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Dive into the research topics where Roointon Erach Pavri is active.

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Featured researches published by Roointon Erach Pavri.


Journal of Engineering for Gas Turbines and Power-transactions of The Asme | 2001

Reduced NOx diffusion flame combustors for industrial gas turbines

Alan S. Feitelberg; V. E. Tangirala; R. A. Elliott; Roointon Erach Pavri; Richard B. Schiefer

This paper describes reduced NO x diffusion flame combustors that have been developed for both simple cycle and regenerative cycle MS3002 and MS5002 gas turbines. Laboratory tests have shown that when firing with natural gas, without water or steam injection, NO x emissions from the new combustors are about 40 percent lower than NO x emissions from the standard combustors. CO emissions are virtually unchanged at base load, but increase at part load conditions. Commercial demonstration tests have confirmed the laboratory results. The standard combustors on both the MS3002 and MS5002 gas turbine are cylindrical cans, approximately 10.5 inches (27 cm) in diameter. A single fuel nozzle is centered at the inlet to each can and produces a swirl stabilized diffusion flame. The walls of the cans are louvered for cooling, and contain an array of mixing and dilution holes that provide the air needed to complete combustion and dilute the burned gas to the desired turbine inlet temperature. The MS3002 turbine is equipped with six combustor cans, while the MS5002 turbine is equipped with twelve combustors. The new, reduced NO x emissions combustors (referred to as a lean head end, or LHE, combustors) retain all of the key features of the conventional combustors; the only major difference is the arrangement of the mixing and dilution holes in the cylindrical combustor cans. By optimizing the number, diameter, and location of these holes, NO x emissions can be reduced considerably. Minor changes are also sometimes made to the combustor cap. The materials of construction, pressure drop, and fuel nozzle are all unchanged. The differences in NO x emissions between the standard and LHE combustors, as well as the variations in NO x emissions with firing temperature, are well correlated using turbulent flame length arguments. Details of this correlation are presented.


Journal of Engineering for Gas Turbines and Power-transactions of The Asme | 2000

Performance of a Reduced NOx Diffusion Flame Combustor for the MS5002 Gas Turbine

Alan S. Feitelberg; Michael D. Starkey; Richard B. Schiefer; Roointon Erach Pavri; Matt Bender; John L. Booth; Gordon R. Schmidt

This paper describes a reduced NO x diffusion flame combustor that has been developed for the MS5002 gas turbine. Laboratory tests have shown that when firing with natural gas, without water or steam injection, NO x emissions from the new combustor are about 40 percent lower than NO x emissions from the standard MS5002 combustor. CO emissions are virtually unchanged at base load, but increase at part load conditions. The laboratory results were confirmed in 1997 by a commercial demonstration test at a British Petroleum site in Prudhoe Bay, Alaska. The standard MS5002 gas turbine is equipped with a conventional, swirl stabilized diffusion flame combustion system. The twelve standard combustors in an MS5002 turbine are cylindrical cans, approximately 27 cm (10.5 in.) in diameter and 112 cm (44 in.) long. A small, annular, vortex generator surrounds the single fuel nozzle that is centered at the inlet to each can. The walls of the cans are louvered for cooling, and contain an array of mixing and dilution holes that provide the air needed to complete combustion and dilute the burned gas to the desired turbine inlet temperature. The new, reduced NO x emissions combustor (referred to as a lean head end, or LHE, combustor) retains all of the key features of the conventional combustor; the only significant difference is the arrangement of the mixing and dilution holes in the cylindrical combustor can. By optimizing the number; diameter, and location of these holes, NO x emissions were substantially reduced. The materials of construction, fuel nozzle, and total combustor air flow were unchanged. The differences in NO x emissions between the standard and LHE combustors, as well as the variations in NO x emissions with firing temperature, were well correlated using turbulent flame length arguments. Details of this correlation are also presented.


