Mechanical Engineering Commons^™

Tubular And Sector Heat Pipes With Interconnected Branches For Gas Turbine And/Or Compressor Cooling, Brian D. Reding Ii

FIU Electronic Theses and Dissertations

Designing turbines for either aerospace or power production is a daunting task for any heat transfer scientist or engineer. Turbine designers are continuously pursuing better ways to convert the stored chemical energy in the fuel into useful work with maximum efficiency. Based on thermodynamic principles, one way to improve thermal efficiency is to increase the turbine inlet pressure and temperature. Generally, the inlet temperature may exceed the capabilities of standard materials for safe and long-life operation of the turbine. Next generation propulsion systems, whether for new supersonic transport or for improving existing aviation transport, will require more aggressive cooling system …