@inproceedings{f9a5d7b873b544d3a81feb83f10450dd,
title = "Design of a SMA-based hold down and release actuator for high preload",
abstract = "A SMA-based hold down and release actuator for high preload is designed and validated. The realization of the release and resetting function depends upon the performance of the trigger unit, which is mainly composed of the SMA wire and the bias spring. According to the force and movement analysis of the trigger unit, the requirements for the trigger force and trigger displacement are required. On the basis, the geometry parameters of the SMA wire and the bias spring are obtained. At last, the function validation tests are conducted on the prototype.",
author = "Dawei Huang and Xiaoyong Zhang and Xiaojun Yan and Mingjing Qi and Hui Zhang",
note = "Publisher Copyright: {\textcopyright} 2018 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.; 54th AIAA/SAE/ASEE Joint Propulsion Conference, 2018 ; Conference date: 09-07-2018 Through 11-07-2018",
year = "2018",
doi = "10.2514/6.2018-4803",
language = "英语",
isbn = "9781624105708",
series = "2018 Joint Propulsion Conference",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "2018 Joint Propulsion Conference",
}