CN107643156A - Three axle rotational shaking tables - Google Patents
Three axle rotational shaking tables Download PDFInfo
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- CN107643156A CN107643156A CN201711032095.5A CN201711032095A CN107643156A CN 107643156 A CN107643156 A CN 107643156A CN 201711032095 A CN201711032095 A CN 201711032095A CN 107643156 A CN107643156 A CN 107643156A
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Abstract
本发明公开了一种三轴转动振动台,该三轴转动振动台由三部分组成。一、转动部分:由直流伺服电机、连接轴,转动架组成;二、摆动部分:由摆动架直流伺服电机以及传动机构组成;三、振动装置:由电动推杆,虎克铰连,球面副以及电磁振动台组成。直流伺服电机通过电机架固定在转台基座上,通过联轴器与传动轴相连接,传动轴与转动架通过键槽相连;摆动架通过键槽与转动架链接;电动推杆通过虎克铰连与球面副分别与摆动架和振动台相连接,虎克铰连通过螺栓分别与摆动架和电动推杆固定。本发明能在地面模拟飞行器空中的飞行姿态以及振动环境,避免了将航空设备安放在无人机上进行实验,从而节省了物力及人力,并且能对相机各参数做出准确的测评。
The invention discloses a three-axis rotating vibrating table, which is composed of three parts. 1. Rotating part: composed of DC servo motor, connecting shaft, and turret; 2. Swing part: composed of DC servo motor and transmission mechanism of the swing frame; 3. Vibration device: composed of electric push rod, Hooke hinge, spherical pair And the composition of the electromagnetic vibrating table. The DC servo motor is fixed on the base of the turntable through the motor frame, connected with the transmission shaft through the coupling, and the transmission shaft is connected with the turret through the keyway; the swing frame is connected with the turret through the keyway; The spherical pair is respectively connected with the swing frame and the vibrating table, and the Hooke hinge is respectively fixed with the swing frame and the electric push rod through bolts. The invention can simulate the flight attitude and vibration environment of the aircraft on the ground, avoids placing aviation equipment on the drone for experiments, thereby saving material resources and manpower, and can accurately evaluate the parameters of the camera.
Description
技术领域technical field
本发明公开了一种三轴转动振动台装置,具体就是模拟影响无人机空中拍照质量的影响因子,本发明主要模拟无人机空中横滚和俯仰的运动姿态以及振动环境。The invention discloses a three-axis rotating vibrating table device, specifically simulating the influencing factors that affect the aerial photographing quality of an unmanned aerial vehicle. The invention mainly simulates the motion posture and the vibration environment of the aerial roll and pitch of the unmanned aerial vehicle.
背景技术Background technique
航空相机是安装在无人机上对地面景物拍照的精密光学仪器。飞机的振动,气流变化、飞机俯仰角的变化都会影响航空相机的拍照清晰度,所以为了提高航空相机的拍照质量需要对航空相机进行多次实验,而实际飞行需要大量的人力物力以及资金的投入。为了减少资金的投入以及缩短研制周期,如何能在地面模拟影响航空相机拍照清晰度的影响因子。现有的电磁振动器可以模拟0.5~10khz的振动频率,但电磁振动器位移比较小不能实现打的俯仰角,而液压振动器虽然有大的位移可以实现大的俯仰角,但其振动频率只能实现在0.5~200hz。而影响拍照质量的频率要高于50hz。Aerial cameras are precision optical instruments installed on drones to take pictures of ground scenes. The vibration of the aircraft, the change of the airflow, and the change of the pitch angle of the aircraft will all affect the photographing clarity of the aerial camera. Therefore, in order to improve the photographing quality of the aerial camera, it is necessary to conduct many experiments on the aerial camera, and the actual flight requires a lot of manpower, material resources and capital investment. . In order to reduce capital investment and shorten the development cycle, how to simulate on the ground the factors that affect the clarity of aerial camera photography. The existing electromagnetic vibrator can simulate the vibration frequency of 0.5~10khz, but the displacement of the electromagnetic vibrator is relatively small and the pitch angle cannot be achieved. Although the hydraulic vibrator has a large displacement and can achieve a large pitch angle, its vibration frequency is only It can be realized at 0.5~200hz. The frequency that affects the photo quality is higher than 50hz.
如何在实验室即能实现大的俯仰角,又能实现大的振动频率,是航空相机地面姿态扰动发生装置急需解决的问题。How to achieve a large pitch angle and a large vibration frequency in the laboratory is an urgent problem to be solved for the ground attitude disturbance generator of the aerial camera.
