Comparisons of Turbine Engine Combustor Exhaust Emissions Measurements Using Three Gas-Sampling Probe Designs

Abstract

The effects of sampling probe design and probe operating procedures on measurements of concentrations of nitric oxide (NO), oxides of nitrogen (NOx) , carbon monoxide (CO), carbon dioxide (CO2), total hydrocarbons (CxHy), and gaseous hydrogen (H2) in the exhaust of a turbine engine combustor were studied. Measurements of the concentrations were made using commerical gas analysis instruments and three types of gas-sampling probes. The probe types were a tubular inlet probe, a quick-quench probe, and a dilution probe. Diluent gas (N2, A, He) and diluent flowrate effects on measurements were studied for the dilution probe. Effects of sampling surface material and sample residence time in the probe were investigated for the tubular inlet probe, and the effects of pressure ratio across the quick-quench probe were determined. At fuel-to-air ratios greater than 0.01, the levels of NO, NOx and CO2 were somewhat smaller for the quick-quench and dilution probes than for the tubular inlet probe. The measured concentrations of carbon monoxide and unburned hydrocarbons, however, were greater for the quick-quench and dilution probes than for the tubular inlet probe.

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1978
Accession Number
ADA061733

Entities

People

  • J. D. Few
  • R. J. Bryson

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Flow
  • Air Force
  • Air Supplies
  • Analyzers
  • Carbon Monoxide
  • Chemical Reactions
  • Chemical Synthesis
  • Chemistry
  • Combustion
  • Combustors
  • Dielectric Gases
  • Engineering
  • Engines
  • Flowmeters
  • Materials
  • Measurement
  • Turbines

Fields of Study

  • Environmental science

Readers

  • Aerosol Science/Aerosol Physics
  • Combustion and Flow Dynamics.
  • Combustion science or combustion engineering.