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An integrated spatial precision two-dimensional scanning mechanism
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A scanning mechanism and precise technology, applied in the field of aerospace, can solve the problems of unable to meet the mechanical interface requirements of hyperspectral detectors, large volume, large power consumption, etc., and achieve the effects of high-precision control, small size, and simple assembly
Active Publication Date: 2019-01-01
SHANGHAI INST OF TECHNICAL PHYSICS - CHINESE ACAD OF SCI
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[0004] It is common to use dual motor drive to realize the two-dimensional scanning structure. The advantage is that it has good adaptability and can meet the requirements of two-dimensional large-angle scanning. The disadvantage is that the volume and power consumption are large, and it cannot meet the mechanical interface requirements of the hyperspectral detector.
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[0027] In order to have a deeper understanding of the present invention, a specific embodiment is listed below, and the present invention is further described in detail in conjunction with the accompanying drawings.
[0028] This example is an integrated, lightweight, and high-pointing two-dimensional scanning mechanism that can adapt to high vacuum and microgravity environments. It is composed of a cross-track scanning mechanism and an along-track scanning mechanism. The overall appearance of the mechanism is as follows: Figure 1-Figure 6 shown.
[0029] like figure 1As shown, the cross-track scanning mechanism mainly includes a scanning mirror 1, a front hinge assembly support 2, a front sealing inner ring 3, a front sealing outer ring 4, a front bearing assembly 5, a rotating shaft 6, a rotating motor 7, and a front housing 8 of the scanning mechanism , angular displacement sensor 9, rear bearing assembly 10, rear sealing inner ring 11, rear sealing outer ring 12, middle ...
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Abstract
The invention discloses a precise and two-dimensional scanning mechanism with integrated space, comprising a rail-crossing scanning mechanism and a rail-along scanning mechanism, wherein the rail-crossing scanning mechanism comprises a scanning mirror, a front shell of the scanning mechanism,a middle end cover of the scanning mechanism, a rotary motor, an angular displacement sensor, a rotary shaft, a bearing assembly, a linear motion shaft,a front hinge assembly, a rear hinge assembly, a front hinge assembly support,a rear hinge assembly support and a seal ring; and the rail-along scanning mechanism comprises a scanning mirror, a linear motor, a linear motion shaft, a rear shell of the scanning mechanism, a rotary shaft, a front hinge assembly, a rear hinge assembly, a front hinge assembly support, a rear hinge assembly support, a seal cover of the linear motor, a front limiting device and a rear limiting device. The advantages of the invention are as follows: compared with the traditional two-dimensional scanning mechanism, the two-dimensional scanning mechanism has the features of integration, light-small type, high pointing precision, low assembly difficulty, etc. One dimension can rotate around 360 degrees, the rotary angle of the other dimension can be confirmed by the limiting device, and the rail-crossing scanning and rail-along scanning are alternative.
Description
technical field [0001] The invention relates to a space two-dimensional scanning mechanism, in particular to an integrated precision two-dimensional scanning mechanism for space photoelectric remote sensing instruments, belonging to the field of aerospace technology. Background technique [0002] Space remote sensing instruments have extremely important uses in space research, earth observation, weather forecasting, and national defense modernization. They are an important means for human beings to develop and utilize space resources, and are the core technology for the development of space payload applications. The FY-1 and FY-3 meteorological satellites of the Fengyun series launched by my country use satellite flight + one-dimensional scanning, and FY-2 uses satellite spin + one-dimensional scanning. The scanning radiometer, medium-resolution spectral imager, infrared spectrometer and other loads on the FY-3 satellite use a 45° scanning mirror to rotate and scan, and the ...
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Application Information
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Patent Type & Authority Patents(China)
IPC IPC(8): G02B26/08G02B26/10
CPCG02B26/0816G02B26/10
Inventor 陈星袁杰顾明剑宋晓伟刘涛
Owner SHANGHAI INST OF TECHNICAL PHYSICS - CHINESE ACAD OF SCI