发明内容Contents of the invention
针对现有技术的缺陷,本发明提供了一种三轴转动振动台装置。主要由由三部分组成。第一部分转动部分,是由直流伺服电机,转动连接轴,转动架组成;第二部分是摆动装置由摆动架直流伺服电机以及传动机构组成;第三部分是俯仰以及振动装置是由电动推杆,虎克铰连,球面副以及电磁振动台;转动部分包括底座、电机、链接件以及转动架;摆动装置是由电机以及摆动支架组成;俯仰以及振动装置是由电动推杆和电磁振动台组成。直流伺服电机通过电机架固定在转台基座上,通过联轴器与传动轴相连接,传动轴与转动架通过键槽相连;摆动架通过键槽与转动架链接;电动推杆通过虎克铰连与球面副分别与摆动架和振动台相连接,虎克铰连通过螺栓分别与摆动架和电动推杆固定。Aiming at the defects of the prior art, the present invention provides a three-axis rotating vibrating table device. It mainly consists of three parts. The first part is the rotating part, which is composed of DC servo motor, rotating connecting shaft and turret; the second part is the swing device, which is composed of the swing frame DC servo motor and the transmission mechanism; the third part is the pitching and vibration device, which is composed of an electric push rod, Hooke hinge, spherical pair and electromagnetic vibration table; the rotating part includes base, motor, link and turret; the swing device is composed of motor and swing bracket; the pitch and vibration device is composed of electric push rod and electromagnetic vibration table. The DC servo motor is fixed on the base of the turntable through the motor frame, connected with the transmission shaft through the coupling, and the transmission shaft is connected with the turret through the keyway; the swing frame is connected with the turret through the keyway; The spherical pair is respectively connected with the swing frame and the vibrating table, and the Hooke hinge is respectively fixed with the swing frame and the electric push rod through bolts.
三轴转动振动台是航空相机地面空中环境模拟装置。可以在实验室对航空相机进行空中飞行模拟,并能够为航空相机的空中性能提供重要参数,从而减少使用实际飞行对其进行检测,进而可以减少人力、物力、以及资金投资,而且缩短了研制周期。The three-axis rotating vibration table is an aerial camera ground air environment simulation device. The aerial flight simulation of the aerial camera can be carried out in the laboratory, and it can provide important parameters for the aerial performance of the aerial camera, thereby reducing the use of actual flight to test it, thereby reducing manpower, material resources, and capital investment, and shortening the development cycle .
本发明是实现在实验室内对航空相机进行检测,其主要技术基础是模拟飞机在空中的振动,横滚,俯仰。通过被测相机对景物的拍照,分析,对航空相机的各项技术指标做出详细的综合性评价。The invention realizes the detection of the aerial camera in the laboratory, and its main technical basis is to simulate the vibration, rolling and pitching of the aircraft in the air. Through the photographing and analysis of the scene by the camera under test, a detailed comprehensive evaluation is made on various technical indicators of the aerial camera.
附图说明Description of drawings
图1是为三轴转动振动台结构示意图。Figure 1 is a schematic diagram of the structure of a three-axis rotating vibration table.
图2 是图1的辅助结构示意图。FIG. 2 is a schematic diagram of an auxiliary structure of FIG. 1 .
图中 1-底座、2-起吊环、3-转动轴、4-转动架、5-摆动架、6-虎克铰连、7-电动推杆、8-电磁振动台、9-挡块、10-球面副、11-振动台面。In the figure, 1-base, 2-lifting ring, 3-rotation shaft, 4-turret, 5-swing frame, 6-Hooke hinge, 7-electric push rod, 8-electromagnetic vibration table, 9-block, 10-spherical pair, 11-vibration table.
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Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108801573A (en) * | 2018-06-14 | 2018-11-13 | 北京卫星环境工程研究所 | Spacecraft high resolution camera optical jitter micro-vibration source ground simulator |
CN108801574A (en) * | 2018-06-15 | 2018-11-13 | 北京卫星环境工程研究所 | The verification system of spacecraft high score camera optical axis jitter performance |
CN108825941A (en) * | 2018-05-03 | 2018-11-16 | 长春工业大学 | A kind of Airborne Camera ground motion test device of multiaxis cooperative motion |
CN108877456A (en) * | 2018-09-01 | 2018-11-23 | 长春工业大学 | Gantry arc orbit simulation test stand |
CN110531566A (en) * | 2019-09-27 | 2019-12-03 | 长春工业大学 | A kind of long-focus based on piezoelectric actuator, which pushes away, sweeps camera apparatus |
CN111157268A (en) * | 2020-01-13 | 2020-05-15 | 吉林大学 | Public transport seat reliability test device |
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Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108825941A (en) * | 2018-05-03 | 2018-11-16 | 长春工业大学 | A kind of Airborne Camera ground motion test device of multiaxis cooperative motion |
CN108801573A (en) * | 2018-06-14 | 2018-11-13 | 北京卫星环境工程研究所 | Spacecraft high resolution camera optical jitter micro-vibration source ground simulator |
CN108801574A (en) * | 2018-06-15 | 2018-11-13 | 北京卫星环境工程研究所 | The verification system of spacecraft high score camera optical axis jitter performance |
CN108877456A (en) * | 2018-09-01 | 2018-11-23 | 长春工业大学 | Gantry arc orbit simulation test stand |
CN110531566A (en) * | 2019-09-27 | 2019-12-03 | 长春工业大学 | A kind of long-focus based on piezoelectric actuator, which pushes away, sweeps camera apparatus |
CN110531566B (en) * | 2019-09-27 | 2024-03-29 | 长春工业大学 | Long-focus push-broom camera device based on piezoelectric actuator |
CN111157268A (en) * | 2020-01-13 | 2020-05-15 | 吉林大学 | Public transport seat reliability test device |
CN111157268B (en) * | 2020-01-13 | 2021-07-30 | 吉林大学 | A reliability test device for public transportation seats |
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Application publication date: 20180130 |