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MITE PROGRAM OVERVIEW AND ACCOMPLISHMENTS

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(MITE-Multidisciplinary University Research Initiative on Intelligent Turbine Engines) Ben T. Zinn Schools of Aerospace and Mechanical Engineering – PowerPoint PPT presentation

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Title: MITE PROGRAM OVERVIEW AND ACCOMPLISHMENTS


1
  • MITE PROGRAM OVERVIEW AND ACCOMPLISHMENTS
  • (MITE-Multidisciplinary University Research
    Initiative on Intelligent Turbine Engines)
  • Ben T. Zinn
  • Schools of Aerospace and Mechanical Engineering
  • Georgia Institute of Technology
  • Atlanta, Georgia
  • MITE Advisory Board Meeting
  • June 17, 1998

2
  • MITE Program Overview
  • Start Date November 1, 1995
  • Research Team Eleven faculty members with
    expertise in controls, compressors,
    combustion, propulsion, fluid mechanics,
    diagnostics, MEMS and neural net.
  • Facilities Combustion, compressor,
    micro- electronics and fluid mechanics
    laboratories
  • Research Areas Control of combustor processes,
    Nonlinear control theory, Control of
    compressor stall and surge, MEMS

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6
MITE Accomplishments Compressors
  • Modeling Efforts
  • Two and three-dimensional compressible flow
    solvers for modeling compressor stall and surge
    control
  • A multi-mode model for rotating stall and
    surgein axial flow compressors
  • A centrifugal compressor model for surge control
    involving pressure, mass flow rate, and impeller
    RPM dynamics
  • Model extensions for compressor stall control via
    fuel modulations

7
MITE Accomplishments Compressors
  • Control methods
  • Reduced order models based on CFD for
    modelingcompression system transients
  • Optimal nonlinear control framework to address
    disturbance rejection, control saturation and
    robustness
  • Adaptive control framework for elimination of
    rotating stall and surge
  • Nonlinear stabilization framework for
    interactionbetween higher order system modes
  • Combined model and fuzzy rule based
    methodologyto address actuator rate and
    amplitude limits
  • Corrections to the theory of rotating stall
    control through amplitude feedback

8
MITE Accomplishments Compressors
  • Experimental Demonstrations
  • Rotating stall control through
  • Throttling
  • Recirculation of air from plenum to inlet
  • Combustion process modulations
  • Passive means
  • New facility development
  • A centrifugal compressor facility for the study
    of flow dynamics, and for the development of
    active and passive control methods

9
MITE Accomplishments Combustors
  • Synthetic Jets and Fuel-Air Mixing Control
  • Demonstrated mixing enhancement in single and
    co-flowing axisymmetric jets through combination
    of direct small-scale excitation and entrainment
    enhancement through amplitude modulation that
    creates large-scale structures
  • Controlled jet spreading and mixing rates,
    circumferential distribution of mixed "fuel",
    and jet swirl produced by azimuthal excitation
  • Pattern Factor Control Using Synthetic Jets
  • Experimentally demonstrated ability to uniformly
    mix combustor exhaust gases containing large
    temperature differences without injecting
    additional fluid

10
MITE Accomplishments Combustors (continues)
  • Liquid Fuel Atomization Control
  • Developed and demonstrated liquid fuel injector
    that can produce small droplets and control
    droplet size over wide range of liquid flow rates
    using air liquid ratio below one
  • Sensors
  • Designed and successfully simulated a
    water-based, line-of-sight absorption sensor
    capable of monitoring combustor efficiency and
    temperature uniformity at the combustor
    exhaust/turbine inlet
  • Developed prototype of a MEMS pressure transducer
    with wireless readout and high temperature
    capability

11
MITE Accomplishments Combustors (continues)
  • Controllers
  • Developed neural network for adaptive control of
    combustion instability with simulated performance
    capable of suppressing instabilities with 10
    noise in a few seconds
  • Designed and produced neural network chip and
    produced real-time test setup for verifying chip
    operation
  • LES Modeling of Two-Phase Combustors
  • Developed new subgrid two-phase large-eddy
    simulation methodology
  • New LES method is more accurate and
    computationally cheaper at a larger droplet
    cut-off size when compared to conventional LES
    approaches

12
  • MITE Technology Transfer
  • Company Contacts
  • Southwest Sciences, MetroLaser, Boeing (St.
    Louis), United Technologies (Multiple contacts),
    General Electric (Multiple contacts), Allison,
    BEI Sensors, Kistler Instruments
  • Government Contacts
  • Wright-Pattersen AFB (Multiple contacts), NASA
    Lewis (Multiple contacts)
  • Patent Applications 4
  • Publications 36
  • Presentations 40
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