 electricity adjusts 16, and the unloaded flight that simulation " returns axle aircraft ", the motor 3 that thermal imaging system 9 and camera lens are installed by central authorities is controlled
System rotates, it is achieved 360 ° of annulars rotate.
During test, motor 3 drives center rod 5 to rotate so that the first bull stick 6 rotates, in real time with the second bull stick 7 simultaneously
Detecting the humiture situation on four test devices 14, the parameter of test can be transferred to bottom by each test sensor simultaneously
On machine 8, slave computer 8 is transferred on host computer so that observer can observe electricity tune 16, motor 17, propeller on computers
The test case of 18.
Based on above-mentioned, loop electrode, electricity can be adjusted 16 to test by this test platform 1 simultaneously.This platform can gather
The pulling force of motor 17, rotating speed, electricity adjust 16 electric currents, battery life, discharging efficiency；Propeller 18 wind cutting power, the fortune of each parts
Trip temperature；And the operating Vibration Condition of system, overall power.Real time data is measured, feedback, record, and data are integrated automatically
Or analyze.Remotely control motor 17 rotating speed, there is protective cover 4, it is ensured that operator safety.Simple in construction, circuit understands, operation
Convenient.
The foregoing is only embodiment of the present utility model, not thereby limit the scope of the claims of the present utility model, every
Utilize equivalent structure or equivalence flow process conversion that this utility model description and accompanying drawing content made, or be directly or indirectly used in
Other relevant technical fields, are the most in like manner included in scope of patent protection of the present utility model.
Claims (6)
1. a unmanned plane dynamical system test platform, including test platform, it is characterised in that: on four limits of described test platform
Being equipped with electricity phase modulation even, the other end that electricity is adjusted is provided with connecting rod and is connected, and the end of connecting rod is provided with location bar, and the top of location bar is provided with
Test device, test device includes testboard and the test sensor on testboard, and wherein testboard is provided with motor, motor master
Axle is provided with the propeller of connection, and test sensor is connected with test platform, and the centre of test platform is provided with through hole, and through hole is just
Lower section is provided with motor, and motor is provided with vertical center rod and is connected, and center rod passes through hole, and the top of center rod sets
Having slave computer, slave computer to include wireless data transmission module, remote sensing module, image transmission module, center rod sets in the lower section of slave computer
Having the first bull stick of level, the centre of center rod is provided with the second bull stick of level and is connected, and the end of the first bull stick is provided with thermal imaging system
With visible light lens, the end of the second bull stick is provided with survey wind-force module.
A kind of unmanned plane dynamical system test platform, it is characterised in that: set on described motor
Protected cover, is provided with arrangements for speed regulation in protective cover, arrangements for speed regulation are connected with computer.
A kind of unmanned plane dynamical system test platform, it is characterised in that: on described test platform also
It is provided with current detection circuit, voltage detecting circuit, decompression voltage regulator, control signal interface and gathers signaling interface, system confession
Electricity input interface.
A kind of unmanned plane dynamical system test platform, it is characterised in that: described test sensor bag
Include Hall element, Temperature Humidity Sensor, pressure transducer and gyro sensor, Hall element and Temperature Humidity Sensor position
On testboard, pressure transducer and gyro sensor are positioned under testboard.
A kind of unmanned plane dynamical system test platform, it is characterised in that: described slave computer is with upper
Machine matches, and host computer includes the image receiver module that matches with described image transmission module and described wireless data transmission module phase
The wireless receiving module joined, image receiver module is connected with video frequency collection card, and wireless receiving module is connected with serial ports modular converter,
Video frequency collection card is connected on computers with serial ports modular converter.
