Six-degree-of-freedom quasi-zero-rigidity vibration isolation system based on Stewart platform

A quasi-zero stiffness, vibration isolation system technology, applied in non-rotation vibration suppression and other directions, to achieve the effect of increasing the vibration isolation frequency band, improving the vibration isolation effect, and ensuring the bearing capacity

Inactive Publication Date: 2015-11-11
XI AN JIAOTONG UNIV
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However, there are few studies on applying the principle of quas

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  • Six-degree-of-freedom quasi-zero-rigidity vibration isolation system based on Stewart platform
  • Six-degree-of-freedom quasi-zero-rigidity vibration isolation system based on Stewart platform
  • Six-degree-of-freedom quasi-zero-rigidity vibration isolation system based on Stewart platform

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[0025] The present invention will be further described in detail below in conjunction with specific embodiments.

[0026] Such as figure 1 As shown, a quasi-zero stiffness vibration isolation system based on the Stewart platform of the present invention includes an upper platform 1, a lower platform 4, six identical legs 3, a hinge block 5, and a first screw 2. The two ends of the leg 3 are fixed on the hinge block 5, and there are three hinge blocks 5 on the upper platform 1 and the lower platform 4, and the three hinge blocks are distributed in the form of an equilateral triangle. The hinge block 5 is fixed on the upper platform 1 and the lower platform 4 by the first screw 2. The Stewart platform is a cuboid structure with two adjacent legs perpendicular to each other. Since the length of the six outriggers is variable, the upper platform has six degrees of freedom relative to the lower platform. Install the equipment that needs vibration isolation on the upper platform to i...

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Abstract

The invention provides a six-degree-of-freedom quasi-zero-rigidity vibration isolation system based on a Stewart platform. The system comprises an upper platform, a lower platform and six same landing legs fixed between the upper platform and the lower platform through hinge blocks. The three hinge blocks are distributed in an equilateral triangle mode, two corresponding landing legs are fixed to each hinge block, the adjacent landing legs are perpendicular, and the upper platform has six degrees of freedom relative to the lower platform. The six landing legs have the quasi-zero-rigidity characteristic, so that the vibration isolation system has the quasi-zero-rigidity characteristic on the six degrees of freedom, the all-order resonant frequency of the vibration isolation system is small, and the wide vibration isolation frequency range is achieved. The system has the advantages of being high in bearing capacity and low in resonant frequency, has the good restraint effect on low-frequency vibration, and is suitable for vibration isolation of flywheel systems and optical cameras in the spaceflight field and vibration isolation of equipment such as precision machine tools and precision measuring systems in the civil field.

Description

technical field [0001] The invention belongs to the technical field of passive vibration isolation, in particular to a six-degree-of-freedom quasi-zero-stiffness vibration isolation system based on a Stewart platform. Background technique [0002] With the advancement of aerospace technology, aerospace equipment is gradually developing in the direction of precision. Low-frequency vibration and micro-vibration in spacecraft will not only cause damage to precision instruments and equipment, but also affect the use of instruments and equipment (such as optical cameras). For precision equipment such as precision machine tools and precision measurement systems, low-frequency vibrations from the surrounding environment such as seismic waves will seriously affect the accuracy of the equipment. Micro-vibration and low-frequency vibration have become the focus and difficulty in the field of vibration control. Vibration isolation is an important means of vibration control. Researche...

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Application Information

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IPC IPC(8): F16F15/04
CPCF16F15/04
Inventor 郑宜生李青频张希农罗亚军张亚红谢石林
Owner XI AN JIAOTONG UNIV
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