Volume 3: Coal, Biomass and Alternative Fuels; Combustion and Fuels; Oil and Gas Applications; Cycle Innovations | 1990

Unburned Hydrocarbon, Volatile Organic Compound, and Aldehyde Emissions From General Electric Heavy-Duty Gas Turbines

Roointon Erach Pavri; Richard A. Symonds

Field data clearly show that the emissions of UHC, VOC, (sometimes also called Reactive Organic Gases), and Aldehydes from GE heavy-duty gas turbines are very low. At loads exceeding 75% of base, these emissions are less than 2 ppm. In fact, stack emissions are often less than background concentration. Proper methods of measurement and quality assurance are necessary to detect and measure such low values. Allowance for background hydrocarbons should be made when guaranteeing UHC/VOC.Copyright


ASME Turbo Expo 2000: Power for Land, Sea, and Air | 2000

Reduced NOx Diffusion Flame Combustors for Industrial Gas Turbines

Alan S. Feitelberg; Venkat E. Tangirala; Richard A. Elliott; Roointon Erach Pavri; Richard B. Schiefer

This paper describes reduced NOx, diffusion flame combustors that have been developed for both simple cycle and regenerative cycle MS3002 and MS5002 gas turbines. Laboratory tests have shown that when firing with natural gas, without water or steam injection, NOx emissions from the new combustors are about 40% lower than NOx emissions from the standard combustors. CO emissions are virtually unchanged at base load, but increase at part load conditions. Commercial demonstration tests have confirmed the laboratory results.The standard combustors on both the MS3002 and MS5002 gas turbine are cylindrical cans, approximately 10.5 inches (27 cm) in diameter. A single fuel nozzle is centered at the inlet to each can and produces a swirl stabilized diffusion flame. The walls of the cans are louvered for cooling, and contain an array of mixing and dilution holes that provide the air needed to complete combustion and dilute the burned gas to the desired turbine inlet temperature. The MS3002 turbine is equipped with six combustor cans, while the MS5002 turbine is equipped with twelve combustors.The new, reduced NOx emissions combustors (referred to as a “lean head end”, or LHE, combustors) retain all of the key features of the conventional combustors; the only major difference is the arrangement of the mixing and dilution holes in the cylindrical combustor cans. By optimizing the number, diameter, and location of these holes, NOx emissions can be reduced considerably. Minor changes are also sometimes made to the combustor cap. The materials of construction, pressure drop, and fuel nozzle are all unchanged.The differences in NOx emissions between the standard and LHE combustors, as well as the variations in NOx emissions with firing temperature, are well correlated using turbulent flame length arguments. Details of this correlation are presented.Copyright


Archive | 2004

Method and apparatus for distributing fluid into a turbomachine

Richard Robert Trewin; Jason Paul Mortzheim; Edip Sevincer; Kevin Richard Kirtley; Roointon Erach Pavri; Xiaoyue Liu


Archive | 2002

Control of gas turbine combustion temperature by compressor bleed air

Richard Lee Nichols; Bruce G. Norman; Kevin Michael Elward; Roointon Erach Pavri; Benjamin Rush; Robert Edward Boettner; John P. Vandevelde


Archive | 1999

Optimized combustor of a gas turbine

Milton Bradford Hilt; John Francis Love; Roointon Erach Pavri; Richard B. Schiefer; Richard A. Symonds; Kevin Michael Elward; Robert Lee Hillis; Alan S. Feitelberg


Archive | 1998

Reduced emissions gas turbine combustor

Alan S. Feitelberg; Kevin Michael Elward; Robert Lee Hillis; Milton Bradford Hilt; John Francis Love; Roointon Erach Pavri; Richard B. Schiefer; Richard A. Symonds


Archive | 1999

LOW EMISSION GAS TURBINE COMBUSTION EQUIPMENT

Kevin Michael Elward; Alan S. Feitelberg; Robert Lee Hillis; Milton Bradford Hilt; John Francis Love; Roointon Erach Pavri; Richard B. Schiefer; Richard A. Symonds; アラン・エス・フェイテルバーグ; ケヴィン・マイケル・エルウォード; ジョン・フランシス・ラブ; ミルトン・ブラッドフォード・ヒルト; リチャード・アーサー・シモンズ; リチャード・ベンジャミン・シーファー; ローイントン・イラック・パブリ; ロバート・リー・ヒリズ


Archive | 2004

METHOD FOR DISPENSING FLUID IN TURBO-MACHINE AND DEVICE

Kevin Richard Kirtley; Xiaoyue Liu; Jason Paul Mortzheim; Roointon Erach Pavri; Edip Sevincer; Richard Robert Trewin; エディップ・セヴィンサー; ケビン・リチャード・カートレイ; ジェーソン・ポール・モリッツハイム; シャオユェ・リュー; リチャード・ロバート・トレウィン; ルイントン・エラク・パヴリ

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