2.4.3: Low Emissions, Quiet, Flameless Combustor - PowerPoint PPT Presentation

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2.4.3: Low Emissions, Quiet, Flameless Combustor

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Government NASA GRC and Air Force laboratory. URETI URETI's on Hypersonics ... A Burner Stabilizing Flame and Flameless Oxidation. 2.4.3 Proposed Approach ... – PowerPoint PPT presentation

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Title: 2.4.3: Low Emissions, Quiet, Flameless Combustor


1
2.4.3 Low Emissions, Quiet, Flameless Combustor
2.4 High Performance Components
Primary Investigators Zinn, Menon and Seitzman
(Ga. Tech)
  • Projects Science Technology Objective(s)
  • Objective 1 Lower NOx, CO and smoke emissions
  • Objective 2 Reduce combustor noise
  • Objective 3 Increase combustor stability
  • Explanatory Figure, Picture, or Graphic
  • Potential/Current Collaborations
  • Government NASA GRC and Air Force laboratory
  • URETI URETIs on Hypersonics
  • Industry All engine companies
  • Synergism with existing programs NASA UEET, GE
    USA Center, GE Power Systems

A Burner Stabilizing Flame and Flameless Oxidation
  • Accomplishments
  • Accomplishment 1 Determination of the
    feasibility of using flameless combustion in
    aircrafts engines
  • Accomplishment 2 Assessment of the benefits of
    flameless combustion in aircraft applications
  • Accomplishment 3 Obtain data for developing
    practical aircraft engines flameless combustors
  • Proposed Research Approach
  • Step 1 Adapt flameless combustion concept to
    aircraft applications
  • Step 2 Investigate analytically and
    experimentally the feasibility of proposed
    flameless combustor concepts
  • Step 3 Demonstrate benefits of flameless
    combustion
  • Milestones
  • 1 Develop aircraft, flameless, combustor
    concepts
  • 2 Demonstrate feasibility of proposed aircraft
    engines flameless combustor concepts
  • 3 Quantify benefits of flameless combustion in
    aircraft applications
  • NASA Relevance/Impact
  • Relevance/impact 1 Reduce NOx, CO and smoke
    emissions
  • Relevance/impact 2 Improve engines
    reliability/safety
  • Relevance/impact 3 Reduce engines noise

2
2.4.3 Proposed Approach
  • Investigate/Modify developed industrial flameless
    combustor concepts for aircraft engine
    applications
  • Use Large Eddy Simulations (LES) to investigate
    the feasibility of the proposed aircraft engines
    flameless combustor concepts
  • Use the prediction of the LES simulations to
    develop a proof of concept flameless combustor
    for aircraft engine applications
  • Use LES simulations and measured data to
  • Quantify the benefits of flameless combustion in
    aircraft applications, and
  • Improve understanding of the fundamental
    processes that control flameless combustion
  • Share developed understanding of flameless
    combustion with NASA, Air Force and Industry in
    an effort to develop practical flameless
    combustors
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