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Universal wind measurement laser radar receiving and transmitting combined telescope device

A combination of wind-measuring lidar and transceiver technology, applied in telescopes, measuring devices, optics, etc., can solve the problems of reduced system flexibility, complicated installation and adjustment, and large phase intensity noise, so as to omit the coaxial calibration process and reduce Effects of coupling loss and optical aberration reduction

Pending Publication Date: 2021-08-06
南京智速物联科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Although the optical fiber circulator has a simple structure and small size, it is conducive to integration, but its phase intensity noise is large, and it has high requirements on the line width of the laser light source, which increases the cost of the light source; while the spatial optical circulator can effectively control the intensity of stray light. It reduces the line width requirements of the light source, but it is bulky and complicated to install and adjust. At the same time, it is necessary to consider the coupling efficiency between the optical fiber and the circulator.
[0005] However, the transceiver telescopes used on the market have poor versatility and cannot be applied to two circulator schemes at the same time. The actual use may require special design, which is not conducive to product production and reduces the flexibility of the system.

Method used

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  • Universal wind measurement laser radar receiving and transmitting combined telescope device
  • Universal wind measurement laser radar receiving and transmitting combined telescope device
  • Universal wind measurement laser radar receiving and transmitting combined telescope device

Examples

Experimental program
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Embodiment 1

[0027] refer to Figure 1-2 , a general-purpose wind-measuring lidar transceiver combined telescope device, including a telescope device body, the telescope device body is connected with a circulator 1, and the telescope device body includes a collimating coupling mirror 2, a beam expander mirror 3 and a compensating mirror 4, In order to meet the requirements of coherent detection, the compensating mirror (4) is composed of a lens or lens combination that reduces system aberration, and can control the system aberration of the entire telescope within λ / 4.

[0028] The collimating coupling mirror 2 and the beam expander 3 are threadedly connected, and the beam expander 3 is provided with a Galilean beam expander. The beam expander 3 is composed of a concave lens 7 and a convex lens 8, and the aperture of the convex lens 8 is larger than that of the concave lens 7. The size of the aperture, the focal length of the convex lens 8 is greater than the focal length of the concave len...

Embodiment 2

[0031] refer to image 3 , the difference from Example 1 is:

[0032] The telescope device body includes a beam expander 3 and a compensation mirror 4. The beam expander 3 is provided with a Galilean beam expander. The beam expander 3 is composed of a concave lens 7 and a convex lens 8. The compensation mirror 4 is a doublet lens 9. It is made of two kinds of lenses in H-K9L and ZF1, and the aperture is 50.8mm. In order to meet the requirements of coherent detection, the compensating mirror 4 controls the system aberration of the entire telescope within λ / 4. Firstly, the collimation coupling The mirror 2 and the beam expander 3 are disassembled, so that this telescope device is suitable for the space optical circulator scheme, so that in the launching process, the beam emitted from the space optical circulator is a parallel beam, which is expanded by the beam expander 3 After beaming, the spot radius of the beam is expanded to 0.8 times the aperture of the compensation mirror...

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PUM

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Abstract

The invention discloses a universal wind measurement laser radar receiving and transmitting combined telescope device which comprises a telescope device body, the telescope device body is connected with a circulator, the telescope device body comprises a collimation coupling mirror, a beam expanding mirror and a compensating mirror, the collimation coupling mirror and the beam expanding mirror are arranged in a threaded connection mode, and the beam expanding mirror is arranged in a Galileo mode and is composed of a concave lens and a convex lens. By arranging the detachable collimation coupling mirror, the telescope device can be suitable for wind measurement laser radars of two schemes of an optical fiber circulator and a spatial optical circulator at the same time, the problems that existing wind measurement laser radars need to be designed separately and do not have formed products are solved, and universal design is achieved; meanwhile, the optical aberration of a telescope system is reduced through the compensating mirror, and a good imaging effect is achieved.

Description

technical field [0001] The invention relates to the technical field of wind-measuring lidar, in particular to a general-purpose wind-measuring lidar transceiver combined telescope device. Background technique [0002] Compared with traditional radar, laser wind radar has higher resolution, higher sensitivity, wider detection range and stronger anti-interference ability. It has been widely used in aerospace, meteorological observation, wind power generation and other fields. [0003] The telescope is an important part of the wind lidar. The two common circulator schemes for the wind lidar with combined transceivers are fiber optic circulators and space optical circulators. Since the laser beam emitted by the fiber optic circulator is divergent, the space The laser beams emitted by the optical circulator are parallel, so the structures of the transceiver telescopes corresponding to the two schemes are different. However, whether it is a fiber optic circulator or a spatial op...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01S17/88G01S17/95G01S7/481G02B23/00
CPCG01S17/88G01S17/95G01S7/481G01S7/4811G02B23/00Y02A90/10
Inventor 林宗强苏景佑张云山姚兆宁刘恒
Owner 南京智速物联科技有限公司
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