GAS TURBINE SYSTEM-MONITORING METHOD AND GAS TURBINE ENGINE-MONITORING SYSTEM TO MONITOR COMBUSTION SYSTEM HAVING WELL-SELECTED BINDER

PURPOSE: A gas turbine system-monitoring method and gas turbine engine-monitoring system are provided to decide wear and maintenance plans and to reduce poisonous release by detecting and monitoring UV-photosensitive material release from a coating and obtaining exact information and specific positi...

Full description

Saved in:
Bibliographic Details
Main Authors RUUD JAMES, DEVITT JOHN W, KOOL LAWRENCE B
Format Patent
LanguageEnglish
Korean
Published 20.05.2004
Edition7
Subjects
AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
ENGINE PLANTS IN GENERAL
GAS-TURBINE PLANTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
LIGHTING
MACHINES OR ENGINES IN GENERAL
MEASURING
MEASURING QUANTITY OF HEAT
MEASURING TEMPERATURE
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
PHYSICS
STEAM ENGINES
TESTING
THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
WEAPONS
Online AccessGet full text

Cover

More Information
Summary:PURPOSE: A gas turbine system-monitoring method and gas turbine engine-monitoring system are provided to decide wear and maintenance plans and to reduce poisonous release by detecting and monitoring UV-photosensitive material release from a coating and obtaining exact information and specific position information. CONSTITUTION: A gas turbine system-monitoring method comprises steps of selecting a binder(14) to monitor temperature by releasing an indicator(12) within a temperature range decided to make a substrate(16) of a gas turbine system take high-temperature operation till the temperature under the critical turbine substrate degradation temperature; combining the indicator and the binder; and coating the substrate with the combined indicator and binder to form monitoring deposits.
Bibliography:Application Number: KR20030080532