Icing Cloud Simulator for Use in Helicopter Engine Induction System Ice Protection Testing

Abstract

Aircraft with Airborne Icing Spraying Systems (AISS) have been used for some time to generate icing clouds into which test aircraft could be flown to show compliance with the requirements of FAR XX.1093. However, the spray arrays used and the relatively large distance between the AISS and aircraft parts to be tested precluded small droplet sizes at high liquid water content at most atmospheric conditions. Some of these shortcomings were overcome by mounting the AISS directly on the test aircraft. This proved to be a very efficient method to develop and certify individual aircraft components. This report describes the methodology and test procedure used with an AISS mounted on a test aircraft to show compliance with FAR 29.1093 for the newly developed inlet of the Bell 222/250-C30G helicopter conversion. Development and certification testing was accomplished in a 4-week period.... Aircraft ice protection, Airborne icing spraying system, AISS, Icing, Inlet.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1992
Accession Number
ADA263203

Entities

People

  • S. W. Brunnenkant

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Ground and Sea Platforms
  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Air Pressure
  • Air Supplies
  • Air Temperature
  • Aircraft Equipment
  • Aircrafts
  • Detectors
  • Flow Rate
  • Foreign Object Damage
  • Heat Transfer
  • Helicopter Engines
  • Helicopters
  • Induction Systems
  • Photoacoustic Tomography
  • Spray Nozzles
  • Test Equipment
  • Transport Aircraft
  • Water Supplies

Fields of Study

  • Environmental science

Readers

  • Aviation Science / Aeronautics.
  • Electrical Engineering
  • Polar and Arctic Studies