Control of starting the APU gas turbine engine at high altitudes

Authors

  • Artem Viktorovich Ivanov Joint Stock Company “Scientific Production Enterprise “Aerosila” (JSC “SPE “Aerosila”), Russia
  • Alena Vitalievna Afanasiev Joint Stock Company “Scientific Production Enterprise “Aerosila” (JSC “SPE “Aerosila”), Russia
  • Vadim Andreevich Shukalyuk Joint Stock Company “Scientific Production Enterprise “Aerosila” (JSC “SPE “Aerosila”), Russia

Keywords:

auxiliary gas turbine engine, automatic control system, fuel overflow, acceleration characteristic, fuel consumption, launch control of APU

Abstract

This article considers modern methods of auxiliary gas turbine engine start control, providing reliable ground and high-altitude gas turbine engine start, the main problems in the process of gas turbine engine start and methods for their solution.

Author Biographies

Artem Viktorovich Ivanov, Joint Stock Company “Scientific Production Enterprise “Aerosila” (JSC “SPE “Aerosila”), Russia

Head of the Calculation and Design Department at JSC “SPE “Aerosila”. Dipl. engineer, special-ty “Aircraft engines and power plants” (MATI, 2011). Cand. Sci., specialty “Heat, electrorocket engines and power plants of aircraft” (MAI, 2019)

Alena Vitalievna Afanasiev, Joint Stock Company “Scientific Production Enterprise “Aerosila” (JSC “SPE “Aerosila”), Russia

Head of the Team of the Mathematical Modeling and Calculation of Automatic Control Systems, the Calculation and Design Department at JSC “SPE “Aerosila”. Dipl. engineer, specialty “Ro-bots and robotic systems” (ASU, 2014)

Vadim Andreevich Shukalyuk, Joint Stock Company “Scientific Production Enterprise “Aerosila” (JSC “SPE “Aerosila”), Russia

design engineer of the Calculation and Design Department at JSC “SPE “Aerosila”. Dipl. master, specialty “Informatics and computer engineering” (MAI, 2019).

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Published

2023-05-04

Issue

Vol. 27 No. 1 (2023)

Section

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