An abrasive layer is formed on the tip portion of a turbine engine blade made of Ti alloy by (a) electroplating a 12-18 microns thick first Ni layer onto the blade tip; (b) electroplating a max. 1 micron thick second Ni layer; (c) electroplating a third Ni layer, immersing the tip in a slurry of electrically non-conductive particles in an electroplating soln. present on a membrane which is permeable to electric current and the soln., and then contg. electroplating of the third Ni layer; (d) electroplating a fourth Ni layer such that the combined thickness of the third and fourth layers corresponds to 50-95% of the mean dimension of the embedded particles, and (e) heat treating the blade to cause diffusion between the first Ni layer and the blade tip.
申请公布号
DE4021044(A1)
申请公布日期
1991.01.17
申请号
DE19904021044
申请日期
1990.07.02
申请人
UNITED TECHNOLOGIES CORP., HARTFORD, CONN., US
发明人
ROUTSIS, KOSTAS, EAST HARTFORD, CONN., US;PARKOS JUN., JOSEPH JOHN, EAST HADDAM, CONN., US;FRELING, MELVIN, WEST HARTFORD, CONN., US