Download or read book An Experimental Study of the Effect of a Pilot Flame on Technically Pre mixed Self excited Combustion Instabilities written by Bridget O'meara and published by . This book was released on 2015 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: Combustion instabilities are a problem facing the gas turbine industry in the operation of lean, pre-mixed combustors. Secondary flames known as "pilot flames" are a common passive control strategy for eliminating combustion instabilities in industrial gas turbines, but the underlying mechanisms responsible for the pilot flame's stabilizing effect are not well understood. This dissertation presents an experimental study of a pilot flame in a single-nozzle, swirl-stabilized, variable length atmospheric combustion test facility and the effect of the pilot on combustion instabilities. A variable length combustor tuned the acoustics of the system to excite instabilities over a range of operating conditions without a pilot flame. The inlet velocity was varied from 25 -- 50 m/s and the equivalence ratio was varied from 0.525 -- 0.65. This range of operating conditions was determined by the operating range of the combustion test facility. Stability at each operating condition and combustor length was characterized by measurements of pressure oscillations in the combustor. The effect of the pilot flame on the magnitude and frequency of combustor stability was then investigated. The mechanisms responsible for the pilot flame effect were studied using chemiluminescence flame images of both stable and unstable flames. Stable flame structure was investigated using stable flame images of CH* chemiluminescence emission. The effect of the pilot on stable flame metrics such as flame length, flame angle, and flame width was investigated. In addition, a new flame metric, flame base distance, was defined to characterize the effect of the pilot flame on stable flame anchoring of the flame base to the centerbody. The effect of the pilot flame on flame base anchoring was investigated because the improved stability with a pilot flame is usually attributed to improved flame anchoring through the recirculation of hot products from the pilot to the main flame base.Chemiluminescence images of unstable flames were used to identify several instability mechanisms and infer how these mechanisms are affected by the pilot flame. Flame images of cases in which the pilot flame did not eliminate the instability were investigated to understand why the pilot flame is not effective in certain cases. The phase of unstable pilot flame oscillations was investigated to determine how the phase of pilot flame oscillations may affect its ability to interfere with instability mechanisms in the main flame. A forced flame response study was conducted to determine the effect of inlet velocity oscillation amplitude on the pilot flame. The flame response was characterized by measurements of velocity oscillations in the injector and chemiluminescence intensity oscillations determined from flame images. As the forcing amplitude increases, the pilot flame's effect on the flame transfer function magnitude becomes weaker. Flame images show that as the forcing amplitude increases, the pilot flame oscillations increase, leading to an ineffective pilot. The results of the flame response portion of this study highlight the effect of instability amplitude on the ability of a pilot flame to eliminate a combustion instability.
Download or read book An Experimental Study of the Effect of a Pilot Flame on Combustion Instabilities written by Jihang Li and published by . This book was released on 2019 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: Lean-premixed gas turbines, due to their superior emission performance, have been widely used in the industry. However, lean-premixed combustion is susceptible to combustion instability, which has become a major concern in the design and operation of lean-premixed gas turbines. Passive secondary flames, also known as pilot flames, are commonly used for control of combustion instability. However, the underlying mechanism whereby a pilot flame suppresses combustion instability is not fully understood. This limits the improvement of pilot systems.This dissertation presents an experimental study on the effect of a pilot flame on combustion instabilities in an atmospheric, laboratory-scale, single-nozzle, swirl-stabilized, lean-premixed combustor. The pilot flame is a central jet flame injected from the centerbody, which can operate in either the technically-premixed or the fully-premixed modes, depending on the types of pilot injectors. Piezoelectric sensors are utilized to measure the pressure fluctuation and the velocity fluctuation. High speed CH* chemiluminescence techniques are used to measure the dynamics of the flame. The instability characteristics of the technically-premixed unpiloted flame are measured at varying combustor length. Four distinct instability modes with different frequencies are observed. A one-dimensional simulation is conducted to calculate the natural frequencies and mode shapes of the instabilities. The effect of varying the percent pilot of a technically-premixed pilot flame on the technically-premixed combustion instabilities in different modes is studied. Instability maps to the percent pilot and the overall equivalence ratio are presented and discussed. The instability boundaries in each instability map, which separates the unstable regions from the stable regions, are discussed in detail by analyzing the high-speed images and Rayleigh index images. The results show that the pilot flame affects the main flame dynamics primarily through enhancing flame attachment and flame oscillation in the inner shear layer. The effect of independently varying the pilot air, pilot fuel and pilot mixture flow rates on the technically-premixed combustion instabilities are studied by utilizing a modified pilot injector. The results show that the effect of the pilot flame on the combustion instability is primarily determined by the equivalence ratio, but not the mixture flow rate of the pilot flame. The results support the statement that pilot flames influence the main flame dynamics by heat recirculation and demonstrate that the effect of the pilot flame is determined by its ability to change the time-averaged recirculation zone temperature. The structures of the pilot flame are presented and discussed.Fully-premixed flame transfer functions under the influence of a premixed pilot flame are investigated. The flame transfer functions show distinct behaviors at low frequencies and high frequencies. At low frequencies, the pilot flame has a weak effect on the FTF gain and phase, while at high frequencies, increasing the percent pilot reduces the FTF gain and shifts the FTF phase. High-speed chemiluminescence images show the pilot flame enhances the fluctuation near the base of the flame, which enhances the destructive interference within the inner shear layer, reduces the FTF gain and shifts the FTF phase at high frequencies. By separating the flame transfer function into different regions, it was found that a pilot flame only influences the inner shear layer, but not the near-wall region and the outer recirculation zone.
