Zobrazeno 1 - 7
of 7
pro vyhledávání: '"Jiri Pecinka"'
The file attached to this record is the author's final peer reviewed version. The Publisher's final version can be found by following the DOI link. The effect of compressor fouling on the performance of a gas turbine has been the subject of several p
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::38ad92ade2d8335b2beceba3353f7980
http://hdl.handle.net/2086/14528
http://hdl.handle.net/2086/14528
Autor:
Ondrej Volny, Jiri Pecinka
Publikováno v:
2017 International Conference on Military Technologies (ICMT).
Electronic engine monitoring systems are used by both civilian and military aircraft operators as a significant support of the condition based maintenance systems. Presented paper describes monitoring system report and analysis of engine usage data o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::132dc6292b06064c41c638f80787eaa7
https://doi.org/10.1109/miltechs.2017.7988819
https://doi.org/10.1109/miltechs.2017.7988819
Publikováno v:
2017 International Conference on Military Technologies (ICMT).
There are various differential pressure methods to measure the air flow rate in a closed duct. These methods are defined by ISO standards, thus providing measurement with high accuracy. General practise for air flow rate measurements with gas turbine
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::554c86e83e06b701aeaeb28c7b8674a3
https://doi.org/10.1109/miltechs.2017.7988816
https://doi.org/10.1109/miltechs.2017.7988816
Autor:
Jakub Hnidka, Jiri Pecinka
Publikováno v:
2016 IEEE 14th International Symposium on Applied Machine Intelligence and Informatics (SAMI).
For a small gas turbine engine test cell newly developed and built at the University of Defence in Brno a system for automated measurement and engine test control was designed. The system is based on National Instruments Compact RIO hardware and LabV
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::968e73b0c4548c83ffd5e8b37f86d0e2
https://doi.org/10.1109/sami.2016.7422977
https://doi.org/10.1109/sami.2016.7422977
Publikováno v:
International Conference on Military Technologies (ICMT) 2015.
A project dealing with small gas turbine engine inlet total pressure distortion testing was solved at the University of Defence. Within this project a new device for creation and measurement of the total pressure inlet distortion was designed. In the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a58edbb247a6e591cfc6f95e0a6feab7
https://doi.org/10.1109/miltechs.2015.7153691
https://doi.org/10.1109/miltechs.2015.7153691
Publikováno v:
International Conference on Military Technologies (ICMT) 2015.
This paper describes the measurement of total pressure distortion of the TJ100 engine inlet and its influence on engine operation. The pressure distortion was generated by a specially designed distortion screen. Measurement was performed at different
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::74daaee34ba0e8f05dcd27416c2aaf36
https://doi.org/10.1109/miltechs.2015.7153692
https://doi.org/10.1109/miltechs.2015.7153692
Publikováno v:
Acta Polytechnica, Vol 57, Iss 1, Pp 22-31 (2017)
Total pressure distortion is one of the three basic flow distortions (total pressure, total temperature and swirl distortion) that might appear at the inlet of a gas turbine engine (GTE) during operation. Different numerical parameters are used for a
Externí odkaz:
https://doaj.org/article/0c4887a3505140f6b0c1e20ecfd21b46