3 edition of Real-time optical fuel-to-air ratio sensor for gas turbine combustors found in the catalog.
Real-time optical fuel-to-air ratio sensor for gas turbine combustors
by National Aeronautics and Space Administration, Glenn Research Center, National Technical Information Service, distributor in [Cleveland, Ohio], [Springfield, Va
Written in English
|Other titles||Real time optical fuel to air ratio sensor for gas turbine combustors.|
|Statement||Quang-Viet Nguyen, Rajiv K. Mongia and Robert W. Dibble.|
|Series||NASA/TM -- 1999-209041., NASA technical memorandum -- 209041.|
|Contributions||Mongia, Rajiv K., Dibble, Robert W., NASA Glenn Research Center.|
|The Physical Object|
ISMA PAPERS Acoustic testing (Session AT) Bayesian focusing: a unified approach to inverse acoustic radiation fixdemocracynow.com, University of Technology of Compiègne, France The localisation and reconstruction of acoustical sources from data supplied by an array of microphones is an inverse problem that has been addressed by various approaches such as beamforming, near-field acoustical . Fuel control for gas turbine with continuous pilot flame. DOEpatents. Swick, Robert M. An improved fuel control for a gas turbine engine having a continuous pilot flam.
Figure shows the effects of turbine inlet temperature, cycle pressure ratio, and bypass ratio on thrust and specific fuel consumption for a high bypass ratio turbofan. Thrust is normalized by core airflow, as opposed to total inlet airflow, to restrict the comparison to a constant gas generator size. In gas turbine combustors, the problem appears to arise from a threefold interaction of combustion, system acoustics, and swirl flow aerodynamics. The principal of acoustic streaming is well known in the areas of rockets and ram jets, but its effect has not been considered to the same extent with swirl combustion systems.
Jun 01, · Closed loop air cooling system for combustion turbines. DOEpatents. Huber, David John; Briesch, Michael Scot. Convective cooling of turbine hot parts using a closed lo. Coatings for High-Temperature Structural Materials - Free download as PDF File .pdf), Text File .txt) or read online for free. This report assesses coatings materials and processes for gas-turbine blades and vanes; determines potential applications of coatings in high-temperature environments; identifies needs for improved coatings for performance enhancements, design considerations, and.
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Real-Time Optical Fuel-to-Air Ratio Sensor for Gas Turbine Combustors Quang-Viet Nguyen Glenn Research Center, Cleveland, Ohio Rajiv K. Mongia and Robert W. Dibble University of California at Berkeley, Berkeley, California Prepared for the International Symposium on Industrial and Environmental Monitors and Biosensors.
Real-Time Optical Fuel-to-Air Ratio Sensor for Gas Turbine Combustors Article (PDF Available) in Proceedings of SPIE - The International Society for Optical Engineering · April with Figure 2 shows the schematic of the real-time TDL sensor for equivalence ratio in gas turbine combustors.
The fiber-coupled DFB laser (NEL NLK1U5FAAA) operating near nm is mounted in a commercial laser mount (ILX Lightwave LDM) and maintained at constant temperature (ILX Lightwave LDM).Cited by: Get this from a library.
Real-time optical fuel-to-air ratio sensor for gas turbine combustors. [Quang-Viet Nguyen; Rajiv K Mongia; Robert W Dibble; NASA Glenn Research Center.].
Time-Resolved Optical Measurements of Fuel-Air Mixedness in Windowless High Speed Research Combustors Fuel distribution measurements in gas turbine combustors are needed from both pollution and fuel-efficiency standpoints.
In addition to providing valuable data for performance The fiber-optic fuel-air sensor, which responds in real time. Optical equivalence ratio sensors for gas turbine combustors Article in Proceedings of the Combustion Institute 30(1) · January with Reads How we measure 'reads'.
Real-time optical fuel-to-air ratio sensor for gas turbine combustors. Fiber optic probe for primary zone fuel distribution measurements in actual liquid-fueled gas turbine combustors. Jong-Guen Lee; Domenic A.
Santavicca. Proc. SPIEAdvanced Sensors and Monitors for Process Industries and the Environment, pg (22 January I monitored the engine RPM (requires a cable not in this kit) and the A/F ratio and it works most of the time and works well.
The software was simple but useful and I found no significant bugs. I also bought the heat sink for the sensor since in a race vehicle, the temperature can get. A system of detection and analysis of gas or fuel oil flames using optical devices, consisting of a sensor that targets the flame's reaction zone through an optical access, a processing and control module, and an actuator, responsible for controlling the damper.
The system optimizes combustion equipment operation by controlling the damper, obtaining better performance and reducing polluting Cited by: "Real-Time Optional Fuel-to-Air Ratio Sensor for Gas Turbine Combustors" Quang-Viet Nguyen, NASA Glenn Research Center, == 86 fixdemocracynow.com "In-Situ Combustion Diagnostics Using Diode Laser Absorption Sensors" Webber fixdemocracynow.com, Stanford University, == fixdemocracynow.com Nov 21, · The fault code on oxygen sensors is one of the most time-consuming fault codes to diagnose.
So take your time and don't get discouraged. The first question has been addressed in the literature. 6–10 Some of these parameters include fuel concentration, fuel-to-air ratio, temperature, pressure, flow dynamics and residual gas concentration. 6 The hostile conditions prevailing in combustors mean that the selected sensors should be able to withstand exposure to such an environment.
CONFERENCE PROCEEDINGS Papers Presentations Journals. Advanced Photonics Journal of Applied Remote Sensing. Apr 11, · Real-Time Optical Fuel-to-Air Ratio Sensor for Gas Turbine Combustors ABSTRACT The 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. This report has been prepared for the Mobile Sources Pollution Control Program and is concerned with aircraft emission control technology.
A parallel investigation of the impact of aircraft emissions has been conducted by NREC for the Bureau of Criteria and Standards.
United States Environmental Protection Agency Office of Air Quality Planning and Standards Research Triangle Park NC EPA/BO21 April Air Municipal Waste Combustor Operator Training Program Instructor's Guide U.S EPA Headquarters Library Mail code T Pennsylvania Avenue NW Washington, DC This ability to automatically design in real time such filters based on measured data could significantly impact many applications.
Desirable approaches will allow real-time, near optimal filter re-design that is then automatically deployed. The approach should lend itself to efficient hardware implementations on a variety of architectures. Full text of "Aeronautical engineering: A continuing bibliography with indexes (supplement )" See other formats.
Full text of "NASA Technical Reports Server (NTRS) Aeronautical engineering: A continuing bibliography with indexes (supplement )" See other formats.
The effect of deterioration in gas turbine pressure ratio and efficiency on fuel cell performance was analyzed, and at the same time, the impact of the degrading fuel cell thermal output on turbine blade aging was modeled to estimate a remaining useful lifetime.
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Eventually the buoyant source term becomes vanishingly.Apr 08, · Real-Time Optical Fuel-to-Air Ratio Sensor for Gas Turbine Combustors ABSTRACT The 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.