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A combustor basket (20) is provided comprising a generally tubular wall (22) defining a cavity (24) and a liner (26) of a ceramic matrix composite material disposed within the cavity (24), wherein an interference fit exists between an outer surface (34) of the liner (26) located in the cavity (24) a

A combustor basket (20) is provided comprising a generally tubular wall (22) defining a cavity (24) and a liner (26) of a ceramic matrix composite material disposed within the cavity (24), wherein an interference fit exists between an outer surface (34) of the liner (26) located in the cavity (24) and an inner surface (28) of the generally tubular wall (22). Advantageously, the novel combustor basket (20) greatly reduces the amount of air or other medium needed to cool the combustor basket body and increases the maximum allowable flame temperature that the combustor basket (20) can withstand. A method of manufacturing the combustor basket (20) is also provided.

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1. A combustor basket of a combustor section, comprising: the combustor basket comprising a generally tubular wall comprising a metallic alloy material defining a cavity with an inlet and an outlet for passing an air-fuel mixture;a liner of a ceramic matrix composite material disposed within the cav

1. A combustor basket of a combustor section, comprising: the combustor basket comprising a generally tubular wall comprising a metallic alloy material defining a cavity with an inlet and an outlet for passing an air-fuel mixture;a liner of a ceramic matrix composite material disposed within the cavity, wherein an interference fit exists between an outer surface of the liner located in the cavity and an inner surface of the generally tubular wall. 2. The combustor basket of claim 1, wherein a degree of interference fit between the generally tubular wall and the liner is from 10 to 45 mils. 3. The combustor basket of claim 1, wherein a thermal conductivity value for the metallic alloy material of the generally tubular wall is at least 5 times greater than a thermal conductivity value for the ceramic matrix composite material of the liner. 4. The combustor basket of claim 1, wherein a coefficient of thermal expansion for the metallic alloy material of the generally tubular wall is at least 1.5 times a value for a coefficient of thermal expansion for the ceramic matrix composite material of the liner. 5. The combustor basket of claim 1, wherein the interference fit is effective for use at a temperature of 1600° C. 6. The combustor basket of claim 1, wherein the combustor basket is used within a gas turbine engine combustor. 7. The combustor basket of claim 1, wherein a thickness of the tubular wall is between 2 mm and 3.5 mm, and wherein a thickness of the liner is between 3 mm and 6 mm. 8. The combustor basket of claim 1, wherein the liner is configured to thermally contract upon exposure of the ceramic matrix composite material of the liner to a temperature less than an ambient temperature, for insertion of the liner within the cavity; and wherein the liner is configured to thermally expand upon exposure of the ceramic matrix composite material of the liner to the ambient temperature, to form the interference fit between the liner and the tubular wall. 9. The combustor basket of claim 3, wherein said thermal conductivity values of the metallic alloy material of the generally tubular wall and the ceramic matrix composite material of the liner are adjusted, such that the liner is configured to expand at a degree relative to a degree of expansion of the tubular wall, to maintain the interference fit. 10. A combustor basket of a combustor section, comprising: the combustor basket comprising a generally tubular wall comprising a metallic alloy material defining a cavity with an inlet and an outlet for passing an air-fuel mixture;a liner of a ceramic matrix composite material disposed within the cavity, wherein an interference fit exists between an outer surface of the liner located in the cavity and an inner surface of the generally tubular wall, where the outer surface of the liner is in full contact with the inner surface of the generally tubular wall; andan alloy attachment welded to an outer surface of the generally tubular wall;wherein the liner has a pre-installation outer diameter that is greater than an inner diameter of the combustor basket; andwherein the interference fit is effective for use at a temperature of 1600° C. 11. The combustor basket of claim 10, wherein the interference fit is accommodated by a temperature differential between the outer surface of the liner and the inner surface of the generally tubular wall. 12. The combustor basket of claim 11, wherein the outer surface of the liner is configured to thermally contract upon exposure to an ambient temperature, to establish the temperature differential. 13. The combustor basket of claim 11, wherein the inner surface of the generally tubular wall is configured to thermally expand upon exposure to heat to establish the temperature differential. 14. The combustor basket of claim 11, wherein the temperature differential is approximately 198 degrees Celsius. 15. A combustor basket of a combustor section, comprising: the combustor basket comprising a generally tubular wall comprising a metallic alloy material defining a cavity with an inlet and an outlet for passing an air-fuel mixture;a liner of a ceramic matrix composite material disposed within the cavity, wherein an interference fit exists between an outer surface of the liner located in the cavity and an inner surface of the generally tubular wall;wherein the liner has a pre-installation outer diameter that is greater than an inner diameter of the combustor basket;wherein the interference fit is effective for use at a temperature of 1600° C.;wherein the liner is configured to thermally contract upon exposure of the ceramic matrix composite material of the liner to a temperature less than an ambient temperature, for insertion of the liner within the cavity; and wherein the liner is configured to thermally expand upon exposure of the ceramic matrix composite material of the liner to the ambient temperature, to form the interference fit between the liner and the tubular wall.