A Thermodynamic Study of a Representative Gas Turbine for Design of a Computer Module for Steady State Engine Monitoring and Trending.

reportActive / Technical Report | Accession Number: ADA072713 | Open PDF

Abstract:

The purpose of this paper is to develop equations which represent the steady state operation of the LM2500 marine gas turbine engines and which could be integrated into an inexpensive computer for use in trending the engine.

Author(s):
Tetlow, Thomas George
Author Organization(s):
NAVAL POSTGRADUATE SCHOOL MONTEREY CA
Descriptive Note:
Master's thesis,
Pagination:
0135

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Subject Terms
Joint Capability Areas:
JCA_4.6_Engineering; JCA_4.6.1_General Engineering; JCA_5_Command and Control; JCA_5.3_Planning; JCA_4_Logistics; JCA_1_Force Support; JCA_4.3_Maintain; JCA_1.2_Force Preparation; JCA_1.2.5_Lessons Learned
Communities of Interest:
Materials and Manufacturing Processes
Descriptor(s):
*THERMODYNAMICS, *GAS TURBINES, *MARINE ENGINES, VELOCITY, MONITORING, PERFORMANCE(ENGINEERING), THESES, OPERATIONAL EFFECTIVENESS, STALLING, COMPUTER APPLICATIONS, EQUATIONS, ENGINE SURGE
Field(s)/Group(s):
Thermodynamics, Jet and Gas Turbine Engines
Keyword(s):
LM 2500 engines
Report Date:
1978 May 01