CN203186583U - Overall unit aging testing device for quad-rotor unmanned aerial vehicle - Google Patents
Overall unit aging testing device for quad-rotor unmanned aerial vehicle Download PDFInfo
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- CN203186583U CN203186583U CN2013200956088U CN201320095608U CN203186583U CN 203186583 U CN203186583 U CN 203186583U CN 2013200956088 U CN2013200956088 U CN 2013200956088U CN 201320095608 U CN201320095608 U CN 201320095608U CN 203186583 U CN203186583 U CN 203186583U
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Abstract
The utility model discloses an overall unit aging testing device for a quad-rotor unmanned aerial vehicle and relates to the field of unmanned aerial vehicles. The overall unit aging testing device for the quad-rotor unmanned aerial vehicle comprises a testing platform, the overall unit of an unmanned aerial vehicle to be tested, a fixing mechanism, a direct current power supply and a control device, wherein the fixing mechanism is installed on the testing platform and used for fixing the overall unit of the unmanned aerial vehicle to be tested; the direct current power supply is connected with the overall unit of the unmanned aerial vehicle to be tested; the control device is connected with the overall unit of the unmanned aerial vehicle to be tested and used for controlling an aging test. According to the overall unit aging testing device for the quad-rotor unmanned aerial vehicle, the overall unit of the unmanned aerial vehicle is fixed on the testing platform through the fixing structure, so that the aging test is easy and convenient to carry out, and the time for the aging test on the overall unit of the unmanned aerial vehicle is saved.
Description
Technical field
The utility model relates to the unmanned vehicle technical field, particularly a kind of four rotor unmanned vehicle complete machine ageing testers.
Background technology
The unmanned vehicle technology reaches its maturity in recent years, unmanned vehicle is widely used in dual-use field, at civil area, small-sized unmanned vehicle is attempted in the application that industries such as fire-fighting, security monitoring, mapping, movies-making have begun a large amount of unmanned vehicles especially.
In fields such as some fire-fightings, emergency event processing, for the performance testing of unmanned vehicle and complete machine aging require high.The utility model provides a kind of ageing tester of four rotor unmanned vehicles.
The utility model content
The purpose of this utility model is to provide a kind of four rotor unmanned vehicle complete machine ageing testers, can save the time of aircraft complete machine burn-in test better, has improved the efficient of burn-in test.
According to an aspect of the present utility model, a kind of four rotor unmanned vehicle complete machine ageing testers are provided, comprising:
Test desk;
Tested unmanned vehicle complete machine;
Be installed in the fixed mechanism that is used for fixing tested unmanned vehicle complete machine on the test desk;
The direct supply that connects described tested unmanned vehicle complete machine; And
The control setup that is used for carrying out burn-in test control that connects described tested unmanned vehicle complete machine.
Preferably, described fixed mechanism comprises four jig arm, is used for fixing respectively four arms of described tested unmanned vehicle complete machine.
Preferably, described fixed mechanism also comprises four rotating shafts that are separately positioned on described four jig arm lower ends, and described rotating shaft is oval.
Preferably, an end of described four rotating shafts is provided with shaft gear by connecting rod respectively.
Preferably, described fixed mechanism also comprises bevel gear, is meshed with described shaft gear respectively.
Preferably, described fixed mechanism also comprises rocking arm, is connected with the other end of one of them rotating shaft.
Preferably, be separately installed with cam and spring between described rotating shaft and the jig arm, be used for controlling unclamping and clamping of jig arm.
Preferably, described control setup comprises remote controller, is used for controlling the burn-in test of described unmanned vehicle complete machine, the data of the burn-in test of demonstration and record.
Compared with prior art, the beneficial effects of the utility model are:
The utility model is fixed on the unmanned vehicle complete machine on the test desk by fixed mechanism indoor, need not in the ground non-stop flight of outdoor several, saved the time of unmanned vehicle complete machine burn-in test, and volume is little, and is simple to operation.
Description of drawings
Fig. 1 is the scheme drawing of a kind of four rotor unmanned vehicle complete machine ageing testers of providing of the utility model.
The specific 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.
The utility model is the burn-in test platform by the exploitation of Engron nurse, main purpose is the complete machine burn-in test for the md4-1000 unmanned vehicle, form the control program that flies by the various parameters of using simulated flight behind the wall of fixing aircraft, be copied to then in the unmanned vehicle complete machine, by remote controller test flight and record test data, realized the purpose of unmanned vehicle complete machine burn-in test.
Fig. 1 is the scheme drawing of a kind of four rotor unmanned vehicle complete machine ageing testers of providing of the utility model, as shown in Figure 1, comprising: test desk 101; Tested unmanned vehicle complete machine 102; Be installed in the fixed mechanism that is used for fixing tested unmanned vehicle complete machine 102 103 on the test desk 101; The direct supply 104 that connects described tested unmanned vehicle complete machine 102; And the control setup 105 that is used for carrying out burn-in test control that connects described tested unmanned vehicle complete machine 102.
Fixed mechanism 103 described in the utility model comprises four jig arm, is used for fixing respectively four arms of described tested unmanned vehicle complete machine; Be separately positioned on four rotating shafts of described four jig arm lower ends, described rotating shaft is oval, and an end of wherein said four rotating shafts is provided with shaft gear by connecting rod respectively; The bevel gear that is meshed with described shaft gear respectively; And the rocking arm that is connected with the other end of one of them rotating shaft.
