Influence of the Slot Fillet and Vane Root Fillet on the Turbine Vane Endwall Cooling Performance
نویسندگان
چکیده
Due to machining techniques and dust deposition, gas turbine upstream slots vane roots are always filleted, significantly affecting the cooling performance of endwall. The effects slot fillet root on endwall were investigated by solving three-dimensional Reynolds-averaged Navier–Stokes (RANS) equations with shear stress transport (SST) k–ω turbulence model. results indicate that velocity distribution coolant is effectively changed introducing fillets. Among four cases, largest adiabatic effectiveness was obtained for case two similar fillets, a 42% increase in effective area compared traditional slot. At MFR = 0.75%, horseshoe vortex weakened introduction small radius, 53% baseline. However, large radius makes boundary layer flow separately prematurely, decreasing performance. lateral coverage jet from filmhole embedded greatly enhanced increasing radius. streamwise decreased thermodynamic loss increased.
منابع مشابه
Flow and Thermal Performance of an Airfoil-endwall Fillet for a Gas Turbine Nozzle Guide Vane
Gas turbine engines are used in a variety of power generation applications, including providing thrust for the F-35 Lightning II Joint Strike Fighter, turning electrical generators in combined-cycle power plants, and powering the M1 Abrams Main Battle Tank. In the high-temperature region of the turbine section, a complex vortical (swirling) flow present near the junction of a turbine airfoil an...
متن کاملFlow and Thermal Performance of a Leading Edge Endwall-airfoil Fillet for a Gas Turbine Nozzle Guide Vane
Gas turbine engines have a high power-to-weight ratio, making them ideal for generation of aircraft thrust, and can have excellent electrical power generation efficiencies when used in a combined cycle power plant. A complex vortical flow at the junction of the nozzle guide vane airfoil and its casing (endwall) in the turbine section tends to decrease aerodynamic efficiency and increase metal t...
متن کاملFlow and Thermal Performance of a Gas Turbine Nozzle Guide Vane with a Leading Edge Fillet
Complex three-dimensional vortex flows develop at the junction of a gas turbine airfoil and its casing (endwall). These flows increase the transfer of heat from the combustion gases to the metal parts and contribute to reduced aerodynamic efficiency. Past studies have shown that the use of a large fillet at the airfoil-endwall junction can reduce or eliminate the endwall vortex flow pattern. To...
متن کاملEndwall Heat Transfer and Shear Stress for a Nozzle Guide Vane with Fillets and a Leakage Interface
Increasing the combustion temperatures in a gas turbine engine to achieve higher efficiency and power output also results in high heat loads to turbine components downstream of the combustor. The challenge of adequately cooling the nozzle guide vane directly downstream of the combustor is compounded by a complex vortical secondary flow at the junction of the endwall and the airfoil. This flow t...
متن کاملThe Influence of Step and Fillet Shape on Nozzle Endwall Heat Transfer
Abstract—There is a gap at combustor-turbine interface where leakage flow comes out to prevent hot gas ingestion into the gas turbine nozzle platform. The leakage flow protects the nozzle endwall surface from the hot gas coming from combustor exit. For controlling flow’s stream, the gap’s geometry is transformed by changing fillet radius size. During the operation, step configuration is occurre...
متن کاملذخیره در منابع من
با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید
ژورنال
عنوان ژورنال: Machines
سال: 2023
ISSN: ['2075-1702']
DOI: https://doi.org/10.3390/machines11070729