Proračun performansi turbovratilnog motora General Electric T700

undergraduate thesis

• Title (english): Performance calculation of General Electric T700 Turboshaft Engine
• Author: Matej Ravlić
• Mentor: Anita Domitrović (mentor)
• Committee member: Karolina Krajček Nikolić (predsjednik povjerenstva)
• Committee member: David Gerhardinger (član povjerenstva)
• Committee member: Davor Franjković (član povjerenstva)
• Granter: University of Zagreb; Faculty of Transport and Traffic Sciences; (Division of Aeronautics); (Department of Aeronautics); Zagreb
• Defense date and country: 2022-09-19, Croatia
• Scientific / art field, discipline and subdiscipline: TECHNICAL SCIENCES; Traffic and Transport Technology; Air Traffic

Abstract

U ovom završnom radu prikazana je kinematska shema, opisan rad, konstrukcija te proračuni performansa turbovratilnog motora General Electric T700 kakav se ugrađuje na helikopter američke proizvodnje Sikorsky UH-60 Black Hawk. Prikazan je termodinamički proračun i idealni ciklus rada. Također su određene performanse u tri režima rada. Za bolje razumijevanje određenih komponenti motora ubačene su skice te sheme određenih sustava.

Abstract (english)

The aim of this thesis is to present kinematic scheme, describe operation, construction and to calculate performance of General Electric T700 turboshaft engine which is powerplant for american Sikorsky UH-60 Black Hawk helicopter. This thesis covers thermodynamic equations, calculations and the ideal thermodynamic cycle. Three main performance regimes od the turboshaft motor will also be defined. For better understanding of certain components there are sketches and schemes of certain systems.

• Keywords: turbovratilni motor; kinematska shema; General Electric T700
• Keywords (english): turboshaft engine; kinematic scheme; General Electric T700
• Language: croatian
• URN:NBN: urn:nbn:hr:119:106627
• Study programme: Title: Aeronautics; Study programme type: university; Study level: undergraduate; Academic / professional title: sveučilišni/a prvostupnik/prvostupnica (baccalaureus/baccalaurea) inženjer/inženjerka aeronautike (sveučilišni/a prvostupnik/prvostupnica (baccalaureus/baccalaurea) inženjer/inženjerka aeronautike)
• Type of resource: Text
• File origin: Born digital
• Access conditions: Open access
• Created on: 2022-10-07 13:44:58