Be separately installed with cam and spring between described rotating shaft and the jig arm, be used for controlling unclamping and clamping of jig arm.
Described control setup 105 comprises remote controller, is used for controlling the burn-in test of described unmanned vehicle complete machine, the data of the burn-in test of demonstration and record.
Fixed mechanism 103 on the described test desk 101 is used for fixing described unmanned vehicle complete machine 102, in test desk 101 places between test, uses jig arm to clamp four arms of unmanned vehicle complete machine 102, and it is fixed on above the test desk 101.Clamping process is to drive the bevel gear motion by rocker arms roll, realizes that with cam jig arm clamps on kinematic axis.
Described direct supply 104 is used to the needed power supply of product between the test aging period, and direct supply 104 is identical with unmanned vehicle complete machine 102 entrained cell pressures, and interface is identical, powers for machine in the burn-in test process.
The utility model is before device uses; by moving test program on computers; configure flight parameter; form driving control documents (aircraft operation control documents at the SD card; the state of flight of analog equipment; and various ultimate limit states; abnomal condition); the SD card is inserted aircraft pcb board place; then the unmanned vehicle complete machine is placed on test desk and fixes with fixed mechanism; plug direct supply, check that then installation is all qualified, close the test fender bracket; begin with remote controller test flight and record test data, reach the qualified and aging purpose of realization complete machine of test products.
In sum, the utlity model has following technique effect:
1, changed in the past with the fixing pattern of aircraft arm of screw, used anchor clamps to have good positioning and do not come off;
2, in order to prevent unreliable the flying out of aircraft propeller loading and unloading, the outer test fender bracket of also having adorned of this device;
3, fixture operation is convenient, and volume is little, and is removable.
Although above the utility model is had been described in detail, the utility model is not limited thereto, 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 (8)
1. a rotor unmanned vehicle complete machine ageing tester is characterized in that, comprising:
Test desk;
Tested unmanned vehicle complete machine;
Be installed in the fixed mechanism that is used for fixing tested unmanned vehicle complete machine on the test desk;
The direct supply that connects described tested unmanned vehicle complete machine; And
The control setup that is used for carrying out burn-in test control that connects described tested unmanned vehicle complete machine.
2. ageing tester according to claim 1 is characterized in that, described fixed mechanism comprises four jig arm, is used for fixing respectively four arms of described tested unmanned vehicle complete machine.
3. ageing tester according to claim 2 is characterized in that, described fixed mechanism also comprises four rotating shafts that are separately positioned on described four jig arm lower ends, and described rotating shaft is oval.
4. ageing tester according to claim 3 is characterized in that, an end of described four rotating shafts is provided with shaft gear by connecting rod respectively.
5. ageing tester according to claim 4 is characterized in that, described fixed mechanism also comprises bevel gear, is meshed with described shaft gear respectively.
6. ageing tester according to claim 5 is characterized in that, described fixed mechanism also comprises rocking arm, is connected with the other end of one of them rotating shaft.
7. ageing tester according to claim 3 is characterized in that, is separately installed with cam and spring between described rotating shaft and the jig arm, is used for controlling unclamping and clamping of jig arm.
8. ageing tester according to claim 1 is characterized in that, described control setup comprises remote controller, is used for controlling the burn-in test of described unmanned vehicle complete machine, the data of the burn-in test of demonstration and record.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2013200956088U CN203186583U (en) | 2013-03-01 | 2013-03-01 | Overall unit aging testing device for quad-rotor unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2013200956088U CN203186583U (en) | 2013-03-01 | 2013-03-01 | Overall unit aging testing device for quad-rotor unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203186583U true CN203186583U (en) | 2013-09-11 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2013200956088U Expired - Fee Related CN203186583U (en) | 2013-03-01 | 2013-03-01 | Overall unit aging testing device for quad-rotor unmanned aerial vehicle |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104699082A (en) * | 2015-04-01 | 2015-06-10 | 北京象限科技有限公司 | Unmanned aerial vehicle whole inertial navigation test bench |
| CN105083585A (en) * | 2015-07-10 | 2015-11-25 | 桂林航天工业学院 | Balance test system of four-rotor aircraft |
| CN106516160A (en) * | 2016-12-12 | 2017-03-22 | 哈尔滨理工大学 | Remote control testing device for rotor lift force parameters |
| CN107719700A (en) * | 2017-09-29 | 2018-02-23 | 深圳市大疆创新科技有限公司 | Unmanned vehicle method of testing and device |
-
2013
- 2013-03-01 CN CN2013200956088U patent/CN203186583U/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104699082A (en) * | 2015-04-01 | 2015-06-10 | 北京象限科技有限公司 | Unmanned aerial vehicle whole inertial navigation test bench |
| CN105083585A (en) * | 2015-07-10 | 2015-11-25 | 桂林航天工业学院 | Balance test system of four-rotor aircraft |
| 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 |
| CN107719700A (en) * | 2017-09-29 | 2018-02-23 | 深圳市大疆创新科技有限公司 | Unmanned vehicle method of testing and device |
| CN107719700B (en) * | 2017-09-29 | 2019-10-18 | 深圳市大疆创新科技有限公司 | Unmanned vehicle test method and device |
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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 | ||
| 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: 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. 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. |
|
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20130911 |