A cooling device for an inertial navigation module

A heat dissipation device and inertial navigation technology, applied in the direction of measuring devices, microstructure devices, microelectronic microstructure devices, etc., can solve the problems of poor effect and difficulty in heat dissipation of inertial navigation modules, and achieve convenient and reliable installation, reduce The overall size, the effect of enhancing the heat dissipation performance

Active Publication Date: 2022-03-04
UNIV OF ELECTRONICS SCI & TECH OF CHINA
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Problems solved by technology

[0004] Aiming at the problem that the heat dissipation effect of the inertial navigation module is difficult and the effect is not good in the prior art, the present invention provides a heat dissipation device for the inertial navigation module, which can adopt a flow-pressure controlled parallel independent heat dissipation method to cope with different positions of the inertial navigation module. Cooling requirements for inertial navigation modules such as accelerometers and gyroscopes can be efficiently, intelligently and safely dissipated

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  • A cooling device for an inertial navigation module
  • A cooling device for an inertial navigation module
  • A cooling device for an inertial navigation module

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Embodiment Construction

[0030] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, and are not intended to limit the present invention, that is, the described embodiments are only some of the embodiments of the present invention, but not all of the embodiments. The components of the embodiments of the invention generally described and illustrated in the figures herein may be arranged and designed in a variety of different configurations.

[0031] Accordingly, the following detailed description of the embodiments of the invention provided in the accompanying drawings is not intended to limit the scope of the claimed invention, but merely represents selected embodiments of the invention. Based on the embodiments of the...

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Abstract

The invention discloses a heat dissipation device for an inertial navigation module, belonging to the technical field of fluid heat dissipation, comprising: a microchannel radiator adopting a shower type multi-channel mixed impact heat dissipation structure, a micropump, a liquid outlet pipe, and corresponding to each chip A number of shunt tubes, multi-channel fluid control valves, return chambers and heat dissipation fins arranged on each shunt pipe; there is a thermal conductive coating between the micro-channel radiator and the PCB board of the inertial navigation chip; through the return chamber and heat dissipation fins The heat dissipation working fluid cooled by the chip is pumped out by the micro pump, and enters the multi-channel fluid control valve through the liquid outlet pipe. The multi-channel fluid control valve changes the flow rate of the working fluid in the shunt pipe based on the real-time temperature of the chip, and the cooled heat dissipation working fluid is introduced through the shunt pipe. The micro-channel radiator, after absorbing the heat of the chip, enters the reflow cavity to form a heat dissipation circuit. The invention can realize intelligent heat dissipation for different regions on the inertial navigation module.

Description

technical field [0001] The invention relates to the technical field of fluid heat dissipation, in particular to a heat dissipation device for an inertial navigation module. Background technique [0002] Gyroscope (also known as angular motion detector) is an instrument that uses the conservation of angular momentum to obtain the precise orientation of moving objects. It is an inertial navigation spare part widely used in modern aerospace and defense industries. It is used in modern drones. Or anti-drone flight control system is widely used, has very important strategic significance. Generally speaking, inertial navigation components such as gyroscopes and accelerometers will be packaged on the same PCB board with other types of chips, such as high-performance LDO power chips, high-performance Cortex-Mo core processors, and highly integrated MEMS sensor chips. Made inertial navigation module. However, with the improvement of chip integration, the heat generated by the chip ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B81B7/00G01C21/16G01C21/18
CPCB81B7/0093G01C21/16G01C21/18B81B2201/0228
Inventor 徐尚龙李强强卫士腾周川翔
Owner UNIV OF ELECTRONICS SCI & TECH OF CHINA
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