External moving cable rotating system and application method thereof

Abstract

The invention provides an external moving cable rotating system. The system is used for accelerating an uplink spacecraft so as to enable the spacecraft to enter an orbit. After the uplink spacecraftis in butt joint with the tail end of a main rope of the external moving cable rotating system, a winch unwinds cables, so that the spacecraft moves outwards on one side and rotates around the centerof mass on the other hand, and mechanical work generated by the cable is converted into electric energy to be stored by the winch or converted into heat energy of a brake. According to the method, theline speed and the centrifugal acceleration of the spacecraft after butt joint can be reduced. In particular, a retarder is arranged in the winch. By means of the method, centrifugal force can be greatly reduced, and comfort is improved. The winch is provided with the retarder with the large heat absorption capacity, so that the self-rotating energy of the system after butt joint can be absorbed,and that the spacecraft is guaranteed to quickly move outwards. By utilizing the winch, the system has an uplink method, so that a high centrifugal force stage of an uplink process of the spacecraftis short, and the comfort is high.

Description

technical field [0001] The invention belongs to the field of space, and relates to a space launch, a launch vehicle, a space transfer cable system, a hoist, and a brake, and in particular to a space transfer cable system for a spacecraft to ascend and move outward. Background technique [0002] Multi-disc brake discs are commonly used brakes on large aircraft. The structure is multi-disc, which consists of a force transmission cylinder, a shaft, a hydraulic component, and multiple brake pads. The brake pads are divided into static discs and moving discs. Usually, each static disc is on the inner side and connected to the shaft, and the moving disc is on the outer side, and the outer edge of each moving disc is connected to the force transmission cylinder. When braking, the hydraulic components generate thrust, which presses the alternately installed moving discs and static discs to generate friction torque to brake the aircraft. When the brake is released, the compressed re...

AI Technical Summary

Problems solved by technology

The spacecraft needs to move inward slowly from 133.33m / s^2, limited by the power of the hoist and power supply, this process generally takes 15-30 minutes, which is very long

In addition, the power of the power supply and hoist is roughly constant. During the high centrifugal force stage, the winding speed of the hoist is very small, and the spacecraft moves inward very slowly. This makes the spacecraft spend a large proportion of time in the high centrifugal force stage.

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