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电磁触发锁紧释放机构设计与试验研究

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近年来发展的以形状记忆合金驱动、热刀为代表的空间应用低冲击锁紧释放装置,解决了火工品解锁器的冲击和污染等问题,但同时引入了解锁同步性差、温度环境适应性不足等问题.为解决上述问题,提出了一种电磁触发锁紧释放机构设计方案,完成了工程样机的研制,并进行了锁紧力加载、最短加电时间、解锁同步性、解锁冲击及真空热环境下解锁等功能性测试.结果表明:加载10 000 N锁紧力工况下,最短加电时长为0.05 s时可以正常解锁,2 000 Hz范围内解锁冲击加速度不大于100g(g为重力加速度),可以兼容0.104 s星载火工品电源,多台解锁器解锁同步性小于0.02 s,热真空过程中低温为-50℃、常温为28 ℃和高温为90 ℃这3种工况下均可以正常解锁.该产品质量轻、尺寸小、解锁响应快、可重复使用、解锁冲击小、解锁同步性和环境适应性好,具有很大的工程应用潜力.
Design and experimental research of electromagnetic hold down and release mechanism
In recent years,with the development of space-application low shock Hold Down and Release Mechanism(HDRM)represented by the shape memory alloy and the thermal knife,such problems as impact and pollution caused by pyro-technics have been solved.However,such setbacks as poor unlocking synchronization and inadequate adaptability to temperature cannot be ignored.In this article,an electromagnetic triggered HDRM is proposed.The prototype is subject to the functional tests,including the load of the locking force,the shortest charging time,the unlock synchronization,the unlock shock,the un-lock in the thermal vacuum environment,and so on.The results show that the shortest charging time under the working condition of 10 000 N locking force is 0.05 s;the release impact acceleration is less than 100g within 2 000 Hz;the 0.104 s pyro actuator power can be compatible;the synchronization of multiple unlocking devices is less than 0.02 s.They be unlocked normally under three working conditions:the low temperature-50 ℃,the normal temperature 28 ℃,and the high temperature 90 ℃ during the thermal vacuum process.The scheme,with the advantages of light weight,compact size,fast response to unlock,ability of recy-cling,minor unlock impact,desirable unlock synchronization and good environmental adaptability,can be widely applied in the engineering field.

space applicationlow shockelectromagneticsegmented nuttest and experiment

黄龙、李旭鹏、张文会

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中国空间技术研究院西安分院,陕西西安 710199

空间应用 低冲击 电磁触发 分瓣螺母 测试试验

2024

机械设计
中国机械工程学会,天津市机械工程学会,天津市机电工业科技信息研究所

机械设计

CSTPCD北大核心
影响因子:0.638
ISSN:1001-2354
年,卷(期):2024.41(4)
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