Theory of Injector Deposits in Spray Combuster

碩士 === 國立成功大學 === 航空太空工程學系 === 85 === Gas turbine is used as a propulsion system of airplanes and as a group electric power generator. Frequently heavy oil has been for the economical reason in the generation of group based electric p...

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Bibliographic Details
Main Authors: Hao, Chin Chuan, 郝治銓
Other Authors: Chiu Hei Huang
Format: Others
Language:zh-TW
Online Access:http://ndltd.ncl.edu.tw/handle/74537309234881730440
Description
Summary:碩士 === 國立成功大學 === 航空太空工程學系 === 85 === Gas turbine is used as a propulsion system of airplanes and as a group electric power generator. Frequently heavy oil has been for the economical reason in the generation of group based electric power generation in the generation of ground based electric power generation. nevertheless the vanadium oxide contained in the heavy oil will harm the turbine blade and other parts exposed to the combustion products. The depositions are found to depend on the atomized condition, formation of liquid film, and its subsequent thermal decomposition of the fuel into carbon and hydrovarbon derivatives. Droplet size, velocity and activation energy, pre-exponential factor ect. are important parameters.