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Airborne liquid cooling type reconnaissance and interference integrated device

A liquid cooling and cabinet technology, applied in cooling/ventilation/heating transformation, chassis/cabinet/drawer parts, electrical components, etc. The problems of large total volume and total weight can achieve the effect of simplifying the relationship between electrical interface and mechanical interface, reducing the total installed volume and total weight, and improving the complexity of liquid cooling pipelines.

Pending Publication Date: 2020-09-18
NO 54 INST OF CHINA ELECTRONICS SCI & TECH GRP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] At present, traditional airborne reconnaissance jamming equipment usually includes more than 10 chassis such as power amplifier chassis, power supply chassis, reconnaissance processing chassis, power switch module, transmitting antenna switch, and receiving antenna switch in different frequency bands. The functions, the size and weight of the chassis are different, resulting in a large number of chassis, a large total volume and weight of the equipment, complex cable connection relationships between the chassis, and poor maintenance of the equipment, which greatly limits the potential performance of the airborne platform's function expansion.
At the same time, each high-power chassis has a large heat consumption, which requires liquid cooling to dissipate heat, and the layout of the liquid cooling pipeline is also relatively complicated.

Method used

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  • Airborne liquid cooling type reconnaissance and interference integrated device
  • Airborne liquid cooling type reconnaissance and interference integrated device
  • Airborne liquid cooling type reconnaissance and interference integrated device

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Embodiment Construction

[0032] Below, the present invention will be further described in conjunction with the accompanying drawings and specific embodiments.

[0033] refer to Figure 1 to Figure 8 , an airborne liquid-cooled reconnaissance and interference integrated device, comprising a box body 1, a circulating flow channel for maintaining heat dissipation is arranged in the box body, an intercooling plate is placed horizontally in the box body, and the intercooling plate connects the box body The cavity is divided into an upper cavity and a lower cavity; the upper surface of the intercooler plate and the upper surface of the lower bottom plate 15 of the box are all provided with track grooves for snapping into the module;

[0034] The low-power module is inserted into the track slot of the upper cavity, and the high-power module 7 is inserted into the track slot of the lower cavity; the back of the upper cavity is the upper printed backplane 8, and the upper printed backplane and the low-power T...

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PUM

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Abstract

The invention discloses an airborne liquid cooling type reconnaissance and interference integrated device, which belongs to the technical field of electronic equipment. The device comprises a box bodyserving as a main body of the device, and all functional modules for executing a reconnaissance interference task are integrally mounted in the box body through unified design of the functional modules; an upper-lower double-layer structure form is adopted; a plurality of low-power modules are arranged on the upper layer, a plurality of high-power modules are arranged on the lower layer, and a plurality of runners are further arranged in the box body for heat dissipation of the modules. The total volume and the total weight of the loading machine are greatly reduced, and the relation betweenan electrical interface and a mechanical interface of the loading machine is greatly simplified.

Description

technical field [0001] The invention relates to the technical field of electronic equipment, in particular to an airborne liquid-cooled integrated reconnaissance and interference device. Background technique [0002] As more and more airborne reconnaissance and jamming equipment perform reconnaissance and jamming tasks in multiple frequency bands, and there are more and more equipment in the aircraft, this requires airborne equipment to be lightweight, integrated, efficient in heat dissipation, and good in electromagnetic compatibility. and other functional integration direction; the basis for achieving the above goals is the improvement of the integration degree of electronic modules, the enhancement of computing power and data processing capacity. The increase in the integration of electronic modules leads to an increase in the thermal power density of the module itself, and the limited space on the carrier requires small equipment, low volume and weight, and simple cable ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H05K5/02H05K5/06H05K7/20
CPCH05K5/0217H05K5/0247H05K5/06H05K5/069H05K7/20254H05K7/20272
Inventor 梁国张朝王金奎王建杨忠陈诗超郑国宏孙彤辉安宁
Owner NO 54 INST OF CHINA ELECTRONICS SCI & TECH GRP
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