Laboratory Evaluation of Novel Particulate Control Concepts for Jet Engine Test Cells.

Abstract

Three control devices were evaluated in the laboratory to determine their ability to reduce visible emissions from jet engine test cells. The three control devices - a low-pressure drop wet scrubber, a wetted-sand filter, and a high-temperature, ceramic fabric baghouse - were tested on the exhaust of a small gas turbine engine with a variable resistive load. Three fuel mixtures were used in experimental runs: 100 percent kerosene, 100 percent toluene, and a 50/50 blend of kerosene and toluene. Smoke number measurements of the treated and untreated exhaust stream were compared to evaluate the reduction in visual emissions for each control device. None of the three devices tested indicated enough reduction in plume opacity to justify construction of full-scale test cell control systems. Recommendations were made for future evaluation of modified wetted sand filter and ceramic fiber baghouse control devices. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1983
Accession Number
ADA137641

Entities

People

  • R. W. Boubel

Organizations

  • Oregon State University

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Air Pollution
  • Barometric Pressure
  • Calorific Value
  • Chemical Synthesis
  • Chemistry
  • Combustion
  • Gas Turbines
  • Jet Engines
  • Liquids
  • Material Degradation Processes
  • Materials Laboratories
  • Materials Science
  • Measurement
  • Organic Materials
  • Thermodynamics
  • Turbines

Readers

  • Aerosol Science/Aerosol Physics
  • Aerospace Engineering