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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Abstract
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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