Mitigating Combustion-driven Oscillation (Thermoacoustic Instability) in Industrial Combustors

ثبت نشده
چکیده

Combustion processes generate a band-limited pseudo-random sound that is often referred to as “combustion roar.” Although combustion roar sound is moderately intense but it is rather straight forward to quiet to a non-objectionable level by properly applying sound absorbing material around the burner area. In addition to the 'roar' sound which almost always exists in any confined combustion, on occasion a very intense, narrow-band (frequently single-frequency/tonal) noise is generated in a combustion chamber resulting in a high-amplitude, self-sustaining pressure oscillation. This phenomenon originates from a coupling between the flame‟s heat release dynamics, the combustor acoustics, as well as transient fluid dynamics in the combustor and is referred to by many names including, but not limited to, „combustiondriven oscillation‟, „combustion dynamic instability‟, and , „thermoacoustic instability‟. The excited acoustic oscillation causes large pressure fluctuations (high combustor noise levels), poor combustion, increased emissions and even catastrophic combustor failure (structural damage). „combustion-driven oscillation‟ has been reported in all types of combustion systems including industrial combustors (heaters, boilers, etc.), propulsion systems (rockets, afterburners) and gas turbine combustors.

برای دانلود متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

ثبت نام

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

منابع مشابه

Experiments , Identification , and Modeling

APRIL 2015 « IEEE CONTROL SYSTEMS MAGAZINE 57 Digital Object Identifier 10.1109/MCS.2014.2384971 Date of publication: 17 March 2015 T he Rijke tube [1] is a classic experiment that is relatively simple and inexpensive to build in a typical university laboratory. Despite its construction simplicity, it can serve to illustrate a wide variety of mathematical modeling, empirical identification, ver...

متن کامل

The Origin of Secondary Peaks with Active Control of Thermoacoustic Instability

This paper deals with the generation of new peaks in the pressure spectrum in controlled combustors in experimental investigations of active control of thermoacoustic instabilities. Typically, the reported experiments have demonstrated that the dominant thermoacoustic instability can be suppressed, but secondary peaks at different frequencies which were not excited in the uncontrolled combustor...

متن کامل

Towards a condition monitoring scheme for thermoacoustic instability detection and fuel blend performance classification using machine learning

The investigation and improvement in fuel performance and combustion is necessary in order to minimize emissions and operation costs in various engineering applications e.g. aerospace. Among these factors, nevertheless, ensuring safe operation is a priority: undesired phenomena, such as thermoacoustic instabilities, can have detrimental effects on jet engines, gas turbines and combustors, in ge...

متن کامل

Thermoacoustic Instability

Continuous combustion processes are prominently encountered in many applications related to power generation, heating and propulsion. Examples include domestic and industrial burners, steam and gas turbines, waste generators, and jet and ramjet engines. Continuous combustion processes exhibit a wide range of dynamics. Of these, conditions which promote coupling with the acoustic field and resul...

متن کامل

Reduced Order Modeling of Reacting Shear Flow

Thermoacoustic instability in premixed combustors occurs occasionally at multiple frequencies, especially in configurations where flames are stabilized on separating shear layers that form downstream of sudden expansions or bluff bodies. While some of these frequencies are related to the acoustic field, others appear to be related to shear flow instability phenomena. It is shown in this paper t...

متن کامل

ذخیره در منابع من


  با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید

برای دانلود متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

ثبت نام

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

عنوان ژورنال:

دوره   شماره 

صفحات  -

تاریخ انتشار 2011