Needs for and means of improving D and CM and trouble-shooting to modules and LRUs for T700-GE-700 engine in Army environment were studied. Recommendations are: Do not modify existing METS for modular fault isolation. However, do computerize the acquisition of the overall engine performance data, introduce the slave chip detector to the depot, expand evaluation of the control system analyzer by Black Hawk companies, support the development of degaussing chip detector, initiate Phase I of multipurpose airborne D and CM system which combines performance, life, overtemp and chip detector monitors, and continue of acquire T700 field data and develop a method to quantify D and CM payoffs such as better engine availability.
Diagnostic and condition monitoring system assessment for army helicopter modular turboshaft engines
Diagnostische und Zustand-Informations-Systembestimmung fuer Armeehubschrauber mit modularen Turbowellenantrieben
US Government Reports ; Okt ; 1-151
1980
151 Seiten
Report
Englisch
Automated Power Assessment for Helicopter Turboshaft Engines
British Library Conference Proceedings | 2008
|Steady-state and Dynamic Monitoring of Helicopter Turboshaft Engines: Analysis and Results
British Library Conference Proceedings | 1995
|U.S. Army rotorcraft turboshaft engines sand & dust erosion considerations
Tema Archiv | 1994
|Calculation of Air Velocity on the Helicopter Turboshaft Engines Inlet
SAE Technical Papers | 2021
|