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Nonuniform Clearance Effects on Windage Heating and Swirl Development in Straight-Through Labyrinth Seals
Publisher: ASCE
Abstract: Straight-through labyrinth seals are reliable noncontact seal structures widely used in aeroengines. Windage heating and swirl development of labyrinth seals are of great significance to the design of secondary air systems. ...
An Onboard Aeroengine Model-Tuning System
Publisher: American Society of Civil Engineers
Abstract: This study investigates an onboard aeroengine model (OBEM)-tuning system (OTS) based on a hybrid Kalman filter, which is mostly used to estimate the aeroengine performance. The OTS structure comprises two parts. One is an ...
Hybrid Diagnosis System for Aeroengine Sensor and Actuator Faults
Publisher: ASCE
Abstract: This paper presents a hybrid model-based fault diagnosis system to distinguish different types of faults and provide accurate fault information under complex fault situations. In the proposed system, a bank of hybrid fault ...
Robust Optimization of the Secondary Air System Axial Bearing Loads with the Labyrinth Clearance Uncertainty
Publisher: American Society of Civil Engineers
Abstract: The secondary air system of a gas turbine engine is a complex fluid network that is sensitive to geometric variations in the flow elements caused by manufacturing, assembly, and operating conditions. Geometric uncertainty ...
Heat Transfer Coefficients of Film Cooling on a Rotating Turbine Blade Model—Part I: Effect of Blowing Ratio
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Experimental investigations were performed to measure the local heat transfer coefficient (hg) distributions of film cooling over a flat blade under both stationary and rotating conditions. Film ...
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