The influence of the applied window function and sampling frequency on the assessment accuracy of the turbine engine in flight control condition based on its ground tests

Open Access

Issue		MATEC Web Conf. Volume 182, 2018 17^th International Conference Diagnostics of Machines and Vehicles


Article Number		01024
Number of page(s)		7
Section		Diagnostics of Machines and Vehicles
DOI		https://doi.org/10.1051/matecconf/201818201024
Published online		30 July 2018

W. Balicki, S. Szczeciń ski, Diagnostyka lotniczych silników turbinowych. Zastosowanie symulacyjnych modeli silników do optymalizacji zbioru parametrów diagnostycznych. Biblioteka Naukowa Instytutu Lotnictwa (2001) [Google Scholar]
W. A. Bodner, Automatyka silników lotniczych, Wyd. MON (1958). [Google Scholar]
K. Golak, Parametryczna ocena turbinowego silnika odrzutowego w locie na podstawie jego prób naziemnych (PhD thesis, 2016) [Google Scholar]
K. Golak, P. Lindstedt, R. Grą dzki, Studies of the jet engine control quality based on its response to the disturbance inflicted on the object, designated from its response to the set point inflicted to the controller, In: Safety and Reliability: Methodology and Applications - Proceedings of the European Safety and Reliability Conference, 137- 140 (2014) [CrossRef] [Google Scholar]
R. Grądzki, P. Lindstedt, K. Golak, Premises of evaluation of the technical object suitability with including the quality of its maintenance and operation, and their initial conditions. In: Safety and Reliability: Methodology and Applications - Proceedings of the European Safety and Reliability Conference, chapter 44; pp. 319 - 326 (2015) [Google Scholar]
K. Kurman, Teoria regulacji podstawy analiza projektowanie, WNT, (1975) [Google Scholar]
P. Lindstedt, K. Golak: Premises of parametrical assessment of turbojet engine in flight regulation condition during ground test, Acta Mechanica et Automatica, 6, no. 1 (2012) [Google Scholar]
Lindstedt P.: Possibilities of assessment of the potential of Aircraft Engines, Solid State Phenomena, 147-149/2009, Trans Tech Publications, (2009) [Google Scholar]
M. Orkisz, Simulation analysis of the influence of variation in some selected design and control parameters on the acceleration time of a turbojet engine, Engineering Transactions, 39, 3-4 (19911) [Google Scholar]
W. I. Pawlak, Computer simulation of transient processes in a turbojet engine, with special attention to amplitudes of thermal shocks in some selected fault models of operations, The Archive of Mechanical Engineering, LIV, no 3 (2007) [Google Scholar]
S. Szczeciń ski. Napę d samolotu 1-22 IRYDA, WPTiL 3/1995 (1995) [Google Scholar]
А. А. Шекяков, Автоматика авиационных и ракетных силовых установок. Ma шиност роение (1970) [Google Scholar]

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