Μελέτη σχεδίασης δοκιμαστηρίου μικρού αεριοστροβίλου

Ντινόπουλος, Γρηγόριος; Ntinopoulos, Grigorios

dc.contributor.author	Ντινόπουλος, Γρηγόριος	el
dc.contributor.author	Ntinopoulos, Grigorios	en
dc.date.accessioned	2019-03-15T09:27:46Z
dc.date.available	2019-03-15T09:27:46Z
dc.date.issued	2019-03-15
dc.identifier.uri	https://dspace.lib.ntua.gr/xmlui/handle/123456789/48446
dc.identifier.uri	http://dx.doi.org/10.26240/heal.ntua.16507
dc.rights	Default License
dc.subject	Αεριοστρόβιλος	el
dc.subject	Μοντελοποιήση	el
dc.subject	Δοκιμαστήριο	el
dc.subject	Σχεδίαση	el
dc.subject	Μετρήσεις	el
dc.subject	Επεξεργασία	el
dc.title	Μελέτη σχεδίασης δοκιμαστηρίου μικρού αεριοστροβίλου	el
heal.type	bachelorThesis
heal.classification	Θερμικές Στροβιλομηχανές	el
heal.language	el
heal.access	free
heal.recordProvider	ntua	el
heal.publicationDate	2018-10-11
heal.abstract	Μελέτη για τη σχεδίαση δοκιμαστηρίου για τοποθέτηση και λειτουργία αεριοστροβίλου ισχύος. Διεξαγωγή και επεξεργασία μετρήσεων.	el
heal.abstract	The present diploma thesis studies the installation o f the engine PT6T - 6 to a test bed inside the facility of the Laboratory of Thermal Turbomachines of National Technical University of Athens. The diploma thesis is composed of two parts. The first concerns the model l ing of the engine and the second focuse s on the design of the test bed and the exploitation of the measurements. In first the engine is presented and details are given concerning its performance . Additionally the parameters of performance of all components are chosen for the desi gn point according to the manual of the engine and the measurements of the LTT . Next to the above, the performance of the engine is examined at the design point based on a simple thermodynamic model. Then the exact model of the engine is pro duced by the PROOSIS program and these results are compared to those of the simple thermodynamic model. Next there is a deep research in order to find the proper location of the design point to the maps of components, calculate the map scalars and test th e off - design performance of the engine . The results are compared to those of the LTT measurements, concerning engines with different serial number. Afterwards the performance of the engine in a test bed facility is described and the need of correction of the performance magnitudes to the reference conditions , because of the change of the enviro n ment al condition. In addition the performance of the engine is examined , concerning the corrected magnitudes, and also the capability of the engine ru nning in part loads is explained , without its components perform o n fearful map areas. The above is needed in order to limit the produced power of the engine to what it can be absorbed by the generator of the test bed of LTT . As far as the second part of the thesis concerns the base of the engine is designed, exactly the same as the one which is used to suppor t the engine in the helicopter. Also the tube system for the expansion of the exhaust gases to the en vironment outside the test ar ea is design ed, doing investigation for the exit area in order to achieve higher produced power. Additionally is mentioned the throttling system of the incoming flow, which the LTT already has, and a preliminary design of the adaptive parts for the i nlet of the engine and the connection of tubes of the throttling system to the inlet of the engine is taking place. According to the above , the ranges of magnitudes of the desired meas ured parameters for different throttling levels of the incomin g flow are examined. In addition the instruments of measurement , which can be used, are presented and their performance is briefly described, while the suitable instruments for operatio n according to the above ranges are chosen. Moreover the parameters, w hich can be measured on the engine , are presented as well as their positions, on which the measurements occurred. Finally, the processing of the data measurement is mentioned, meaning the exploitatio n of the measured performance paramet ers of the engine to calculate those, which are impossible to measure, due to non - existing measuring locations or due to ex treme conditions, as it happens in combustor exit .	en
heal.advisorName	Μαθιουδάκης, Κωνσταντίνος	el
heal.advisorName	Αρετάκης, Νικόλαος	el
heal.committeeMemberName	Μαθιουδάκης, Κωνσταντίνος	el
heal.committeeMemberName	Αρετάκης, Νικόλαος	el
heal.committeeMemberName	Γιαννάκογλου, Κυριάκος	el
heal.academicPublisher	Εθνικό Μετσόβιο Πολυτεχνείο. Σχολή Μηχανολόγων Μηχανικών. Τομέας Ρευστών. Εργαστήριο Θερμικών Στροβιλομηχανών	el
heal.academicPublisherID	ntua
heal.numberOfPages	150 σ.
heal.numberOfPages	150 σ.
heal.fullTextAvailability	true