Methodology for estimating the power of a turboprop engine as part of a parallel scheme hybrid power plant with a capacity of up to 800 kW

Abstract

The paper presents a methodology for estimating the power of a turboprop engine as part of a parallel scheme hybrid power plant with a capacity of up to 800 kW. The specific fuel consumption on the throttling coefficient rating is analytically calculated. The dependence of the mass-to-power ratio on the power is given. A demonstration calculation of the power as part of the GSU for the M-101T aircraft has been performed. Based on the methodology, recommendations are given for the use of hybrid power plant on aircraft with a take-off power plant capacity of up to 800 kW. doi 10.54708/19926502_2026_30111175