Door-Triggering Mechanism for Large-Scale Rapid-Decompression Experiments

Author:

Zhang Lei1ORCID,Han Xiao1,Zhang Xinbin2,Yan Jihong2

Affiliation:

1. Beijing Institute of Spacecraft Environment Engineering, Beijing 100094, China

2. Laboratory for Space Environment and Physical Sciences, Harbin Institute of Technology, Harbin 150001, China

Abstract

For large-scale rapid-decompression experiments, a new door-triggering mechanism is proposed for a 750 mm diameter pressure relief channel. Quick opening of the door is realized by utilizing a spring-based release mechanism to instantly convert large amounts of elastic potential energy into kinetic energy. To counteract the significant inertial effect of the high-speed door on the chamber, a flywheel-based cushioning mechanism is designed to absorb the kinetic energy of the door after opening. This carefully designed mechanism consists of the closing mechanism, energy storage unit, locking/releasing mechanism, and cushioning mechanism. Kinetic models are established to analyze the dynamic properties. Simulation results reveal that it takes approximately 280 ms for the door to open from 0° to 90°. This work can provide insights for the development of large-scale rapid-decompression equipment in the future.

Funder

Science and Technology on Reliability and Environmental Engineering Laboratory of BISEE Foundation

Publisher

Hindawi Limited

Subject

Aerospace Engineering

Reference18 articles.

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