4.7 Article

Measurement of Transient Flash Evaporation Flow in Liquefied Gas Propulsion Using Dual-Plane ECT

出版社

IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC
DOI: 10.1109/TIM.2023.3272380

关键词

Capacitance; Propulsion; Capacitance measurement; Liquids; Temperature measurement; Velocity measurement; Permittivity measurement; Electrical capacitance tomography (ECT); flash evaporation; liquid holdup; mass flow rate; online flow measurement; tiny tube; transient flow

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This article presents the measurement of transient flash evaporation flow in liquefied gas propulsion (LGP) using a dual-plane electrical capacitance tomography (ECT) sensor. The study introduces a method for more accurate liquid holdup measurement, an adaptive cross correlation algorithm for stable velocity measurement, and compensation methods to account for temperature and pressure changes. Simulations and experiments validated the effectiveness of the proposed methods in deriving the mass flow rate of the two-phase flow. The research has important implications for online control of LGP and estimating the remaining life of small spacecrafts.
In this article, the transient flash evaporation flow in liquefied gas propulsion (LGP) was measured using a dual-plane electrical capacitance tomography (ECT) sensor. The novelty mainly stems from a selection method for more accurate liquid holdup measurement, a constrained adaptive cross correlation algorithm for more stable velocity, and compensation methods against the changes in temperature and pressure. By the selection method, interelectrodes capacitances that contribute less to the flow measurement, are removed from each data frame and more accurate liquid holdup is derived via image reconstruction. The adaptive cross correlation algorithm with a constraint on the correlation coefficient is adopted to alleviate the adverse effect of the fast changes of flow pattern on the velocity measurement. Then, the compensation methods are realized by correcting the deviations of phase density and permittivity caused by dramatic temperature and pressure changes. Simulations and experiments validated the effectiveness of the proposed methods to derive the mass flow rate of the two-phase flow via the measured liquid holdup, flow velocity, and estimated phase density. It is shown that the remaining mass of propellant in the storage tank calculated from the mass flow rate is in good agreement with the measured reference by the electronic balance, where the average relative errors under different initial pressures are less than 10%. To the best of our knowledge, this is the first time of transient flash evaporation flow measurement in a lab-built LGP device, which is promising to be applied for the effective online control to maximize the output impulse of LGP and estimate the remaining life of small spacecrafts.

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