Accession Number:

AD0775304

Title:

The Feasibility of Detecting a Burner-Can Burn-Through by Means of CO, CO2, Pressure, and Air Temperature Levels in a Jet Engine Nacelle.

Descriptive Note:

Final rept. Jan 72-Jul 73,

Corporate Author:

NATIONAL AVIATION FACILITIES EXPERIMENTAL CENTER ATLANTIC CITY N J

Personal Author(s):

Report Date:

1974-03-01

Pagination or Media Count:

27.0

Abstract:

Full-scale tests simulating engine combustion section thermal failure burn-through were conducted using a cowled J-57 engine to determine the feasibility of detecting a burn-through by monitoring the carbon monoxide CO, carbon dioxide CO2, a pressure level, or air temperature in the nacelle before, during, and after engine case rupture. Results of the tests indicated that CO, CO2, pressure, and air temperature in the nacelle cannot be relied upon for early detection of a burn-through. Test results also indicated that containment of a burn-through flame in the nacelle creates extremely high temperatures in the nacelle and can cause extensive structural damage. Author

Subject Categories:

  • Aircraft
  • Safety Engineering
  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE