CN202836835U - Unmanned aerial vehicle lift force and torsion force test device - Google Patents
Unmanned aerial vehicle lift force and torsion force test device Download PDFInfo
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- CN202836835U CN202836835U CN 201220505244 CN201220505244U CN202836835U CN 202836835 U CN202836835 U CN 202836835U CN 201220505244 CN201220505244 CN 201220505244 CN 201220505244 U CN201220505244 U CN 201220505244U CN 202836835 U CN202836835 U CN 202836835U
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Abstract
The utility model discloses an unmanned aerial vehicle lift force and torsion force test device. The unmanned aerial vehicle lift force and torsion force test device comprises a testing frame, a sensor system installed at a top end of the testing frame, a tested motor blade assembly installed on the sensor system, and a control device connected to the sensor system. The unmanned aerial vehicle lift force and torsion force test device is used for the testing on the lift force and the torsion force of rotor wings of an unmanned aerial vehicle, and provides key test parameters for the product quality judgment and the development process of the unmanned aerial vehicle. The unmanned aerial vehicle lift force and torsion force test device tests the pull force and the torsion force generated by motor blades under the work condition, and provides the basis for the product quality judgment and product design.
Description
Technical field
The utility model relates to the unmanned vehicle field, relates in particular to a kind of unmanned vehicle lift, torque test device.
Background technology
Unmanned vehicle is the not manned vehicle that utilizes radio robot and the presetting apparatus of providing for oneself to handle.Without driving cabin, but the equipment such as robot pilot, presetting apparatus are installed on the machine.On ground, the naval vessels or machine tool remote-controlled station personnel by equipment such as radars, to its follow the tracks of, location, remote control, remote measurement and digital transmission.Rotor craft is that nobody is important a kind of in-flight, rotor unmanned aircraft is divided into again the types such as single rotor, the bispin wing, many rotors, rotor unmanned aircraft, multi-rotor aerocraft particularly, since its landing flexibly, easily control, the characteristics such as good stability, be widely used in the purposes such as aerial reconnaissance, supervision, trunking traffic, rescue, small size mapping.
The rotor torsion of rotor craft and value of thrust are core design foundation and the product quality bases for estimation of the type aircraft, at present also unripe especially at product for the testing apparatus of rotor torsion and pulling force, in quality of production judgement and research and development engineering, provide foundation, existing proving installation complex structure, complex operation, and cost is higher.
The utility model content
The purpose of this utility model is to provide a kind of unmanned vehicle lift, torque test device, and pulling force and the torsion that can carry out producing under the duty to the motor paddle components be better measured, and provides foundation for judging product quality, product design.
According to an aspect of the present utility model, the utility model provides a kind of unmanned vehicle lift, torque test device, comprising:
Testing jig;
Be installed in the sensing system on testing jig top;
Be installed on the sensing system by the measured motor paddle components; And
The control device that connects described sensing system.
Preferably, described sensing system comprises:
For detection of by the pulling force sensor of measured motor paddle components lift; And
For detection of by the torsion torque sensor of measured motor paddle components torsion.
Preferably, described torsion torque sensor is positioned at the top of described pulling force sensor.
Preferably, describedly be connected by measured motor paddle components and torsion torque sensor upper end.
Preferably, described pulling force sensor is connected with the torsion torque sensor lower end.
Preferably, described pulling force sensor lower end connects described testing jig top.
Preferably, three-legged support is equipped with in described testing jig bottom.
Preferably, described is the motor that blade is housed by the measured motor paddle components.
Preferably, described control device comprises:
Control is by the motor speed of measured motor paddle components and process lift that pulling force sensor and torsion torque sensor detect and the control panel of torsion signal; And
Connect the PC that described control panel is used for sending to control panel motor speed steering order and reception and processing lift and torsion signal.
Preferably, comprise that also connecting described control panel is used for the direct supply that provided electric energy by the measured motor paddle components for described.
Compared with prior art, the beneficial effects of the utility model are: this device is used for the test of unmanned vehicle rotor lift and torsion, for providing important test parameter in the judgement of unmanned vehicle production quality and the R﹠D process.By this device pulling force and torsion that the motor blade carries out producing under the duty are tested, provided foundation for judging product quality and product design.
Description of drawings
Fig. 1 is the unmanned vehicle lift that provides of the utility model embodiment, the functional block diagram of torque test device;
Fig. 2 is the unmanned vehicle lift that provides of the utility model embodiment, the structural drawing of torque test device.
Embodiment
Below in conjunction with accompanying drawing preferred embodiment of the present utility model is elaborated, should be appreciated that following illustrated preferred embodiment only is used for description and interpretation the utility model, and be not used in restriction the utility model.
Fig. 1 has shown the unmanned vehicle lift that the utility model embodiment provides, the functional block diagram of torque test device, as shown in Figure 1, comprising: testing jig 101; Be installed in the sensing system 102 on testing jig 101 tops; Be installed on the sensing system 102 by measured motor paddle components 103; And the control device 104 that connects described sensing system.
Furtherly, described device comprises that also connecting described control panel is used for the direct supply 105 that provided electric energy by measured motor paddle components 103 for described.
Fig. 2 has shown the unmanned vehicle lift that the utility model embodiment provides, the structural drawing of torque test device, as shown in Figure 2.
Described sensing system 102 comprises: for detection of by the pulling force sensor 1022 of measured motor paddle components 103 lift; And for detection of by the torsion torque sensor 1021 of measured motor paddle components 103 torsion.
Specifically, described sensing system 102 is installed to the device top, adopt the outsourcing sensor assembly, can obtain respectively pulling force and two parameters of torsion when motor 1032 energisings drive by pulling force sensor 1022 and torsion torque sensor 1021 when blade 1031 rotates.
Furtherly, described torsion torque sensor 1021 is positioned at the top of described pulling force sensor 1022, describedly be connected with torsion torque sensor 1021 upper ends by measured motor paddle components 103, described pulling force sensor 1022 is connected with torsion torque sensor 1021 lower ends, and described pulling force sensor 1022 lower ends connect described testing jig 101 tops.
Described control device 104 comprises: control is by motor 1032 rotating speeds of measured motor paddle components 103 and process pulling force sensor 1022 and lift that torsion torque sensor 1021 is detected and the control panel 1041 of torsion signal; And connect described control panel 1041 for the PC 1042 that sends motors 1032 rotating speed steering orders and reception and processing lift and torsion signal to control panel 1041.
Described control panel 1041 is used for the electric current of control inputs motor 1032, by adjusting the electric current of input motor 1032, reaches the purpose of control blade 1031 rotating speeds.
Described .PC machine 1042 is for software provides operation platform, and software carries out the setting of every test parameter and the demonstration of test result.
Three-legged support 1011 is equipped with in described testing jig 101 bottoms; Described is motors 1032 that blade 1031 is housed by measured motor paddle components 103.
Specifically, described testing jig 101 has three supports, can be according to the position adjustments testing jig 101 of three supports perpendicular to ground, and testing jig 101 tops are according to motor-paddle components, apart from floor level 2m, blade 1031 rotations cause unexpected injury to the people in the time of can preventing from testing.
Principle of work of the present utility model: by software by electric current or rotating speed are arranged, thereby detect lift and the torsion that motor turns round and produces under different rotating speeds, electric current, and the result is directly shown at software, and generates the PNG file and preserve.
In sum, the beneficial effects of the utility model are to test by the pulling force and the torsion that the motor blade are carried out produce under the duty, provide foundation for judging product quality and product design.
Although above the utility model is had been described in detail, the utility model is not limited to this, and those skilled in the art of the present technique can carry out various modifications according to principle of the present utility model.Therefore, all modifications of doing according to the utility model principle all should be understood to fall into protection domain of the present utility model.
Claims (10)
1. a unmanned vehicle lift, torque test device is characterized in that, comprising:
Testing jig;
Be installed in the sensing system on testing jig top;
Be installed on the sensing system by the measured motor paddle components; And
The control device that connects described sensing system.
2. device according to claim 1 is characterized in that, described sensing system comprises:
For detection of by the pulling force sensor of measured motor paddle components lift; And
For detection of by the torsion torque sensor of measured motor paddle components torsion.
3. device according to claim 2 is characterized in that, described torsion torque sensor is positioned at the top of described pulling force sensor.
4. device according to claim 3 is characterized in that, describedly is connected by measured motor paddle components and torsion torque sensor upper end.
5. device according to claim 3 is characterized in that, described pulling force sensor is connected with the torsion torque sensor lower end.
6. device according to claim 5 is characterized in that, described pulling force sensor lower end connects described testing jig top.
7. each described device is characterized in that according to claim 1-6, and three-legged support is equipped with in described testing jig bottom.
8. device according to claim 2 is characterized in that, described is the motor that blade is housed by the measured motor paddle components.
9. device according to claim 8 is characterized in that, described control device comprises:
Control is by the motor speed of measured motor paddle components and process lift that pulling force sensor and torsion torque sensor detect and the control panel of torsion signal; And
Connect the PC that described control panel is used for sending to control panel motor speed steering order and reception and processing lift and torsion signal.
10. device according to claim 9 is characterized in that, comprises that also connecting described control panel is used for the direct supply that provided electric energy by the measured motor paddle components for described.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220505244 CN202836835U (en) | 2012-09-28 | 2012-09-28 | Unmanned aerial vehicle lift force and torsion force test device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220505244 CN202836835U (en) | 2012-09-28 | 2012-09-28 | Unmanned aerial vehicle lift force and torsion force test device |
Publications (1)
| Publication Number | Publication Date |
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| CN202836835U true CN202836835U (en) | 2013-03-27 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN 201220505244 Expired - Lifetime CN202836835U (en) | 2012-09-28 | 2012-09-28 | Unmanned aerial vehicle lift force and torsion force test device |
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| CN103983403A (en) * | 2014-01-21 | 2014-08-13 | 浙江大学 | Apparatus and method for measuring operating performance and parameters of motor propeller system |
| CN105044599A (en) * | 2015-07-24 | 2015-11-11 | 华南农业大学 | Unmanned aerial vehicle motor-propeller efficiency test device and method |
| CN105547554A (en) * | 2015-12-23 | 2016-05-04 | 北京航天控制仪器研究所 | Apparatus used for measuring small spiral wing lift force and torque and method thereof |
| CN106092196A (en) * | 2016-06-22 | 2016-11-09 | 中国科学院光电研究院 | A kind of aerostatics mass property measurement method of parameters |
| CN106347705A (en) * | 2016-10-31 | 2017-01-25 | 安徽理工大学 | Rotor lift force testing system for unmanned aerial vehicle |
| CN106516160A (en) * | 2016-12-12 | 2017-03-22 | 哈尔滨理工大学 | Remote control testing device for rotor lift force parameters |
| CN106595933A (en) * | 2017-02-07 | 2017-04-26 | 常州市易电电气有限公司 | Test apparatus used for unmanned aerial vehicle motor dynamic tension and torsion |
| CN106768565A (en) * | 2017-03-09 | 2017-05-31 | 北京尖翼科技有限公司 | A kind of test device of small-sized unmanned aircraft motor |
| CN107024310A (en) * | 2017-06-01 | 2017-08-08 | 上海未来伙伴机器人有限公司 | A kind of Power System of Flight Vehicle test device |
| CN107192532A (en) * | 2017-06-09 | 2017-09-22 | 昆明理工大学 | A kind of measurement apparatus and measuring method of four-axle aircraft brushless electric machine thrust coefficient |
| CN107356433A (en) * | 2017-06-09 | 2017-11-17 | 昆明理工大学 | A kind of measurement apparatus and measuring method of four-axle aircraft brushless electric machine torque coefficient |
| CN113804473A (en) * | 2021-10-09 | 2021-12-17 | 北京理工大学 | Device and method for measuring aerodynamic performance of rotor type wall climbing robot |
| CN117689276A (en) * | 2024-02-04 | 2024-03-12 | 济宁久邦工程机械设备有限公司 | Machine vision-based production quality analysis method for folding arm of overhead working truck |
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2012
- 2012-09-28 CN CN 201220505244 patent/CN202836835U/en not_active Expired - Lifetime
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN103983403A (en) * | 2014-01-21 | 2014-08-13 | 浙江大学 | Apparatus and method for measuring operating performance and parameters of motor propeller system |
| CN103983403B (en) * | 2014-01-21 | 2016-05-11 | 浙江大学 | Measure the apparatus and method of motor propeller system service behaviour and parameter |
| CN105044599A (en) * | 2015-07-24 | 2015-11-11 | 华南农业大学 | Unmanned aerial vehicle motor-propeller efficiency test device and method |
| CN105044599B (en) * | 2015-07-24 | 2018-03-20 | 华南农业大学 | A kind of efficiency test device and method suitable for unmanned plane motor oar |
