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Evaluation of Contaminant-Promoted Ignition in Scuba Equipment and Breathing-Gas Delivery Systems

机译:水肺设备和呼吸气体输送系统中促进污染促进点火的评价

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As the underwater diving industry continues to use greater concentrations of oxygen in its scuba systems, contaminant ignition becomes of greater concern. In this study, several scuba component assemblies from the Neutral Buoyancy Lab at NASA Johnson Space Center were tested after 1 year of use. They were pneumatically impacted with 50 percent nitrox gas at 20.7 MPa (3000 psi) to evaluate their ignition resistance then disassembled to assess their cleanliness. A follow-up study was then conducted on the ignition thresholds of hydrocarbon-based oil films in oxygen and nitrox environments to characterize the cleaning requirements for these systems. Stainless steel tubes were contaminated to known levels and tested by pneumatic impact. Ignition was determined with a photocell connected to the end of the contaminated tube. The results of the scuba component tests, cleanliness evaluation, and contaminant ignition study are discussed and compared for 50 percent nitrox and 100 percent oxygen environments.
机译:随着水下潜水行业继续在其水肺系统中使用更高浓度的氧气,污染物点火成为更大的关注。在这项研究中,在使用1年后,美国国家航空航天局安森空间中心的中性浮力实验室的几个水肺组件组件进行了测试。它们在20.7MPa(3000psi)下用50%的硝基克斯气体受到气动影响,以评估其点火电阻,然后拆卸以评估它们的清洁度。然后对氧气和硝基氧化物环境中的烃基油膜的点火阈值进行后续研究,以表征这些系统的清洁要求。不锈钢管被污染到已知水平并通过气动冲击测试。用连接到污染管末端的光电池确定点火。讨论了水肺组分试验,清洁度评估和污染点火研究的结果,并将其与50%的硝基克和100%的氧环境进行了比较。

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