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一种超高声速飞行器部件分离风洞实验同步起爆装置
苑朝凯; 王春; 姜宗林
2019-01-04
Rights Holder中国科学院力学研究所
Abstract本发明公开了一种高超声速飞行器部件分离风洞实验同步起爆装置,包括:同步触发单元(1)、起爆控制单元(2)、恒流单元(3)。本发明解决了起爆过程与风洞有效实验时间同步问题、起爆过程监测等问题,避免了风洞辅助大功率设备的强电磁干扰诱发的误起爆问题,为风洞验证飞行器部件分离方案可行性提供了实验基础,使部件分离验证方案不再局限于实际飞行实验,降低了飞行器研制成本和周期。
Application Date2017-02-14
Patent NumberZL201710077319.8
Language中文
Country中国
Agency北京和信华成知识产权代理事务所
Document Type专利
Identifierhttp://dspace.imech.ac.cn/handle/311007/80895
Collection高温气体动力学国家重点实验室
Affiliation中国科学院力学研究所
Recommended Citation
GB/T 7714
苑朝凯,王春,姜宗林. 一种超高声速飞行器部件分离风洞实验同步起爆装置. ZL201710077319.8[P]. 2019-01-04.
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