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Embedded shaking system of laser gyroscope

A laser gyro and embedded technology, applied in the direction of Sagnac effect gyroscope, etc., can solve the problem of uneven heat transfer between the shell and the resonant cavity, so as to improve the uniformity and assembly stress, enhance the rigidity, and solve the problem of uneven heat transfer. uniform effect

Active Publication Date: 2021-04-16
HUAZHONG PHOTOELECTRIC TECH INST (CHINA SHIPBUILDING IND CORP THE NO 717 INST)
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  • Claims
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Problems solved by technology

[0004] The invention provides a laser gyro embedded shaking system, which cancels the shell boss structure, integrates the supporting boss and the shaking wheel in the prior art, and solves the uneven heat transfer between the shell and the resonant cavity from the structural design At the same time, the stiffness of the laser gyro shaking system is improved to the greatest extent, and it also effectively avoids the problem that the shaking performance of the laser gyro is affected by the inconsistency of the screw installation torque between the shell support boss and the shaking wheel

Method used

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  • Embedded shaking system of laser gyroscope

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Embodiment Construction

[0014] Embodiments of the present invention will be described in detail below in conjunction with the accompanying drawings.

[0015] Such as figure 1 As shown, the structure of this embodiment includes an embedded vibrating wheel 1, a piezoelectric ceramic sheet 2, a disc base 3 and a planar shell 5, and a piece of piezoelectric ceramic is provided on both sides of the spoke 6 of the embedded vibrating wheel 1. The sheet 2, the lower end of the embedded vibrating wheel 1 is fixedly connected with the disc base 3, and the disc base 3 is fixed at the inner bottom of the planar shell 5.

[0016] In this embodiment, the lower end of the embedded vibrating wheel 1 and the disc base 3 are integrally structured.

[0017] In this embodiment, the lower end of the embedded shaking wheel 1 is evenly provided with a plurality of supporting steel columns 5 integrally structured with the shaking wheel 1 along the circumferential direction, and the lower ends of the steel columns 5 are int...

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Abstract

The invention provides an embedded shaking system of a laser gyroscope, a shell boss structure is canceled, and a supporting boss and a shaking wheel in the prior art are integrated into a whole, so that the problem of non-uniform heat transfer between the shell and a resonant cavity is solved from the aspect of structural design, and meanwhile, the rigidity of the laser gyroscope shaking system is improved to the maximum extent; the problem that the jittering performance of the laser gyroscope is affected by inconsistent screw installation torque of the shell supporting boss and the jittering wheel is effectively avoided. According to the technical scheme, the laser gyro comprises the embedded shaking wheel, piezoelectric ceramic pieces, a disc base and a planar shell, the two side faces of each spoke of the embedded shaking wheel are each provided with one piezoelectric ceramic piece, and the two ends of each spoke of the embedded shaking wheel are each provided with one piezoelectric ceramic piece. The lower end of the embedded shaking wheel is fixedly connected with a disc base, and the disc base is fixed to the inner bottom of the planar shell.

Description

technical field [0001] The invention relates to the technical field of laser gyroscope manufacturing, in particular to a laser gyroscope embedded shaking system. Background technique [0002] In order to eliminate the influence of the blocking effect that the laser gyroscope cannot measure small angular rates, the current jitter bias technology is usually used. Since the mechanical jitter bias technology does not increase the complexity of the optical path and does not introduce cumulative errors, the machine jitter bias technology has been the most widely used. [0003] Due to the difference between the application environment of the shaking mechanism and the shell, the shaking mechanism usually uses super Invar (Invar) material with a low expansion coefficient, and the shell is made of high-strength and corrosion-resistant aviation duralumin (7075) material. It is separated from the resonant cavity by a certain distance, and the shell is usually processed with a structure...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01C19/66
Inventor 王利伟杨志斌孙仁胜王强
Owner HUAZHONG PHOTOELECTRIC TECH INST (CHINA SHIPBUILDING IND CORP THE NO 717 INST)