| CN105547554A (en) * | 2015-12-23 | 2016-05-04 | 北京航天控制仪器研究所 | Apparatus used for measuring small spiral wing lift force and torque and method thereof |
| CN105547554B (en) * | 2015-12-23 | 2018-05-22 | 北京航天控制仪器研究所 | A kind of device and method for being used to measure compact spiral wing lift and torque |
| CN106092196A (en) * | 2016-06-22 | 2016-11-09 | 中国科学院光电研究院 | A kind of aerostatics mass property measurement method of parameters |
| CN106347705A (en) * | 2016-10-31 | 2017-01-25 | 安徽理工大学 | Rotor lift force testing system for unmanned aerial vehicle |
| CN106516160A (en) * | 2016-12-12 | 2017-03-22 | 哈尔滨理工大学 | Remote control testing device for rotor lift force parameters |
| CN106516160B (en) * | 2016-12-12 | 2018-11-23 | 哈尔滨理工大学 | A kind of remote-controlled test device of rotor lift parameter |
| CN106595933A (en) * | 2017-02-07 | 2017-04-26 | 常州市易电电气有限公司 | Test apparatus used for unmanned aerial vehicle motor dynamic tension and torsion |
| CN106768565A (en) * | 2017-03-09 | 2017-05-31 | 北京尖翼科技有限公司 | A kind of test device of small-sized unmanned aircraft motor |
| CN106768565B (en) * | 2017-03-09 | 2022-08-23 | 北京尖翼科技有限公司 | Testing arrangement of small-size unmanned vehicles motor |
| CN107024310A (en) * | 2017-06-01 | 2017-08-08 | 上海未来伙伴机器人有限公司 | A kind of Power System of Flight Vehicle test device |
| CN107192532A (en) * | 2017-06-09 | 2017-09-22 | 昆明理工大学 | A kind of measurement apparatus and measuring method of four-axle aircraft brushless electric machine thrust coefficient |
| CN107356433B (en) * | 2017-06-09 | 2019-05-10 | 昆明理工大学 | A kind of measuring device and measuring method of four-axle aircraft brushless motor torque coefficient |
| CN107192532B (en) * | 2017-06-09 | 2019-05-14 | 昆明理工大学 | A kind of measuring device and measuring method of four-axle aircraft brushless motor thrust coefficient |
| CN107356433A (en) * | 2017-06-09 | 2017-11-17 | 昆明理工大学 | A kind of measurement apparatus and measuring method of four-axle aircraft brushless electric machine torque coefficient |
| CN113804473A (en) * | 2021-10-09 | 2021-12-17 | 北京理工大学 | Device and method for measuring aerodynamic performance of rotor type wall climbing robot |
| CN113804473B (en) * | 2021-10-09 | 2022-07-05 | 北京理工大学 | Device and method for measuring aerodynamic performance of rotor wing type wall climbing robot |
| CN117689276A (en) * | 2024-02-04 | 2024-03-12 | 济宁久邦工程机械设备有限公司 | Machine vision-based production quality analysis method for folding arm of overhead working truck |
| CN117689276B (en) * | 2024-02-04 | 2024-04-19 | 济宁久邦工程机械设备有限公司 | Machine vision-based production quality analysis method for folding arm of overhead working truck |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C56 | Change in the name or address of the patentee | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 528305, No. 7, Jianye Middle Road, Shunde hi tech Zone (Ronggui), Guangdong, Foshan Patentee after: FOSHAN AIRCAM UAV TECHNOLOGY Corp. Address before: 528305, No. 7, Jianye Middle Road, Shunde hi tech Zone (Ronggui), Guangdong, Foshan Patentee before: FOSHAN AIRCAM UAV TECHNOLOGY Co.,Ltd. |
|
| CP01 | Change in the name or title of a patent holder |
Address after: 528305 No. 7 Jianye Middle Road, Shunde High-tech Zone, Foshan City, Guangdong Province Patentee after: Magnesium Kezhongsi Technology (Foshan) Co.,Ltd. Address before: 528305 No. 7 Jianye Middle Road, Shunde High-tech Zone, Foshan City, Guangdong Province Patentee before: Foshan Anlcom Technology Co.,Ltd. Address after: 528305 No. 7 Jianye Middle Road, Shunde High-tech Zone, Foshan City, Guangdong Province Patentee after: Foshan Anlcom Technology Co.,Ltd. Address before: 528305 No. 7 Jianye Middle Road, Shunde High-tech Zone, Foshan City, Guangdong Province Patentee before: FOSHAN AIRCAM UAV TECHNOLOGY Corp. |
|
| CP01 | Change in the name or title of a patent holder | ||
| CX01 | Expiry of patent term |
Granted publication date: 20130327 |
|
| CX01 | Expiry of patent term |