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- W2130682008 abstract "Future generation gas turbine combustors for power production are expected to have the capability of operating on high hydrogen content fuels. To ensure the implementation of high hydrogen content (HHC) fuel in a power generation without negotiating with operational or emission advantages, the study of the flame stability regime and behavior of (HHC) fuel under gas turbine condition leads to the necessity of the development of an optically accessible high-pressure combustor. This paper represents a design of an optically high-pressure combustor facility based on 500 kW power and 15-bar pressure which is the representative pressure of real gas turbine. The combustion chamber is designed to accommodate multiple geometrical configurations including a non-swirl stabilized, swirl flow, and center-body stabilized swirl flow flame that will admit to see how the change of geometry influences the flame behavior and flashback propensity .Combustor is made of stainless steel chamber having three optically accessible windows and multiple instrumentation ports for a broad range of investigation techniques allowing for analysis of combustion and ignition. Finite element analysis has performed to get the wall thickness. The test chamber is also fitted with a variable area flow restrictor to control the desired pressure across the combustion chamber. cooling system is also included in the design to extract heat and avoid structural failure. The outer test section is equipped with copper coiling using cooling water as a driving fluid.The use of a variable throat area restrictor, multiple cooling systems, as well removable modular sections and optical access will allow the combustor to be compatible to work in a wide range of operations and have the flexibility operating with variable syngas compositions along with a variety of fuel to analyze the flame structure, flow field characterization using high speed particle image velocimetry (PIV), emission analysis and flashback propensity in high hydrogen content fuel under realistic gas turbine condition ." @default.
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- W2130682008 date "2012-07-30" @default.
- W2130682008 modified "2023-10-17" @default.
- W2130682008 title "Design and Development of an Optically Accessible High Pressure Combustor" @default.
- W2130682008 cites W1970824564 @default.
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- W2130682008 doi "https://doi.org/10.2514/6.2012-3784" @default.
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