Gas Turbine Engine Starting Applicated on TV2-117 Turboshaft

Authors

  • R. M. Catana Gas Turbine Experimentation Complex, RR&DI for Gas Turbines Comoti, Bucharest, Romania
  • G. Cican Aerospace Sciences, “Elie Carafoli” Department, Politehnica University of Bucharest, Bucharest, Romania
  • G. Dediu Aerospace Sciences, “Elie Carafoli” Department, Politehnica University of Bucharest, Bucharest, Romania
Volume: 7 | Issue: 5 | Pages: 2005-2009 | October 2017 | https://doi.org/10.48084/etasr.1315

Abstract

The paper presents the examination of two different types of engine starting configurations, applicated on TV2-117A turboshaft, running into the test bench. The first type of starting configuration is a normal starting, with the engine connected to the dynamometer which controls the free turbine speed by the dynamometer load. The second type of starting is a different one, the engine is not connected with the dynamometer, therefore it results that there is no control of the free turbine speed from the dynamometer, only from the engine but in particular conditions. To achieve the starting phase an instrumentation scheme is created, to control and monitor the engine, and a starting sequence with all the parameters, confirmations and commands that are involved into the starting phase. The engine starting is performed by the test bench operating system, composed of an acquisition system and a programmable controller, wherewith is running the starting sequence.

Keywords:

turboshaft, starting, instrumentation scheme, graphic interface, monitoring parameters

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References

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G. Cican, V. Stanciu, V. Silvestru, R. M. Catana, Fundamentals of Gas Turbine Engine Starting, Processes and Experiments, Printech, Bucharest, 2016

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How to Cite

[1]
Catana, R.M., Cican, G. and Dediu, G. 2017. Gas Turbine Engine Starting Applicated on TV2-117 Turboshaft. Engineering, Technology & Applied Science Research. 7, 5 (Oct. 2017), 2005–2009. DOI:https://doi.org/10.48084/etasr.1315.

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