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高壓氫氣/甲烷混合氣體泄漏激波傳播特性研究

Study on propagation characteristics of shock waves during the leakage of a high-pressure hydrogen/methane mixture

  • 摘要: 在以傳統化石能源為主體到純氫氣大規模應用的過渡階段,氫氣/甲烷混合氣體作為氫能的重要載體,是氫能應用體系的重要組成部分,而高壓氫氣/甲烷混合氣體泄漏自燃威脅著氫能的大規模安全應用. 另一方面,在氫氣中加入少量甲烷可以在一定程度上降低其自燃傾向,從而提高氫能高壓儲存和運輸的安全性. 泄漏過程中激波造成的局部區域溫度急劇升高是引發氫氣/甲烷混合氣體自燃的直接原因,也是決定自燃特性的關鍵因素. 為此,本文聚焦高壓氫氣/甲烷混合氣體泄漏過程中激波演化過程和特性參數,基于改進高壓可燃氣體泄漏自燃實驗系統開展實驗研究. 實驗結果顯示:爆破片破裂后首先在泄漏管道內形成前沿激波,并且隨著激波的傳播,前沿激波與氫氣/甲烷混合氣體主射流距離越來越大. 與此同時,在矩形管道角落處產生反射激波,最終在泄漏管道內形成復雜的多維反射激波. 泄漏壓力增大,激波壓力和激波傳播速度明顯增大;摻甲烷比例增大,激波壓力和激波傳播速度明顯減小. 基于激波管流動理論,結合美國國家標準與技術研究院物性數據庫構建了高壓氫氣/甲烷混合氣體泄漏激波特性參數計算模型. 通過文獻數據和本文實驗數據對比分析,證實了優化后的激波特性參數計算模型在高壓氫氣/甲烷混合氣體泄漏激波特性參數計算中的適用性. 研究結果可為高壓氫氣/甲烷混合氣體泄漏自燃現象提供理論依據以及為相關實驗設計提供參考.

     

    Abstract: The transition from traditional fossil fuels to the widespread use of hydrogen energy marks a critical phase in energy evolution. Hydrogen/methane mixtures, serving as crucial carriers of hydrogen energy, play a key role in this process. However, the high risk of spontaneous ignition during high-pressure hydrogen leakage poses a significant safety challenge. Incorporating small amounts of methane into hydrogen can reduce this tendency, thereby enhancing the safety of high-pressure storage and transportation. Spontaneous ignition is triggered by abrupt localized temperature rises caused by shock waves during leakage; these shock waves are fundamental in determining the ignition characteristics of hydrogen/methane mixtures. Methane blending significantly changes shockwave behavior, affecting their propagation, and the resulting temperature and pressure changes influence spontaneous ignition; however, the underlying mechanisms of these effects remain unclear. This paper focuses on the evolution and characteristics of shock waves in high-pressure hydrogen/methane mixture leakage using an improved experimental system for spontaneous ignition research. Experimental results indicate that upon bursting disc rupture, a leading shock wave forms in the discharge tube, and as the shock wave propagates, the distance between the leading shock wave and the main jet of the hydrogen/methane mixture gradually increases. Simultaneously, the shape discontinuity between the circular rupture and the rectangular discharge tube creates reflected shock waves at the corners, developing into complex multidimensional shock waves reflected within the discharge tube. Leakage pressure and methane blending ratio significantly impact shock wave characteristics. Higher leakage pressures increase shock wave pressure and propagation velocity, whereas greater methane blending ratios reduce them. Using shock tube flow theory and the physical property database of National Institute of Standards and Technology, a calculation model was developed to predict shock wave parameters during hydrogen/methane leaks. A comparative analysis with literature and experimental data confirmed the applicability of the optimized calculation model for shock wave characteristic parameters in high-pressure hydrogen/methane mixture discharge scenarios. Spontaneous ignition reactions within the rectangular tube influence internal pressure dynamics. When burst pressure is below the critical threshold for ignition, during the leakage process of high-pressure H2/CH4 mixture, the pressure at sensor P2 exceeds that at P3 during leakage. Conversely, when the pressure is far above this threshold, spontaneous ignition occurs within the rectangular tube and develops into intense combustion near P3, subsequently elevating the pressure at P3, manifesting as P3 > P2. At pressures slightly above the critical threshold, the pressure relationship between P2 and P3 depends on the methane ratio. These findings provide a theoretical foundation for understanding spontaneous ignition phenomena during hydrogen/methane leakage and serve as a reference for future experimental designs.

     

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