Abradable ceramic seal and method of making same

Claim 2

In a method for forming a fluid seal abradable coating on one of a pair of members having relative rotational movement, said one member being the turbine engine casing having a thermal barrier coating of the stabilized zirconia type applied to a bond layer consisting essentially of a NiCrAly alloy covering said casing, the steps of codepositing heat softened, molten zirconia and an oxide from the group consisting of Y 2 O 3 , MgO and CaO, and a thermally decomposable organic filler powder to form a layer of the desired depth on said thermal barrier coating, and heating said layer to an elevated temperature and for a time period as necessary to decompose said orgaic filler powder and produce a porous abradable layer having from about 20 to about 33% voids.

Claim 3

A method as set forth in claim 1 wherein the thickness of said layer is from about 0.040 to about 0.060 inches.

Claim 4

A method as set forth in claim 2 wherein said organic filler powder is a polyester powder of -140 +325 mesh size and said heating is accomplished at about 1800° F. for a period of about 4 hours.

Claim 5

In a method for forming an abradable fluid seal porous coating adherent to the thermal barrier coating of the stabilized zirconia type provided on a bond layer consisting essentially of a NiCrAly alloy on the surface of a turbine engine casing, the steps of depositing on said thermal barrier coating a ceramic material consisting essentially of zirconia and an oxide from the group consisting of Y 2 O 3 , MgO and CaO, by passing said material in powder form through a depositing unit adapted to heat said material to the softening point and spray a stream thereof to enable plastic deformation of the material when deposited on said surface, codepositing a thermally decomposable organic filler powder with said ceramic material by feeding said organic filler powder into said ceramic material stream at a point downstream from the spray nozzle of said depositing unit so as to control the residence time of said organic filler powder in said ceramic material stream to prevent thermal decomposition prior to deposition on said surface, and heating said codeposited ceramic material and organic powder to decompose said organic powder and produce a porous abradable coating on said surface having from about 20 to about 33% voids.

Claim 6

In a method for forming an abradable fluid seal porous coating adherent to the thermal barrier coating of the stabilized zirconia type provided on a bond layer consisting essentially of a NiCrAly alloy on the surface of a turbine engine casing, the steps of depositing on said thermal barrier coating a ceramic material consisting essentially of zirconia and an oxide from the group consisting of Y 2 O 3 , MgO and CaO, by passing said material in powder form through a depositing unit adapted to heat said material to the softening point and spray a stream thereof to enable plastic deformation of the material when deposited on said surface, codepositing a thermally decomposable organic filler powder with said ceramic material by feeding said organic filler powder into said ceramic material stream at a point downstream from the spray nozzle of said depositing unit so as to control the residence time of said organic filler powder in said ceramic material stream to prevent thermal decomposition prior to deposition on said surface, and heating said codeposited ceramic material and organic powder to decompose said organic powder and produce a porous abradable coating on said surface having from about 20 to about 33% voids.

Claim 7

A method as set forth in claim 4 wherein the thickness of said coating is from about 0.040 to about 0.060 inches.

Claim 8

A method as set forth in claim 5 wherein said organic filler powder is a polyester powder of -140 +325 mesh size and said heating is accomplished at about 1800° F. for a period of about 4 hours.