Download or read book Experimental Study of Premixed Flames in a Taylor Couette Combustor written by Vahid Vaezi and published by . This book was released on 2000 with total page 310 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Stabilization and Dynamic of Premixed Swirling Flames written by Paul Palies and published by Academic Press. This book was released on 2020-07-03 with total page 402 pages. Available in PDF, EPUB and Kindle. Book excerpt: Stabilization and Dynamic of Premixed Swirling Flames: Prevaporized, Stratified, Partially, and Fully Premixed Regimes focuses on swirling flames in various premixed modes (stratified, partially, fully, prevaporized) for the combustor, and development and design of current and future swirl-stabilized combustion systems. This includes predicting capabilities, modeling of turbulent combustion, liquid fuel modeling, and a complete overview of stabilization of these flames in aeroengines. The book also discusses the effects of the operating envelope on upstream fresh gases and the subsequent impact of flame speed, combustion, and mixing, the theoretical framework for flame stabilization, and fully lean premixed injector design. Specific attention is paid to ground gas turbine applications, and a comprehensive review of stabilization mechanisms for premixed, partially-premixed, and stratified premixed flames. The last chapter covers the design of a fully premixed injector for future jet engine applications. Features a complete view of the challenges at the intersection of swirling flame combustors, their requirements, and the physics of fluids at work Addresses the challenges of turbulent combustion modeling with numerical simulations Includes the presentation of the very latest numerical results and analyses of flashback, lean blowout, and combustion instabilities Covers the design of a fully premixed injector for future jet engine applications
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1994 with total page 836 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Turbulent Premixed Flames written by Nedunchezhian Swaminathan and published by Cambridge University Press. This book was released on 2011-04-25 with total page 447 pages. Available in PDF, EPUB and Kindle. Book excerpt: A work on turbulent premixed combustion is important because of increased concern about the environmental impact of combustion and the search for new combustion concepts and technologies. An improved understanding of lean fuel turbulent premixed flames must play a central role in the fundamental science of these new concepts. Lean premixed flames have the potential to offer ultra-low emission levels, but they are notoriously susceptible to combustion oscillations. Thus, sophisticated control measures are inevitably required. The editors' intent is to set out the modeling aspects in the field of turbulent premixed combustion. Good progress has been made on this topic, and this cohesive volume contains contributions from international experts on various subtopics of the lean premixed flame problem.
Download or read book An Experimental Study of Flamelet Surfaces in Turbulent Combustion written by and published by . This book was released on 1990 with total page 27 pages. Available in PDF, EPUB and Kindle. Book excerpt: The major objective of the research reported was to study the properties of constant scalar property surfaces in turbulent reacting flows. Two dimensional image measurements were made in premixed turbulent flames and in jets and jet flames. Point-in-space, time-series measurements were also made, and the data used to study the properties of surface crossing statistics in jets and premixed flames. In addition, the hypothesis that, for the purpose of estimating the mean surface area per unit volume, surfaces in turbulent flow can be represented by fractal surfaces was used to develop models for the mean chemical reaction rate in premixed flames and for the source term in the equation for intermittency in free jets. Also a new method for making conditional velocity measurements in premixed flames was developed and applied to obtain unique data for velocity in these flames and to study jumps, across flamelets, of certain velocity statistics. Major findings for the flows and conditions studied include: (1) for the premixed case flamelet surfaces are fractal as are constant mixture fraction surfaces in jets and constant temperature surfaces in jet flames; (2) in jets the surface fractal dimension is between 2.3 to 2.4; (3) level crossing sets from time-series data are not simple fractal sets; (4) the idea of fractal bursts is introduced to help interpret the crossing sets; and (5) unique fully-conditional velocity data give a measure of velocity jumps across flamelets in premixed combustion.
