IP Library › Granted Patent US 7,052,527
Granted Patent B2
US 7,052,527 · App. 10/834,215 · Granted May 30, 2006

Thermal spray composition and method of deposition for abradable seals

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Quick Facts
Patent No.
US 7,052,527
App. No.
10/834,215
Granted
May 30, 2006
Kind
B2
Abstract

A thermal spray composition and method of deposition for abradable seals for use in gas turbine engines, turbochargers and steam turbines. The thermal spray composition comprises a mixture of metal-clad solid lubricant particles and unclad solid lubricants particles for producing an abradable seal used in the compressor section of gas engines, aircraft engines, radial compressors and the like. The metal is selected from alloys of Ni, Co, Cu, Fe and Al, preferably Ni alloys, and the solid lubricant is at least one of hexagonal boron nitride, graphite, calcium fluoride, lithium fluoride and molybdenum disulphide, preferably hexagonal boron nitride or hexagonal boron nitride and graphite.

Claims (11)

1. A thermal spray powder composition for an abradable seal comprising about 70 to 95 wt % of a metal-clad solid lubricant and about 5 to 30 wt % solid lubricant.

2. A thermal spray powder composition for an abradable seal comprising about 80 to 90 wt % of a metal-clad solid lubricant and about 10 to 20 wt % of unclad solid lubricant.

3. A thermal spray composition as claimed in claim 1 , in which the solid lubricant is at least one lubricant powder selected from the group consisting of hexagonal boron nitride, graphite, calcium fluoride, lithium fluoride, magnesium fluoride, barium fluoride, tungsten disulfide and molybdenum disulfide particles.

4. A thermal spray composition as claimed in claim 1 , in which the solid lubricant is a mixture of hexagonal boron nitride and graphite particles.

5. A thermal spray composition as claimed in claim 1 , in which the solid lubricant is hexagonal boron nitride particles.

6. A thermal spray composition as claimed in claim 3 , in which the thermal spray composition is a powder, a wire or a rod and in which the metal alloy cladding is selected from the group consisting of Ni, Co, Cu, Fe, Al, and combinations and alloys thereof.

7. A thermal spray composition as claimed in claim 4 , in which the metal alloy cladding is selected from the group consisting of Ni, Co, Fe and combinations and alloys thereof.

8. A thermal spray composition as claimed in claim 5 , in which the metal alloy cladding is Ni, NiCr, NiCrAl or Ni alloy.

9. A thermal spray composition as claimed in claim 5 , in which the metal alloy cladding is NiCrAl.

10. A thermal spray composition as claimed in claim 5 , in which the metal alloy cladding is selected from the group consisting of Ni, Co, Fe and combinations and alloys thereof.

11. An abradable seal for gas turbine engines, turbo changers, compressors or steam turbines produced by applying an adherent coating having a thickness up to 3 mm to a substrate by thermally spraying a composition thereon comprising about 70 to 95 wt % of a metal-clad solid lubricant comprised of hexagonal boron nitride clad with a metal selected from the group consisting of Ni, NiCr, NiCrAl and Ni alloy, and about 5 to 30 wt % of a solid lubricant comprised of hexagonal boron nitride.