An improved damping and vibration isolation device for remote sensors based on bi-pod support

Abstract

The invention provides a remote sensor damping and vibration-isolation device improved based on a bi-pod supporting mode, and relates to the technical field of optical remote sensing vibration isolation. The remote sensor damping and vibration-isolation device comprises lower adapting supports, vibration isolation metal outer rods, vibration isolation metal inner rods and an upper adapting support, wherein the lower adapting supports are located in the same plane and horizontally fixed at the lower end of the remote sensor damping and vibration-isolation device; one end of each vibration isolation metal outer rod is fixedly connected with the corresponding lower adapting support, and the vibration isolation metal inner rods are fixedly mounted in the vibration isolation metal outer rods and extend out of the upper end faces, in the axial direction, of the vibration isolation metal outer rods; the ends, extending out of the vibration isolation metal outer rods, of the vibration isolation metal inner rods are fixedly connected; and the upper adapting support is fixedly mounted at the joint of the vibration isolation metal inner rods. The remote sensor damping and vibration-isolation device is high in vibration reduction efficiency and few in consumed system resource, functional separation of a rigid supporting structure and a damping and vibration reduction structure is achieved, the technical problem that the rigidity of a vibration isolation system is hard to maintain effectively is solved, and the temperature maintaining purpose of a working section of the damping and vibration isolation system is achieved.

Description

Technical field [0001] The invention relates to the technical field of optical remote sensing vibration isolation, in particular to a remote sensor damping vibration isolation device based on an improved bi-pod support method. Background technique [0002] The vibration environment of the space launch process has the characteristics of a large number of levels and a wide frequency domain. During the process of the aerospace precision optical remote sensor being transported to a predetermined orbit, the vibration and mechanical environment during the launch phase is quite harsh. The NASA research report (NASA TN D-6474, September, 1971.) pointed out that: about 45% of space equipment failures It is caused by vibration during launch. With the rapid development of optical remote sensing, the demand for high-resolution cameras has become increasingly prominent. The development trend of large aperture and long focal length makes the scale of optical remote sensors gradually evolve f...

AI Technical Summary

Problems solved by technology

However, the above systems are only suitable for light load vibration isolation, and all require control systems and energy to operate

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