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Laser cooling device for aircraft laser guidance instrument

A laser guidance and cooling device technology, applied in laser cooling devices, household refrigeration devices, semiconductor lasers, etc., can solve the problem that the refrigeration unit cannot meet the cooling requirements, and achieve the effect of good cooling effect, small cooling system and flexible layout.

Inactive Publication Date: 2011-08-10
HARBIN INST OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to solve the problem that the existing ventilation cooling, water cooling, electric cooling and refrigerating unit cannot cool the laser of the aircraft laser guidance instrument, and provides a laser cooling device for the aircraft laser guidance instrument

Method used

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  • Laser cooling device for aircraft laser guidance instrument
  • Laser cooling device for aircraft laser guidance instrument
  • Laser cooling device for aircraft laser guidance instrument

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specific Embodiment approach 1

[0008] Specific implementation mode one: the following combination Figure 1 to Figure 5 Describe this embodiment, this embodiment comprises liquid ammonia evaporative cooler 1, liquid ammonia bottle 2, circulating water pump 3 and solenoid valve 4, and liquid ammonia evaporative cooler 1 is shell-and-tube structure, and liquid ammonia evaporative cooler 1 consists of shell 1 -1 and the cooling water coil 1-2, the cooling water coil 1-2 is arranged inside the housing 1-1, the water inlet and outlet of the cooling water coil 1-2 are exposed outside the housing 1-1, and the liquid ammonia The bottle 2 is filled with liquid ammonia, an electromagnetic valve 4 is set between the liquid ammonia bottle 2 and the ammonia inlet of the casing 1-1, and the water outlet of the cooling water coil 1-2 is connected with the circulating water pump 3.

[0009] The outlet of the liquid ammonia bottle 2, the liquid ammonia inlet of the shell 1-1 and the ammonia vapor outlet of the shell 1-1 are...

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Abstract

The invention relates to a laser cooling device for an aircraft laser guidance instrument, belonging to the field of laser refrigeration. The laser cooling device aims at solving the problem that the existing ventilation cooling, water cooling, electricity refrigeration cooling and refrigeration machine set can not meet the cooling of the laser of the aircraft laser guidance instrument, and comprises a liquid ammonia steaming evaporative cooler, a liquid ammonia cylinder, a circulating water pump and an electromagnetic valve, wherein the liquid ammonia steaming evaporative cooler is a shell-and-tube structure and consists of a shell and a cooling water coil tube; the cooling water coil tube is arranged inside the shell; a water inlet and a water outlet of the cooling water coil pipe are exposed out of the shell; the liquid ammonia cylinder is internally filled with liquid ammonia; the electromagnetic valve is arranged between the liquid ammonia cylinder and the ammonia inlet of the shell; and the water outlet of the cooling water coil pipe is connected with the circulating water pump. The laser cooling device is used for the cooling of the laser of the aircraft laser guidance instrument.

Description

technical field [0001] The invention relates to a laser cooling device for aircraft laser guidance instruments, which belongs to the field of laser refrigeration. Background technique [0002] The aircraft laser guidance instrument system will generate a certain amount of heat during the working process, which will increase the temperature of the instrument itself and affect its working accuracy. In order to ensure the working accuracy of the laser-guided instrument and make it work within a certain temperature range, it is necessary to discharge the heat generated during the working process of the instrument in time. Therefore, it is necessary to develop a refrigeration system that can meet the requirements of the stable operation of the laser guidance instrument system of the aircraft. [0003] There are many ways to discharge the heat generated during the working process of the laser guidance instrument system: cooling methods such as ventilation cooling, water cooling, ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): H01S5/024H01S3/04F25D3/10
Inventor 孙剑峰付忠斌李炳熙李琦王骐
Owner HARBIN INST OF TECH