Fuel injector development for low emission gas turbine combustors

Rao, KVL and Abbey, DK (1977) Fuel injector development for low emission gas turbine combustors. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    The ever increasing application of gasturbine engines for all transport, marine, and ground installations has caused some general concern over the of possible increase in the contamination/already over pollutant environment. Recent studies have revealed that the conventional combustor designs currently employed in gasturbines are, responsible for. the emissions of the pollutants, to a great extent. Among other things, the new design concepts have emphasized the importance of fuel injection techniques and its effects on the low emission combustor development. This paper deals13; with the design development and evaluation of 'air-atomisers' as a possible replacement for the conventional duplex atomiser employed hitherto, and compares their relative performance.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Gasturbine engines;Fuel injection techniques
    Subjects: AERONAUTICS > Aircraft Propulsion and Power
    Division/Department: Propulsion Division, Propulsion Division
    Depositing User: M/S ICAST NAL
    Date Deposited: 13 Nov 2006
    Last Modified: 24 May 2010 09:53
    URI: http://nal-ir.nal.res.in/id/eprint/3407

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