一种用于光通信的机载光电设备

Through innovative design of the mounting base, frame, and optical receiver, the problems of large size and high maintenance difficulty of airborne optoelectronic equipment have been solved, realizing the miniaturization and ease of maintenance of the equipment, and improving the reliability and ease of operation of the equipment.

CN224511483UActive Publication Date: 2026-07-17ARMOR ACADEMY OF CHINESE PEOPLES LIBERATION ARMY

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
ARMOR ACADEMY OF CHINESE PEOPLES LIBERATION ARMY
Filing Date
2025-07-08
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

Existing airborne optoelectronic equipment is large in size and weight, and difficult to maintain, making it difficult to meet the requirements of modern aviation platforms for equipment miniaturization, lightweighting, high reliability, and ease of maintenance.

Method used

The structure adopts a mounting base, a first frame, a second frame, and optoelectronic components. It combines multiple optical receivers arranged in a ring and a two-frame structure to achieve comprehensive reception of optical signals and convenient maintenance. It can be connected to drones or light aircraft through conventional connection methods and uses electronic calibration technology to improve optical axis consistency.

Benefits of technology

It achieves miniaturization and lightweighting of the equipment, simplifies the maintenance process, improves the reliability and ease of operation of the equipment, and is suitable for small aircraft with limited load capacity.

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    Figure CN224511483U_ABST
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Abstract

本实用新型涉及一种用于光通信的机载光电设备,其包括安装底座、第一框架、第二框架以及光电组件。安装底座上环形间隔设置有多个光学接收器,光学接收器能够接收由光电组件发射后反射回的光信号,安装底座的一端能够与无人机或轻型飞机可拆卸连接。第一框架与安装底座通过第一轴系机构转动连接,第二框架与第一框架通过第二轴系机构转动连接,光电组件设置于第二框架中。采用多个光学接收器环形排布弥补单个探测器视场小的不足。光学接收器采用分散布置的多个模块设计,维修更换便捷,简化了维护流程,提高设备的可靠性和操作便捷性。两框架结构简单、且体积小重量轻,用于单载荷或多载荷的小型光电平台上,适装于带载能力有限的小型飞机。
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Claims

1. An airborne optoelectronic device for optical communication, characterized in that, The airborne optoelectronic device for optical communication comprises a mounting base (4), a first frame (1), a second frame (2) and an optoelectronic assembly (3); A plurality of optical receivers (5) are annularly and spacedly arranged on the mounting base (4), the optical receivers (5) can receive optical signals reflected after being emitted by the optoelectronic assembly (3), and one end of the mounting base (4) can be detachably connected with a drone or a light aircraft; The first frame (1) is rotationally connected with the mounting base (4) through a first shafting mechanism, the second frame (2) is rotationally connected with the first frame (1) through a second shafting mechanism, and the optoelectronic assembly (3) is arranged in the second frame (2).

2. The airborne optoelectronic equipment for optical communications of claim 1, wherein, The mounting base (4) comprises a fixing seat (41) and an adapter seat (42); A plurality of the optical receivers (5) are arranged on the fixing seat (41), the adapter seat (42) is connected with the fixing seat (41), and the first frame (1) is rotationally connected with the adapter seat (42) through the first shafting mechanism.

3. The airborne optoelectronic device for optical communication of claim 2, wherein, The fixing seat (41) is in the shape of a circular truncated cone, a plurality of mounting holes (43) are spacedly arranged on the side surface of the fixing seat (41), and a plurality of the optical receivers (5) are detachably connected with the mounting holes (43) in one-to-one correspondence.

4. The airborne optoelectronic device for optical communication of claim 3, wherein, An annular groove (44) is arranged on the inner side surface of the fixing seat (41), a connecting groove (45) is arranged at the position corresponding to each of the mounting holes (43), and the two ends of the connecting groove (45) are respectively in communication with the annular groove (44) and the mounting hole (43) in one-to-one correspondence. A threading hole is arranged on the fixing seat (41) and is in communication with the groove bottom of the annular groove (44).

5. The airborne optoelectronic device for optical communication of claim 3, wherein, The optical receiver (5) comprises, in sequence along the propagation path of light, a filter (51), a lens (52) and a detector (53), the filter (51) is arranged in the mounting hole (43), and the lens (52) and the detector (53) are arranged in the fixing seat (41).

6. The airborne optoelectronic device for optical communication of claim 1, wherein, The number of the optical receivers (5) is eight.

7. The airborne optoelectronic device for optical communication of claim 1, wherein, The optoelectronic assembly (3) comprises a mounting rack (31) and a visible light camera, an image tracker, a laser range finder and a servo controller arranged on the mounting rack (31), and the mounting rack (31) is detachably connected with the second frame (2).

8. The airborne optoelectronic device for optical communication of claim 7, wherein, The visible light camera and the laser range finder are detachably connected with the mounting rack (31) through an adjusting block.

9. The airborne optoelectronic device for optical communication of claim 7, wherein, The lens (52) of the laser range finder is a cylindrical lens (52).