توضیحات
Gas turbine development is constantly moving forward and for higher efficiency hotter turbine inlet temperature is required. Because of that, one o the largest design problems is to find efficient ways to cool the hot parts in the gas turbine. The task was to develop and evaluate new alternative cooling andmounting concepts for a transition duct in the latest gas turbine. Transitionduct is a hot part and has the task to guide the hot gas from the combustionchamber to the turbine inlet in a gas turbine. DOWNLOAD FILE
توضیحات تکمیلی
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