Anti-shaking mechanism for rocket detector based on Steadicam system

Abstract

The invention relates to the technical field of shaking of a detector caused by rocket ignition, and discloses an anti-shaking mechanism for a rocket detector based on a Steadicam system. The anti-shaking mechanism comprises a shell, wherein a sliding rod is fixedly connected inside the shell; the sliding rod is sleeved with a damping arm; an elastic force adjusting button is movably connected tothe surface of the lower part of the damping arm; an objective table is fixedly connected to the right side of the damping arm; a sliding rail is fixedly arranged on the surface of the objective table; a supporting rod is fixedly connected to the lower part of the objective table; a sleeve is welded to the inside of the damping arm; a spring ring is sleeved with the sleeve; a pulley is fixedly connected to the right end of the spring ring through a connecting rod; the surface of the pulley is wound with a cable; a cable reel is movably connected to the right side of the pulley through the cable; an adjusting screw is wound with and connected to one end, away from the cable reel, of the cable; and the upper part of the adjusting screw is sleeved with an adjusting nut. The anti-shaking mechanism is based on the anti-shaking theory of a chicken head.

Description

technical field [0001] The invention relates to the technical field of detector shaking caused by rocket ignition, in particular to an anti-shake mechanism for a rocket detector based on a Steadicam system. Background technique [0002] With the advancement and development of science and technology, people have more and more detection and understanding of space. At present, the existing rocket launcher technology is relatively mature. With the rocket as a carrier, many detectors can be attached to explore space. As we all know When the rocket is launched, there will be huge shaking due to the injection of fuel. The detector is a precision machine, and the huge shaking will affect its working effect and damage the internal parts. Therefore, I consider using the camera’s stabilization device to eliminate the The phenomenon that the rocket ignites and the detector shakes. [0003] The comparative patent number is CN108490638A, the present invention discloses an optical anti-sh...

AI Technical Summary

Problems solved by technology

[0006] This patent can effectively cooperate with the Steadicam system to prevent shaking, but the driving force of its work depends on the motor, because the fuel carried by the rocket is obtained through precise calculation. If additional things are needed to consume fuel and energy, It will waste a lot of manpower and material resources to recalculate the energy consumed

[0007] Therefore, it is necessary to design a stable device that can adapt to different gravitational forces and is not disturbed by magnetic fields and external factors, so as to solve the problem of shaking the detector due to rocket ignition

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