Download or read book Dynamics of a Perfectly Premixed Jet Flame Exhibiting Self excited High frequency Transverse Thermoacoustic Instabilities written by Lucky Vo Tran and published by . This book was released on 2019 with total page 153 pages. Available in PDF, EPUB and Kindle. Book excerpt: This work is an investigation of the behavior of a premixed turbulent jet flame in a cylindrical dump combustor. The degeneracy of the simple configuration in this study lends itself for a detailed study of inherent mechanisms of a self-excited thermoacoustic instability in isolation from system coupling effects, enabling detailed numerical simulations to be carried out to supplement experimental findings. Tests were done at a nominal pressure of 8 bar and inlet temperature around 450 ̊C. Self-excited large eddy simulations were also carried out in OpenFOAM, using a b-[xi] flame-wrinkling model to model the combustion process. Eigenfrequency analysis in COMSOL was also done to support and explain the findings from both the numerical simulations and trends observed in the experiments. Measurements from high frequency pressure transducers were analyzed to determine the frequencies of the excited modes in the rig test and compared to the spectra from the LES simulation. The time-resolved fields from the LES simulation were phase-averaged to deduce the acoustic-flame interactions. Despite the (axis)symmetry in this configuration, the non-axisymmetric 1T and 1T1L modes were (simultaneously) excited. Two distinct behaviors are noted for the dynamic flame behavior. In the downstream region, the flame motion is well described by a bulk kinematic displacement as a result of the interaction of the flame front with the local acoustic perturbation. In the upstream region, near the combustor dump plane, large-scale wrinkles are observed in the flame front that have characteristics of a convective wave. The current findings provide additional evidence supporting and further establishing the theory of inherent acoustic-flame interactions as an excitation mechanism (distinct from acoustically-induced hydrodynamic oscillations) for high-frequency, transverse thermoacoustic instabilities.
Download or read book An Experimental Study of Forced Flame Response in Technically Premixed Flames in a Lean Premixed Gas Turbine Combustor written by Poravee Orawannukul and published by . This book was released on 2014 with total page 225 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA SP written by and published by . This book was released on 1962 with total page 156 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Experimental Investigation of the Premixed Combustion Instability written by B. I. Braynin and published by . This book was released on 1992 with total page 6 pages. Available in PDF, EPUB and Kindle. Book excerpt: The investigation of local and spatial flow field featured in the lean premixed propane/air flame with flashback happening continuously was made. LDV measurements were supplemented by pressure and flame position measurements, flow and flame front structure visualizations. Two flow duct configurations with different inlet/outlet conditions were investigated. (Author).
Download or read book Aeronautical Engineering written by and published by . This book was released on 1981 with total page 822 pages. Available in PDF, EPUB and Kindle. Book excerpt: A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).
Download or read book An Experimental Study of Flame Stabilization Mechanisms in Turbulent Non premixed Jet Flames Under Autoignitive Conditions written by Aravind Ramachandran and published by . This book was released on 2019 with total page 137 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A Theoretical and Experimental Study of Preferential diffusion stretch Interactions of Laminar Premixed Flames written by Oh Chae Kwon and published by . This book was released on 2000 with total page 536 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book International Aerospace Abstracts written by and published by . This book was released on 1999 with total page 1042 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Concord Clothing Gazette written by and published by . This book was released on 1878 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book An Experimental Study of Burner Stabilized Turbulent Flames in Premixed Reactants written by M. D. Fox and published by . This book was released on 1962 with total page 33 pages. Available in PDF, EPUB and Kindle. Book excerpt: Current concepts of flame propagation in premixed, turbulent gas streams are examined. This leads to the conclusion that the link between theory and experiment is entirely inadequate and incapable of improvement by existing methods. A series of new methods is implemented in an attempt to short-circuit the unprofitable chain of hypothesis and experiment which has hampered the identification of dubious steps. Methods of introducing uniform turbulence at relatively slow flows and improvements in light sources allow analysis of the approach flow by photographing particles illuminated by an interrupted Tyndall beam. Three new optical deflection methods are used to give a measure of the randomness of flame-front orientation, of the time-mean structure of the flame and of the instantaneous shape of the corrugated front. It is found that this corrugated surface propagates at a velocity considerably in excess of the normal laminar burning velocity. Quantitative analysis of the frequency of "peaks" and "valleys" on the surface, together with comparative data from the apex of laminar flames, suggests an explanation in terms of the effects of curvature and, secondarily, of the influence of small scale turbulence.
