HIGH IMPACT SHOCK TEST OF A GENERAL ELECTRIC LM2500 PROPULSION GAS TURBINE MODULE

Discusses the high impact shock testing of a General Electric Propulsion Gas Turbine Module to the requirements of Military Specification MIL-S-901C. This shock qualification is just one of a comprehensive program of tests to be performed to fully qualify the LM2500 Gas Turbine and the DD-963 Propulsion System components specifically for the Spruance (DD-963) Class Destroyers. The description of the gas turbine and the preparation for, and the conduct of the shock test, and a review of the shock test results are presented.

  • Supplemental Notes:
    • Paper for meeting April 8-12, 1973.
  • Corporate Authors:

    American Society of Mechanical Engineers

    Two Park Avenue
    New York, NY  United States  10016-5990
  • Authors:
    • Bobo, W R
  • Publication Date: 1973-4

Media Info

  • Pagination: 11 p.

Subject/Index Terms

Filing Info

  • Accession Number: 00047659
  • Record Type: Publication
  • Source Agency: Engineering Index
  • Report/Paper Numbers: Paper n 73-GT-88
  • Files: TRIS
  • Created Date: Oct 31 1973 12:00AM