A kind of unmanned plane dynamical system test platform, it is characterised in that: described electricity is adjusted upper for three-phase
Output.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201620555138.2U CN205670022U (en) | 2016-06-08 | 2016-06-08 | A kind of unmanned plane dynamical system test platform |
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| CN201620555138.2U CN205670022U (en) | 2016-06-08 | 2016-06-08 | A kind of unmanned plane dynamical system test platform |
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| CN205670022U true CN205670022U (en) | 2016-11-02 |
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Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106644487A (en) * | 2016-12-26 | 2017-05-10 | 广东容祺智能科技有限公司 | Power testing system of brushless motor for unmanned aerial vehicle |
| CN106679930A (en) * | 2016-12-06 | 2017-05-17 | 中国航空工业集团公司成都飞机设计研究所 | Vehicle-mounted aerodynamic force and power test-measurement method and device of small unmanned aerial vehicle (UAV) |
| CN106872085A (en) * | 2017-03-08 | 2017-06-20 | 武汉飞流智能技术有限公司 | A kind of unmanned plane horn kinetic energy efficiency automatic test device |
| CN107765182A (en) * | 2017-12-07 | 2018-03-06 | 智灵飞（北京）科技有限公司 | A kind of ground unmanned plane motor electricity commissioning test system and method based on LABVIEW |
| CN107942999A (en) * | 2017-11-24 | 2018-04-20 | 安徽维新能源技术有限公司 | A kind of three-in-one dynamical system intelligence test platform |
| CN110641731A (en) * | 2019-09-29 | 2020-01-03 | 江苏科技大学 | Rotor motor lift force measuring device for multi-rotor unmanned aerial vehicle |
| CN113252996A (en) * | 2021-05-13 | 2021-08-13 | 新疆师范大学 | Unmanned aerial vehicle electromagnetic field testboard |
-
2016
- 2016-06-08 CN CN201620555138.2U patent/CN205670022U/en active Active
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106679930A (en) * | 2016-12-06 | 2017-05-17 | 中国航空工业集团公司成都飞机设计研究所 | Vehicle-mounted aerodynamic force and power test-measurement method and device of small unmanned aerial vehicle (UAV) |
| CN106644487A (en) * | 2016-12-26 | 2017-05-10 | 广东容祺智能科技有限公司 | Power testing system of brushless motor for unmanned aerial vehicle |
| CN106644487B (en) * | 2016-12-26 | 2019-04-02 | 广东容祺智能科技有限公司 | A kind of dynamic test system of unmanned plane brushless motor |
| CN106872085A (en) * | 2017-03-08 | 2017-06-20 | 武汉飞流智能技术有限公司 | A kind of unmanned plane horn kinetic energy efficiency automatic test device |
| CN106872085B (en) * | 2017-03-08 | 2020-09-04 | 武汉飞流智能技术有限公司 | Automatic testing arrangement of unmanned aerial vehicle horn kinetic energy efficiency |
| CN107942999A (en) * | 2017-11-24 | 2018-04-20 | 安徽维新能源技术有限公司 | A kind of three-in-one dynamical system intelligence test platform |
| CN107942999B (en) * | 2017-11-24 | 2020-06-23 | 安徽一维新能源技术有限公司 | Trinity driving system intelligent test platform |
| CN107765182A (en) * | 2017-12-07 | 2018-03-06 | 智灵飞（北京）科技有限公司 | A kind of ground unmanned plane motor electricity commissioning test system and method based on LABVIEW |
| CN110641731A (en) * | 2019-09-29 | 2020-01-03 | 江苏科技大学 | Rotor motor lift force measuring device for multi-rotor unmanned aerial vehicle |
| CN110641731B (en) * | 2019-09-29 | 2022-11-15 | 江苏科技大学 | Rotor motor lift force measuring device for multi-rotor unmanned aerial vehicle |
| CN113252996A (en) * | 2021-05-13 | 2021-08-13 | 新疆师范大学 | Unmanned aerial vehicle electromagnetic field testboard |
| CN113252996B (en) * | 2021-05-13 | 2023-09-05 | 新疆师范大学 | Unmanned aerial vehicle electromagnetic field testboard |
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