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公开(公告)号:US20170253821A1
公开(公告)日:2017-09-07
申请号:US15058305
申请日:2016-03-02
Applicant: GENERAL ELECTRIC COMPANY
Inventor: Pierre MONTAGNE , Krishnamurthy ANAND , Prajina BHATTACHARYA , Paul Stephen DIMASCIO , Jeffrey Scott GOLDMEER , Abdurrahman Abdallah KHALIDI , Praveen Babulal JAIN , Adarsh SHUKLA , Eklavya CALLA , Paul Burchell GLASER
CPC classification number: C10L10/04 , C10L1/12 , C10L1/1208 , C10L1/1216 , C10L1/1225 , C10L1/125 , C10L1/1266 , C10L1/1275 , C10L1/1283 , C10L10/06 , C10L2200/0213 , C10L2200/0218 , C10L2200/0222 , C10L2200/0227 , C10L2200/024 , C10L2200/0438 , C10L2200/0446 , C10L2270/04 , F02C3/30 , F05D2260/95 , F05D2300/30
Abstract: A gas turbine process includes supplying a fuel to a gas turbine, combusting the fuel in the gas turbine with a hot gas path temperature reaching at least 1100° C. during operation of the gas turbine, and supplying an inhibition composition including at least one yttrium-containing inorganic compound to interact with the vanadium and inhibit vanadium hot corrosion in the gas turbine caused by vanadium as a fuel impurity in the fuel. A process includes supplying an inhibition composition including at least one yttrium-containing inorganic compound to a hot gas path or a combustor of a gas turbine. A fuel composition includes a fuel including at least one fuel impurity including vanadium and an inhibition composition including at least one yttrium-containing compound. An atomic ratio of yttrium to vanadium in the fuel composition is in a range of 1 to 1.5.