Accession Number : ADA132357

Title :   Jet Engine Burn-Through Investigation. Volume 2. Engine Tests Raw Data.

Descriptive Note : Final rept. Jun-Sep 72,


Personal Author(s) : Schumacker,Richard W

PDF Url : ADA132357

Report Date : Mar 1973

Pagination or Media Count : 301

Abstract : The work performed during this program was directed toward determining the acoustic characteristics of simulated burn-through failures. To determine the feasibility of detecting this failure acoustically two types of jet engines (J-47 and J-57) were modified to simulate burn-through failures. Magnetic tape recordings of the modified engines were made to determine the extent of the acoustic spectrum; the relationships of engine speed to failure-related sound pressure levels and acoustic spectrum; the effect of sensor location to detect the failure acoustically; and characteristic acoustic spectra at burn-through. The recorded data was analyzed by real time spectrum analysis and mean square techniques. Results indicated that the simulated burn-through failure acoustic spectra consists primarily of broadband random noise above 5 kHz. It was also determined that sensor location is an important factor in detecting burn-through failures. Based on the results it is concluded that acoustic detection of a burn-through failure is feasible. Recommendations for a monitor and detector based on the results of this program have been included. Volume I contains the Sonic Analysis. (Author)

Descriptors :   *Burnthrough, *Acoustic detectors, *Turbojet engines, Acoustic data, Acoustic measurement, Energy levels, Fuel lines, Combustors, Combustion chambers, Failure(Mechanics), Simulation, Sound pressure, Spectrum analysis, Real time, Experimental data, Noise(Sound), Broadband, Intensity, Microphones, Monitors, Feasibility studies

Subject Categories : Test Facilities, Equipment and Methods
      Acoustic Detection and Detectors
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE