Skip to main content
U.S. Department of Energy
Office of Scientific and Technical Information

Partial Premixing Effects on the Reacting Jet of a High-Pressure Axially Staged Combustor

Journal Article · · Journal of Engineering for Gas Turbines and Power
DOI:https://doi.org/10.1115/1.4049700· OSTI ID:1844597
 [1];  [2];  [2];  [3];  [2]
  1. Univ. of Central Florida, Orlando, FL (United States); Embry-Riddle Aeronautical University
  2. Univ. of Central Florida, Orlando, FL (United States)
  3. Embry-Riddle Aeronautical Univ., Daytona Beach, FL (United States)

The effects of partial premixing on a reacting jet-in-crossflow is investigated in a five atmosphere axially staged combustor at stationary gas turbine relevant conditions. The facility consists of a dump style headend burner that provides a crossflow with a quasi-uniform velocity and temperature profile to the axial stage to isolate the effects of the jet-in-crossflow. The headend burner is run with methane and air at a lean equivalence ratio to match industry emission standards. For this work, the total air to the headend and axial stage is kept constant, and fuel is split between the headend and axial stage to represent different gas turbine loading conditions. For the cases analyzed, the fuel split to the axial stage went up to 25%. The axial stage consists of an optically accessible test section with a coaxial injector that provides variability to how long the methane and air can mix before entering the facility. Three different premixed levels are studied: fully premixed, nonpremixed, and partially premixed. The flow-field characteristics of the reacting jet-in-crossflow are analyzed using particle image velocimetry (PIV), and flame behavior is quantified by employing CH* chemiluminescence. NO measurements are made at the exit of the facility using a Horiba emissions analyzer. Furthermore, two different flames are observed: flames that burn in the leeward recirculation region and flames that burn at the core of the jet.

Research Organization:
Embry-Riddle Aeronautical Univ., Daytona Beach, FL (United States)
Sponsoring Organization:
USDOE
Grant/Contract Number:
FE0031227
OSTI ID:
1844597
Journal Information:
Journal of Engineering for Gas Turbines and Power, Journal Name: Journal of Engineering for Gas Turbines and Power Journal Issue: 3 Vol. 143; ISSN 0742-4795
Publisher:
ASMECopyright Statement
Country of Publication:
United States
Language:
English

References (10)

Nitric oxide levels of turbulent jet diffusion flames: Effects of residence time and damkohler number journal January 1992
Oxides of nitrogen emissions from turbulent jet flames: Part II—Fuel dilution and partial premixing effects journal May 1993
NOx emission and major species concentrations in partially premixed laminar methane/air co-flow jet flames journal May 1996
The auto-ignition temperature of methane journal January 1984
Effects of turbulence on nonpremixed ignition of hydrogen in heated counterflow journal February 2003
A study of pollutant emission characteristics of partially premixed turbulent jet flames journal March 1999
Time-averaged characteristics of a reacting fuel jet in vitiated cross-flow journal July 2014
Flowfield measurements and flame stabilization of a premixed reacting jet in vitiated crossflow journal October 2015
Emission Measurements and CH* Chemiluminescence of a Staged Combustion Rig for Stationary Gas Turbine Applications journal June 2012
A Model for Predicting the Lift-Off Height of Premixed Jets in Vitiated Cross Flow journal March 2016

Similar Records

Fuel Stratification Influence on NOx Emission in a Premixed Axial Reacting Jet-in-Crossflow at High Pressure
Journal Article · Wed Mar 03 23:00:00 EST 2021 · Journal of Energy Resources Technology · OSTI ID:1844555

The Influence of Pressure on Flame-Flow Characteristics of a Reacting Jet in Crossflow
Journal Article · Fri Jul 30 00:00:00 EDT 2021 · Journal of Energy Resources Technology · OSTI ID:1844553

Characteristics of a Reacting Jet-in-Crossflow at Elevated Pressures
Conference · Wed Aug 21 00:00:00 EDT 2019 · OSTI ID:1559031