Session: 40-07: Turbine Secondary Flows and Interactions II
Paper Number: 153843
Aeromechanical Assessment of an Optical Probe Installed in a Two-Stage High-Pressure Gas Turbine
In recent years, the increasing demand for sustainable energy production has led to the adoption of innovative fuels in Gas Turbine (GT) plants. Among these sustainable fuels, hydrogen is regarded as one of the most promising options. GT combustors have pl ayed and continue to play a crucial role in research endeavors aimed at accommodating various fuels while minimizing alterations to turbine design. Consequently, changes in combustor shape and design philosophy necessitate a thorough investigation of High Pressure Turbine (HPT) operating conditions. In this regard, rigorous experimental procedures and probes must be developed for a detailed flow field characterization.
This paper numerically investigates the aeromechanical impact of an intrusive cylindrical probe installed near the Leading Edge (LE) of the second vane row of a commercial HPT module. The investigations are focused on the unsteady forcing acting on the pro be to avoid possible resonance issues, as well as on the influence of the probe itself on the stage flow field, as the probe diameter is comparable to the LE radius of the blades.
Computational Fluid Dynamics (CFD) has proven to be a powerful and reliable tool for turbomachinery applications over the years. Specifically, the URANS approach has demonstrated its ability to accurately predict the forces acting on turbine blade rows. Th erefore, both steady state and unsteady CFD methods are employed in this work to analyze the flow field modification related to the inclusion probe and finally the mechanical response of the probe is investigated using a Finite
Element Model (FEM).
Presenting Author: Innocenti Giacomo Baker Hughes
Presenting Author Biography: Giacomo Innocenti got the PhD from University of Florence
Authors:
Giacomo Innocenti Baker HughesLorenzo Miris Baker Hughes
Lorenzo Pinelli University of Florence
Giuseppe Del Vescovo Baker Hughes
Enrico Beghini Baker Hughes
Girolamo Tripoli Baker Hughes
Alberto Scotti Del Greco Baker Hughes
Michele Marconcini University of Florence
Aeromechanical Assessment of an Optical Probe Installed in a Two-Stage High-Pressure Gas Turbine
Paper Type
Technical Paper Publication