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Research of the High Altitude Control Strategy of the Piston Aero-engine Using Two-stage Turbocharger Coupled with single Supercharging System
ISSN: 0148-7191, e-ISSN: 2688-3627
Published December 19, 2019 by SAE International in United States
This content contains downloadable datasetsAnnotation ability available
Aiming at the high altitude operation problems for piston-type aero-engines and to improve the practical ceiling and high altitude dynamic performance, this thesis analyzes a controllable three-stage composite supercharging system, using a two-stage turbocharger coupled supercharger method. The GT-Power simulation model of a four-cylinder boxer engine was established, and the control strategy of variable flight height was obtained. The simulation research of engine performance from 0 to 20,000 meters above sea level has been carried out, which shows that the engine power is at the same level as the plain condition, and it could still maintain 85.28 percent of power even at the height of 20,000 meters, which meets the flight requirements of the aircraft.
CitationYao, Y., Shi, L., Zhang, Z., Xiao, M. et al., "Research of the High Altitude Control Strategy of the Piston Aero-engine Using Two-stage Turbocharger Coupled with single Supercharging System," SAE Technical Paper 2019-01-2211, 2019, https://doi.org/10.4271/2019-01-2211.
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