航天推进技术研究院主办
BAI Shaoqing,SUN Liang.Research of bursting pressure stability for membrane valve[J].Journal of Rocket Propulsion,2015,41(06):46-50.
膜片阀破裂压力稳定性研究
- Title:
- Research of bursting pressure stability for membrane valve
- 分类号:
- V434-34
- 文献标志码:
- A
- 摘要:
- 膜片破裂压力是膜片阀最关键的性能参数,由于影响因素较多,通常膜片破裂压力散差较大,不容易满足系统的使用要求。为提高膜片阀破裂压力稳定性,通过理论分析和应力计算,从原材料、加工、测量和试验系统等方面,对影响膜片破裂压力的各因素进行了梳理和分析,提出需进行着重控制的3个影响因素,包括材料抗拉强度、刻痕剩余厚度和试验系统,并通过了某姿控动力系统贮箱后膜片组件研制的验证。研究结果表明,通过对材料抗拉强度、刻痕剩余厚度和试验系统进行严格控制,能够有效提高膜片阀破裂压力稳定性,该方法可推广应用于同类产品的研制。
- Abstract:
- The membrane bursting pressure is the key performance parameter for a membrane valve, but there are many influencing factors to course great difference of membrane bursting pressure usually, which can't satisfy system's requirement easily. In order to improve the bursting pressure stability of the membrane valve, in this paper, all the influencing factors in the aspects of raw material, fabrication, measurement and testing system are collated and analysed by theoretical analyse and stress calculation. Based on this, three main factors which should be strictly controlled are listed. They are extension strength of material, rest thickness of nicks, and testing system. The control measures were used in membrane valve of a power system. The results show that the bursting pressure stability for membrane valve can be improved effectively by strict control to the three factors, and it can be used in research of other similar products.
参考文献/References:
[1]朱宁昌. 液体火箭发动机设计(下)[M]. 北京: 宇航出版社, 1994.
[2]宁建华. 光刻膜片在膜片阀中的应用[J]. 火箭推进, 2005, 31(1): 33-34.
NING Jianhua. Photoetching diaphragm in burst valve application[J]. Journal of Rocket Propulsion, 2005, 31(1): 33-34.
[3]龚志钰, 李章政. 材料力学[M]. 北京: 科学出版社, 1999.
[4]杨源泉. 阀门设计手册[M]. 北京: 机械工业出版社, 1992.
[5]陆培文, 高凤琴. 阀门设计计算手册[M]. 2版. 北京: 中国标准出版社, 2008.
[6]陆培文. 实用阀门设计手册[M]. 2版. 北京: 机械工业出版社, 2007.
[7]张清双, 尹玉杰, 李树勋, 等. 阀门和驱动装置技术手册[M]. 北京: 化学工业出版社, 2010.
[8]张旭虎, 唐斌, 李金山, 等. 航天器贮箱用钛制隔膜变形过程的数值模拟[J]. 宇航学报, 2010, 31(9): 2184-2188.
[9]罗胜彬, 宋春华, 韦兴平, 等. 非接触测量技术发展研究综述[J]. 机床与液压, 2013, 41(23): 150-153.
[10]张善群. 当代国外液体火箭发动机阀门研究与发展[J]. 航天推进与动力, 2004, 2(2): 1-8.
[11]余武江, 王海洲, 陈二锋, 等. 单向阀三维动态流场稳定性仿真研究[J]. 火箭推进, 2015, 41(1): 82-89.
YU Wujiang, WANG Haizhou, Chen Erfeng, et al. Research on three-dimensional dynamic flow stability of check valve[J]. Journal of Rocket Propulsion, 2015, 41(1): 82-89.
[12]陈展, 王可立, 郝伟涛. 空间流量调节阀的润滑[J]. 火箭推进, 2012, 38(4): 49-54.
CHEN Zhan, WANG Keli, HE Weitao. Lubrication scheme of flow control valve used in space[J]. Journal of Rocket Propulsion, 2012, 38(4): 49-54.
相似文献/References:
[1]宁建华.光刻膜片在膜片阀中的应用[J].火箭推进,2005,31(01):33.
Ning Jianhua.Photoetching diaphragm in burst valve application[J].Journal of Rocket Propulsion,2005,31(06):33.
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备注/Memo
收稿日期:2015-06-23;修回日期:2015-08-01 作者简介:白少卿(1983—),男,硕士,工程师,研究领域为火箭姿控发动机阀门