Comparison Between Air-Assisted and Single-Fluid Pressure Atomizers for Direct-Injection SI Engines Via Spatial and Temporal Mass Flux Measurements,

Abstract

Two distinct atomization strategies are contrasted through the measurement of time and spatially dependent mass flux. The two systems investigated include a pressure atomizer (6.9 MPa opening pressure) and an air assist atomizer. Both systems have potential for use in direct injection spark ignition engines. The mass flux data presented were obtained using a spray patternator that was developed to allow phased sampling of the spray. The temporal mass related history of the spray was reconstructed as volume versus time plots and interpolated mass flux contour plots. Results indicate substantial differences in the distribution of both mass and mass flux in space and time for the two injection systems. For example, the pressure atomizer at high mass delivery rates produced a spray that collapsed into a dispersed cylindrical shape while at low rates, generated a hollow cone structure. In addition, the air-assist device discharges 87% of its injected volume within the first of three poppet oscillations while producing a wide hollow cone structure.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1997
Accession Number
ADA324774

Entities

People

  • Eric Eberhardt
  • Jay K. Martin
  • Jeffrey A. Hoffman

Organizations

  • University of Wisconsin–Madison

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Abstracts
  • Efficiency
  • Engines
  • Fluids
  • Fuel Injection
  • Fuel Sprays
  • Fuel Systems
  • Fuels
  • High Pressure
  • Injectors
  • Leading Edges
  • Liquid Phases
  • Liquids
  • Measurement
  • Military Research
  • Spark Ignition
  • Steady State

Readers

  • Fluid Dynamics.
  • Petroleum Engineering
  • Structural Dynamics.

Technology Areas

  • Space
  • Space - Hall-Effect Thruster