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Development of evaporation pressure-capacity control strategy for aircraft vapor cycle system

机译:飞机蒸汽循环系统蒸发压力控制策略的发展

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摘要

The conventional superheat-capacity control strategy fails to regulate the superheat steadily because of the violent oscillation at certain situations. This paper newly proposed an evaporation pressure-capacity control strategy to simulate the vapor cycle system by modulating the EEV opening to control the evaporation pressure rather than the superheat. A dual SISO expert PID controller with a feedforward compensator was employed to compare the control performance of the conventional superheat-capacity control strategy with the developed strategy. Experimental results showed both control strategies could regulate the capacity satisfactorily, but the new strategy could maintain the evaporation pressure stably. The conventional method failed to maintain the superheat around the target because of the violent oscillation observed. The developed strategy could regulate the aircraft vapor cycle system smoothly and reliably even under fast and widely changing environment. In addition, violent oscillation of superheat with big change width and quick frequency was observed and reported. (C) 2017 Elsevier Ltd and IIR. All rights reserved.
机译:由于某些情况下的剧烈振荡,传统的超热容量控制策略未能稳定地调节过热。本文新提出了蒸发压力控制策略来模拟蒸汽循环系统,通过调制EEV开口来控制蒸发压力而不是过热。采用具有前馈补偿器的双SISO专家PID控制器进行比较传统的超热能力控制策略与开发策略的控制性能。实验结果表明,控制策略均可令人满意地调节容量,但新策略可以稳定地保持蒸发压力。由于观察到的剧烈振荡,常规方法未能在目标周围保持过热。即使在快速且广泛改变环境下,开发策略也可以平稳可靠地调节飞机蒸汽循环系统。此外,观察到并报告了具有大变化宽度和快速频率的过热剧烈振荡。 (c)2017年Elsevier Ltd和IIR。版权所有。

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