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Vibration isolator

A vibration isolator and vibration isolation technology, applied in the direction of shock absorbers, shock absorbers, springs/shock absorbers, etc., can solve the problems affecting the imaging quality, deflection motion, angular displacement, etc. of the airborne photoelectric platform

Active Publication Date: 2019-06-14
CHINA AIRPLANT STRENGTH RES INST +1
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  • Description
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Problems solved by technology

[0002] The airborne optoelectronic platform is the main equipment for aerial reconnaissance. It is used to obtain high-quality images. The vibration isolator is designed to reduce the vibration transmitted from the airframe to the airborne optoelectronic platform. It is connected to the airborne optoelectronic platform through a mounting core. In the current vibration isolator, in addition to axial and radial movement, the mounting core can also undergo deflection motion, resulting in angular displacement. Studies have shown that the angular displacement of the mounting core seriously affects the imaging quality of the airborne optoelectronic platform

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Embodiment Construction

[0038] The application 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 related application, not to limit the application. In addition, it should be noted that, for ease of description, only parts relevant to the present application are shown in the drawings.

[0039] It should be noted that, in the case of no conflict, the embodiments in the present application and the features in the embodiments can be combined with each other. The present application will be described in detail below with reference to the accompanying drawings and embodiments.

[0040] It should be noted that in the description of this application, the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc. The terms of the indicated direction or positional relationship are based on the direction or positional ...

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Abstract

The invention belongs to the technical field of vibration isolation design and particularly relates to a vibration isolator. The vibration isolator comprises an installation core, an axial vibration isolation component and a radial vibration isolation component, wherein the axial vibration isolation component is provided with an axial vibration isolation cavity, the installation core is arranged to run through the axial vibration isolation cavity and is capable of moving in the axial motion relative to the axial vibration isolation component, and the axial vibration isolation component limitsthe installation core to move in the radial direction; the radial vibration isolation component is provided with a radial vibration isolation cavity and a vibration isolation through hole communicating with the radial vibration isolation cavity; the axial vibration isolation component is arranged inside the radial vibration isolation cavity, one end of the installation core stretches out of the vibration isolation through hole, and the installation core is in clearance fit with the vibration isolation through hole; and the axial vibration isolation component can move in the radial direction relative to the radial vibration isolation component, and the radial vibration isolation component limits the axial vibration isolation component to move in the axial direction.

Description

technical field [0001] The application belongs to the technical field of vibration isolation design, and in particular relates to a vibration isolator. Background technique [0002] The airborne optoelectronic platform is the main equipment for aerial reconnaissance. It is used to obtain high-quality images. The vibration isolator is designed to reduce the vibration transmitted from the airframe to the airborne optoelectronic platform. It is connected to the airborne optoelectronic platform through a mounting core. In the current vibration isolator, in addition to axial and radial movement, the mounting core can also undergo deflection motion and produce angular displacement. Studies have shown that the angular displacement of the mounting core seriously affects the imaging quality of the airborne optoelectronic platform. [0003] Therefore, it is desirable to have a technical solution to overcome or at least alleviate at least one of the above-mentioned drawbacks of the pri...

Claims

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Application Information

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IPC IPC(8): F16F7/00F16F3/087B64D47/00
Inventor 杨强董万元段宇星赵苗苗苏渤
Owner CHINA AIRPLANT STRENGTH RES INST