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A Highly Reliable Circuit Based on Shock Absorbing System

A shock-absorbing system and a reliable technology, applied in space navigation equipment, space navigation vehicles, space navigation equipment, etc., can solve problems such as unfavorable heat dissipation of power modules or active devices, lower device performance, and increase structural space , to achieve the effect of reducing the risk of failure, improving reliability, and symmetrical and compact structure

Active Publication Date: 2020-08-18
SHANGHAI AEROSPACE CONTROL TECH INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The disadvantage of this type of installation method is that the filling glue on the board is not conducive to the heat dissipation of the power module or active devices, and at the same time, under high temperature conditions, it will cause thermal stress and reduce the normal working performance of the devices
The use of springs or non-metallic materials not only has high manufacturing costs, but also increases the structural space and complicates assembly.

Method used

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  • A Highly Reliable Circuit Based on Shock Absorbing System
  • A Highly Reliable Circuit Based on Shock Absorbing System
  • A Highly Reliable Circuit Based on Shock Absorbing System

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Embodiment Construction

[0036] The present invention will be further elaborated below by describing a preferred specific embodiment in detail in conjunction with the accompanying drawings.

[0037] Such as Figure 1~3 As shown, the present invention provides a highly reliable circuit based on a shock absorbing system, which includes: a power supply unit 1, which is an object to be shock-absorbed, and which includes a cooling plate 8. In this embodiment, the cooling plate 8 is arranged on a mounting surface A plurality of power supply modules, a power supply circuit board is arranged on the other mounting surface of the cooling plate 8; the overall structure of the cooling plate 8 is similar to a cuboid structure, and a plurality of opening slots are opened on the end surface of the cooling plate 8, threaded holes are opened on four sides, and four There are through holes on the top corner, and the four through holes are symmetrically arranged respectively. The welding pins pass through the opening gr...

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Abstract

The invention discloses a high-reliability circuit based on a vibration reduction system. The high-reliability circuit comprises a power supply part, a fixed frame, a navigation circuit board, four vibration reduction devices, and an optical fiber inertial navigation shell, wherein the power supply part is an object to be carried out vibration reduction, and comprises a heat dissipation plate; thefixed frame is fixed on the periphery of the heat dissipation plate of the power supply part, the navigation circuit board is fixed on the fixed frame, and the four vibration reduction devices, are located at the four vertexes of the heat dissipation plate correspondingly; and a structure composed of the power supply part, the fixed frame, the navigation circuit board and the four vibration reduction devices is arranged inside the optical fiber inertial navigation shell, the four vibration reduction devices are connected with the interior of the optical fiber inertial navigation shell and theheat dissipation plate through a first screw and a first nut. The high-reliability circuit has the advantages that the modularization is realized, the integral assembly is simple, the structure is symmetrical and compact, the vibration reduction systematization configuration is simple, the space volume is saved, the anti-vibration property is good, and the risk of failure of components such as crystal oscillators is reduced, and the reliability of components on a navigation board and a power circuit board is integrally improved.

Description

technical field [0001] The invention relates to the technical field of circuits with a shock absorbing structure, in particular to a highly reliable circuit based on a shock absorbing system. Background technique [0002] The fiber-optic inertial navigation of space round-trip aircraft provides real-time position and attitude information for the aircraft. Severe random vibration is the main mechanical environment faced by the fiber optic inertial navigation system on the aircraft, and these vibrations are transmitted to the fiber optic inertial navigation system installed on the aircraft. When the PCB vibrates violently, electronic components such as electronic components such as crystal oscillators that are sensitive to vibration will cause pin breakage or functional failure, and if the vibration level is too large, the performance of the device in working condition will also be at risk of performance degradation. In order to provide a good dynamic working environment, red...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01C21/16B64G1/66
CPCB64G1/66G01C21/16
Inventor 吴成智吴枫谷丛林建华邵添羿孙家骥幸伟高福隆杨文平薛劲松
Owner SHANGHAI AEROSPACE CONTROL TECH INST