TITLE

Gas turbine combustors drive emissions toward nil

AUTHOR(S)
Peltier, Robert
PUB. DATE
March 2003
SOURCE
Power;Mar2003, Vol. 147 Issue 2, p23
SOURCE TYPE
Trade Publication
DOC. TYPE
Article
ABSTRACT
Discusses control technologies to achieve lower NO[subx] emissions, as of March 2003. Background on the integration of dry low-emission combustion technology into product lines of gas turbine original equipment manufacturers during the 1980s; Factors that contribute to low emissions of NO[subx]; Details on emission reduction technologies such as surface-stabilized fuel injector.
ACCESSION #
9349970

 

Related Articles

  • GAS TURBINES FOR MARINE APPLICATIONS. EXERGY ANALYSIS FOR AN IMPROVED GAS TURBINE. FEIZA, MEMET; DANIELA, MITU // Analele Universitatii Maritime Constanta;2011, Vol. 12 Issue 15, p141 

    In marine applications, the gas turbine is usually driving the propellers of ships or ferry. The major advantage of gas turbines over conventional steam turbines or marine diesel main engines is their excellent power to weight ratio. However, the increasing price of fuel determined a lot of ship...

  • Development of Air Supply System for Gas Turbine Combustor Test Rig. Kamarudin, Norhaimi Izlan; Hanafi, Muhammad; Mantari, Asril Rajo; Jaafar, Mohammad Nazri Mohd // AIP Conference Proceedings;6/28/2010, Vol. 1225 Issue 1, p874 

    Complete combustion process occurs when the air and fuel burns at their stoichiometric ratio, which determines the appropriate amount of air needed to be supplied to the combustion chamber. Thus, designing an appropriate air supply system is important, especially for multi-fuel combustion. Each...

  • Dry, low NOx combustors adapt smoothly to GT10, GT35 ranges. Strand, Torsten // Offshore;Jul96, Vol. 56 Issue 7, p93 

    Reports on ABB Stal's development of gas turbine combustors for low flame temperature and very low nitrogen oxide production. Combustion methods; Operating experience.

  • NEW DESIGN OF IGNITON SYSTEM OF GAS TURBINE. SINGH, RAHUL; JAIN, AMBER; KUMAR, HARISH // Applied Mechanics & Materials;2014, Issue 592-594, p1662 

    This paper is all about a new type of ignition system for igniting the air-fuel mixture within combustion chamber of a gas turbine engine. In this system there will a separate ignition inside the primary combustion chamber which will be outside the main combustion chamber and responsible for...

  • Catalysts cuts turbine pollutants. Soast, Allen // ENR: Engineering News-Record;01/06/97, Vol. 238 Issue 1, p20 

    Focuses on the launching of a low-cost, flameless combustion system for gas turbines that is claimed to eliminate polluting emissions. Description of the catalyst used in the system; Features of the system; Background to the development of the system.

  • Energy Analysis of Pressurized Solid Oxide Fuel Cell Combined Power Turbine. Ayazi, M.; Karami, R.; Kamkari, B. // World Academy of Science, Engineering & Technology;2011, Issue 58, p988 

    Solid oxide fuel cells have been considered in the last years as one of the most promising technologies for very highefficiency electric energy generation from hydrogen or other hydrocarbons, both with simple fuel cell plants and with integrated gas turbine-fuel cell systems. In the present...

  • Bio-Fuel Atomizer Design for Micro-Gas Turbine. Abdul Halim, A. K.; Jaafar, M. N. M.; Ishak, M. S. A. // International Review of Mechanical Engineering;May2011, Vol. 5 Issue 4, p712 

    Recently, the increasing costs of fuel have become a major concern and always being debated. The increasing demand and decreasing in the fuel resources have contribute to the action of finding the alternative fuels. The research of micro gas turbine which is being powered by bio- fuel has become...

  • Experimental Investigations on Axial Temperature Profiles, Liner Wall Temperature Distribution and Exit Gas Temperature Distribution at Different Equivalence Ratios of A Tubular Type Gas Turbine Combustors. Kulshreshtha, Digvijay B.; Channiwala, S. A.; Dikshit, Saurabh B.; Chaudhari, Kamlesh V. // International Journal of Applied Engineering Research;2009, Vol. 4 Issue 3, p421 

    The development of the combustion chamber for 20kw gas turbine unit using kerosene type fuel has been undertaken keeping in view the basic requirements of a good combustion chamber, namely, high combustion efficiency, low pressure loss, smooth ignition, wide stability limits, size and shape...

  • Spray Combustion Dynamics under Thermoacoustic Oscillations. Chishty, Wajid A.; Lepera, Stephen D.; Vandsburger, Uri // World Academy of Science, Engineering & Technology;Mar2011, Issue 51, p1065 

    No abstract available.

Share

Read the Article

Courtesy of

Sorry, but this item is not currently available from your library.

Try another library?
Sign out of this library

Other Topics