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Manufacturing Influences on Pressure Losses of Channel Fed Holes
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Variations from manufacturing can influence the overall pressure drop and subsequent flow rates through supply holes in such applications as filmcooling, transpiration cooling, and impingement cooling that are supplied by ...
Strategies for High-Accuracy Measurements of Stage Efficiency for a Cooled Turbine
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Gas turbines are used in a broad range of aerospace and land-based applications from power generation to aviation, and their usage is projected to continue to grow. It is therefore critical to improve turbine efficiency ...
Use of Multiple Tracer Gases to Quantify Vane Trailing Edge Flow Into Turbine Rim Seals
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Overlapping features are commonly used as rim seals between stationary and rotating components in a turbine stage. These rim seals are used to prevent main gas path ingestion to the wheelspace cavity, which reduces the ...
Evaluating Thin-Film Thermocouple Performance on Additively Manufactured Turbine Airfoils
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: As gas turbine engine designs continue to target higher turbine entry temperatures for increased thermal efficiency, gas turbine manufacturers and operators require additional feedback from life-limited engine components. ...
Influence of Dilution and Effusion Flows in Generating Variable Inlet Profiles for a High-Pressure Turbine
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The elevated flow temperatures and pressures exiting gas turbine combustors affect the efficiency and durability of the high-pressure turbine stage. Understanding the effects that result from the upstream dilution and ...
Integration of Cooling Holes Into a Turbine Vane Made Using Additive Manufacturing
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Additive manufacturing (AM) has emerged as a method to prototype novel designs for turbine airfoil cooling with complex internal and film cooling geometries. Creating engine scale features with AM comes with challenges ...
Quantifying Part-to-Part Flow Variations and Cooling Effectiveness in Engine-Run Blades
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: As turbine inlet temperatures continue to increase for modern gas turbine engines, the lifing of hot section components operating in a range of environments is becoming increasingly challenging. Engine operations in harsh ...
Effects of Purge Jet Momentum on Sealing Effectiveness
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Driven by the need for higher cycle efficiencies, overall pressure ratios for gas turbine engines continue to be pushed higher thereby resulting in increasing gas temperatures. Secondary air, bled from the compressor, is ...
Effects of Purge Flow Configuration on Sealing Effectiveness in a Rotor–Stator Cavity
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Secondary air is bled from the compressor in a gas turbine engine to cool turbine components and seal the cavities between stages. Unsealed cavities can lead to hot gas ingestion, which can degrade critical components or, ...
Scaling Sealing Effectiveness in a Stator–Rotor Cavity for Differing Blade Spans
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: As engine development continues to advance toward increased efficiency and reduced fuel consumption, efficient use of compressor bypass cooling flow becomes increasingly important. In particular, optimal use of compressor ...