Advanced thermally conductive lightweight elastomeric seal
A thermally conductive lightweight elastomeric seal including a stator substrate having an external surface; a casing coupled to the external surface, the casing including radial walls extending orthogonal radially from the external surface; an abradable material disposed within the casing, the abradable material comprises an elastomer material with imbedded metal-coated hollow microspheres, wherein the abradable material comprises a density of 0.5 to 0.6 grams/cubic centimeter; the abradable material and the casing being coupled together.
1. A thermally conductive lightweight elastomeric seal comprising:
a stator substrate having an external surface;
a casing coupled to the external surface, the casing including radial walls extending orthogonal radially from the external surface;
an abradable material disposed within the casing, the abradable material comprises an elastomer material with imbedded metal-coated hollow microspheres, wherein the abradable material comprises a density of 0.5 to 0.6 grams/cubic centimeter, wherein the abradable material comprises elastic moduli ranging from 200-500 pounds per square inch; and
the abradable material and the casing being coupled together.
2. The thermally conductive lightweight elastomeric seal according to claim 1 , wherein the casing includes a floor directly coupled to the external surface and coupled to the abradable material.
3. The thermally conductive lightweight elastomeric seal according to claim 1 , wherein the elastomer material is selected from the group consisting of nitrile, polyurethane, viton and silicone.
4. The thermally conductive lightweight elastomeric seal according to claim 1 , wherein the abradable material comprises thermal conductivities ranging from 1.3-2.0 W/mK.
5. The thermally conductive lightweight elastomeric seal according to claim 1 , wherein the radial walls extending orthogonal radially from the exterior surface are configured to contain the abradable material within the radial walls, relative to an axis A.
6. The thermally conductive lightweight elastomeric seal according to claim 1 , wherein the casing and the abradable material comprise a ratio of elastic modulus of the casing to the abradable material of 50 to 5000.
7. A thermally conductive lightweight elastomeric seal for a gas turbine engine rotor and stator comprising:
a stator substrate having an external surface;
a casing coupled to the external surface, the casing including radial walls extending radially from the external surface;
an abradable material disposed within the casing radial walls relative to an axis A, the abradable material comprises an elastomer material with imbedded metal-coated hollow microspheres, wherein the abradable material comprises a density of 0.5 to 0.6 grams/cubic centimeter, wherein the abradable material comprises thermal conductivities ranging from 1.3-2.0 W/mK; and
the abradable material and the casing being coupled together.
8. The thermally conductive lightweight elastomeric seal for the gas turbine engine rotor and stator according to claim 7 , wherein the metal-coated hollow microspheres are pretreated with an adhesion promoter.
9. The thermally conductive lightweight elastomeric seal for the gas turbine engine rotor and stator according to claim 7 , wherein the casing comprises a material selected from the group consisting of polyether ketone, polyether ether ketone, polyetherimide, polyamide imide, polyphenylene sulfide or polyphenylsulfone and a reinforced thermoset organic matrix composite.
10. The thermally conductive lightweight elastomeric seal for the gas turbine engine rotor and stator according to claim 9 , wherein the reinforced thermoset organic matrix composite is selected from the group consisting of an epoxy or imide-based resin reinforced with at least one of a carbon fiber, a glass fiber and a fabric, wherein the fabric includes carbon or glass.
11. The thermally conductive lightweight elastomeric seal for the gas turbine engine rotor and stator according to claim 7 , wherein the casing comprises neat or reinforced thermoplastic.
12. The thermally conductive lightweight elastomeric seal for the gas turbine engine rotor and stator according to claim 7 , wherein the elastomer material is selected from the group consisting of nitrile, polyurethane, viton and silicone.
13. A gas turbine engine abradable seal thermal conduction process comprising:
providing a stator substrate having an external surface;
coupling a casing to the external surface, the casing including radial walls extending radially from the external surface;
disposing an abradable material within the casing radial walls relative to an axis A, wherein the abradable material comprises an elastomer material with imbedded metal-coated hollow microspheres, wherein the abradable material comprises a density of 0.5 to 0.6 grams/cubic centimeter, wherein the abradable material comprises elastic moduli ranging from 200-500 pounds per square inch; and
coupling the abradable material and the casing together.
14. The process of claim 13 , wherein the casing includes a floor directly coupled to the exterior surface; and coupling the floor to the abradable material.
15. The process of claim 13 , wherein the casing and the abradable material comprise a ratio of elastic modulus of the casing to the abradable material of 50 to 5000.
16. The process of claim 13 , wherein the elastomer material is selected from the group consisting of nitrile, polyurethane, viton and silicone.
17. The process of claim 13 , further comprising:
fabricating the gas turbine engine abradable seal in-situ with low modulus abradable material loaded and cured into the casing following installation of the abradable seal.
18. The process of claim 13 , wherein the abradable material comprises thermal conductivities ranging from 1.3-2.0 W/mK.