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公开(公告)号:US20180355745A1
公开(公告)日:2018-12-13
申请号:US15974821
申请日:2018-05-09
Applicant: General Electric Company
Inventor: Paul MATHEW , Mohandas NAYAK , Krishnendu SAHA , Deoras PRABHUDHARWADKAR
CPC classification number: F01D11/125 , B22F1/0059 , B22F7/08 , B22F2301/15 , B22F2302/45 , B22F2998/10 , B22F2999/00 , F01D11/001 , F01D11/127 , F05D2220/32 , F05D2230/21 , F05D2230/40 , F05D2300/224 , F05D2300/228 , F05D2300/43 , B22F7/04 , B22F7/002 , B22F2007/066 , B22F3/10
Abstract: A filled abradable seal component, an associated method of manufacturing, and a turbomachine including the filled abradable seal component are disclosed. The method includes positioning the abradable seal component including a plurality of honeycomb cells, applying a filler material on the abradable seal component to fill the plurality of honeycomb cells, and curing the filler material at a temperature below 250 degrees Celsius to produce the filled abradable seal component. The filler material includes an abradable material, a binder material, and a fluid catalyst. The abradable material includes at least one of nickel chromium aluminum-bentonite, cobalt nickel chromium aluminum yttrium-polyester, cobalt nickel chromium aluminum yttrium-boron nitride, aluminum silicon-bentonite, aluminum bronze-polyester, nickel graphite, or aluminum silicon-boron nitride. The binder material includes at least one of aluminum, nickel-aluminum, aluminum thiophosphate, or aluminum thiosulfate. The fluid catalyst includes a solvent having hydroxyl groups.