Flame Transfer Function Measurement of a Hydrogen-Blended Sequential Combustor

Fuente: arXiv
Enregistré dans:
Détails bibliographiques
Auteurs principaux: Dharmaputra, Bayu, Nagpure, Pushkin, Impagnatiello, Matteo, Noiray, Nicolas
Format: Preprint
Publié: 2024
Sujets:
Accès en ligne:
Tags: Ajouter un tag
Pas de tags, Soyez le premier à ajouter un tag!
_version_ 1866916576611008512
author Dharmaputra, Bayu
Nagpure, Pushkin
Impagnatiello, Matteo
Noiray, Nicolas
author_facet Dharmaputra, Bayu
Nagpure, Pushkin
Impagnatiello, Matteo
Noiray, Nicolas
contents The flame transfer function (FTF) relates acoustic perturbations and the coherent heat release rate response. This frequency-dependent function governs the thermoacoustic stability of a combustor. The FTF measurement is therefore of great interest for predicting the stability of the a practical combustor connected to the engine's compressor and turbine. In this study, the flame transfer function of the sequential flame of an atmospheric constant pressure sequential combustor (CPSC) is experimentally measured. The thermal power of both the first- and second-stage flames is kept constant and their ratio is fixed at 1:1. The effects of hydrogen blending in the first and second stage fuel mixture on the sequential FTF are analyzed. The FTF of the sequential flame is fitted with a distributed time delay (DTD) model with two pulses. The trends of the model parameters obtained are consistent with the chemiluminescence OH* of the sequential flame.
format Preprint
id arxiv_https___arxiv_org_abs_2408_03357
institution arXiv
publishDate 2024
record_format arxiv
spellingShingle Flame Transfer Function Measurement of a Hydrogen-Blended Sequential Combustor
Dharmaputra, Bayu
Nagpure, Pushkin
Impagnatiello, Matteo
Noiray, Nicolas
Fluid Dynamics
Applied Physics
The flame transfer function (FTF) relates acoustic perturbations and the coherent heat release rate response. This frequency-dependent function governs the thermoacoustic stability of a combustor. The FTF measurement is therefore of great interest for predicting the stability of the a practical combustor connected to the engine's compressor and turbine. In this study, the flame transfer function of the sequential flame of an atmospheric constant pressure sequential combustor (CPSC) is experimentally measured. The thermal power of both the first- and second-stage flames is kept constant and their ratio is fixed at 1:1. The effects of hydrogen blending in the first and second stage fuel mixture on the sequential FTF are analyzed. The FTF of the sequential flame is fitted with a distributed time delay (DTD) model with two pulses. The trends of the model parameters obtained are consistent with the chemiluminescence OH* of the sequential flame.
title Flame Transfer Function Measurement of a Hydrogen-Blended Sequential Combustor
topic Fluid Dynamics
Applied Physics
url https://arxiv.org/abs/2408.03357