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Real-Time Optical Fuel-to-Air Ratio Sensor for Gas Turbine CombustorsThe measurement of the temporal distribution of fuel in gas turbine combustors is important in considering pollution, combustion efficiency and combustor dynamics and acoustics. Much of the previous work in measuring fuel distributions in gas turbine combustors has focused on the spatial aspect of the distribution. The temporal aspect however, has often been overlooked, even though it is just as important. In part, this is due to the challenges of applying real-time diagnostic techniques in a high pressure and high temperature environment. A simple and low-cost instrument that non-intrusively measures the real-time fuel-to-air ratio (FAR) in a gas turbine combustor has been developed. The device uses a dual wavelength laser absorption technique to measure the concentration of most hydrocarbon fuels such as jet fuel, methane, propane, etc. The device can be configured to use fiber optics to measure the local FAR inside a high pressure test rig without the need for windows. Alternatively, the device can readily be used in test rigs that have existing windows without modifications. An initial application of this instrument was to obtain time-resolved measurements of the FAR in the premixer of a lean premixed prevaporized (LPP) combustor at inlet air pressures and temperatures as high as 17 atm at 800 K, with liquid JP-8 as the fuel. Results will be presented that quantitatively show the transient nature of the local FAR inside a LPP gas turbine combustor at actual operating conditions. The high speed (kHz) time resolution of this device, combined with a rugged fiber optic delivery system, should enable the realization of a flight capable active-feedback and control system for the abatement of noise and pollutant emissions in the future. Other applications that require an in-situ and time-resolved measurement of fuel vapor concentrations should also find this device to be of use.
Document ID
19990040657
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Nguyen, Quang-Viet (NASA Glenn Research Center Cleveland, OH United States)
Mongia, Rajiv K. (California Univ. Berkeley, CA United States)
Dibble, Robert W. (California Univ. Berkeley, CA United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1999
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-11566
NASA/TM-1999-209041
NAS 1.15:209041
Funding Number(s)
PROJECT: RTOP 523-36-13
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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