A Formal Computer Based Design Environment for Aircraft Engine Control Systems

Gray, J.O.; Downes, C.G.

doi:10.1016/b978-0-08-035738-6.50074-4

Computer Aided Design in Control Systems 1988 1989

DOI: 10.1016/b978-0-08-035738-6.50074-4

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A Formal Computer Based Design Environment for Aircraft Engine Control Systems

J.O. Gray

C.G. Downes

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2020

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Numerical Investigation on the Dynamic Characteristics of an Adjustable Power Turbine Used in Environmental Control System

Zhang

et al. 2020

Complexity

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In this paper, the environmental control system of aircraft driven by a power turbine is further analyzed. Through the numerical simulation of the change of the bleed state under different flight conditions and the change of the flow field under different nozzle opening, the simulation results are verified by the experimental results, and the specific change rules of the power turbine output torque, power, and bleed flow are obtained. It is analyzed quantitatively that adjusting the adjustable nozzle ring can keep the output power stable, widen the flight envelope, and improve the stability of the environmental control system.

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Numerical Investigation on the Dynamic Characteristics of an Adjustable Power Turbine Used in Environmental Control System

Zhang

et al. 2020

Complexity

View full text Add to dashboard Cite

show abstract

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A Formal Computer Based Design Environment for Aircraft Engine Control Systems

Cited by 1 publication

References 4 publications

Numerical Investigation on the Dynamic Characteristics of an Adjustable Power Turbine Used in Environmental Control System

Numerical Investigation on the Dynamic Characteristics of an Adjustable Power Turbine Used in Environmental Control System

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