|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F02C-009/18 F01D-017/10 F01D-021/00 F02C-009/46|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 2|
In one example embodiment, a gas turbine system includes a gas turbine, a compressor bleed valve, various sensors, and a valve health assessment system. The compressor bleed valve bleeds a portion of air received by the compressor during certain operating modes. The valve health assessment system includes a processor that uses a neural network model to generate a first failure mode predictor of the compressor bleed valve by processing operational data provided by the various sensors. The processor also generates a second failure mode predictor of the com...
1. A method comprising: receiving in a processor, from at least one sensor, operational data associated with at least one component of a gas turbine;generating, by the processor, a first failure mode predictor of a compressor bleed valve, based at least in part on the operational data, wherein generating the first failure mode predictor comprises using a model to process the operational data associated with the at least one component of the gas turbine;generating, by the processor, a second failure mode predictor of the compressor bleed valve based at le...