http://rdf.ncbi.nlm.nih.gov/pubchem/patent/KR-100825142-B1
Outgoing Links
| Predicate | Object |
|---|---|
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C9-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G01K11-06 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C9-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C7-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F01D25-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G01K11-06 |
| filingDate | 2003-11-14-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate | 2008-04-24-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationDate | 2008-04-24-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | KR-100825142-B1 |
| titleOfInvention | Gas Turbine System Monitoring Method and Gas Turbine Engine Monitoring System |
| abstract | A method of forming a monitoring deposit on gas 16 includes determining a temperature range such that the gas 16 is provided with an operating high temperature below the critical gas 16 degradation temperature, and within the determined temperature range. Selecting the binder 14 to monitor the temperature by releasing an indicator, combining the indicator with the binder, and applying the combined indicator and binder to the gas 16 to deposit the monitoring. Forming a step. The product includes a gas 16 and a combination of indicators and binders applied within the gas 16, wherein the binder 14 is capable of operating at high temperatures below the critical gas 16 degradation temperature. Release the indicator within a temperature range determined to be subjected to. In addition, the method for monitoring a gas turbine system includes the binder 14 to monitor the temperature by releasing the indicator within a temperature range determined to permit the gas in the system to undergo a high temperature operation below the critical turbine gas 16 degradation temperature. And selecting the indicator, combining the indicator with the binder, and applying the combined indicator and the binder to form the monitoring deposit. The system for monitoring a gas turbine engine includes a gas 16 and a combined indicator and binder applied on the gas 16, wherein the binder 14 is capable of hot operation up to a critical gas deterioration temperature. The indicator is released within a temperature range determined to be received by the gas 16. |
| priorityDate | 2002-11-15-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 19.