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An apparatus and method for protecting an inner radial surface of a housing of a turbomachine from corrosion. The method includes tapering the inner radial surface of the housing and a corresponding outer radial surface of a corrosion-resistant liner, and heating the housing to increase a diameter o

An apparatus and method for protecting an inner radial surface of a housing of a turbomachine from corrosion. The method includes tapering the inner radial surface of the housing and a corresponding outer radial surface of a corrosion-resistant liner, and heating the housing to increase a diameter of the inner radial surface of the housing. The method also includes inserting the corrosion-resistant liner at least partially into the housing, and attaching the corrosion-resistant liner to the inner radial surface of the housing a solid-state bonding process.

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1. A method for protecting an inner radial surface of a housing of a turbomachine from corrosion, comprising: tapering the inner radial surface of the housing and a corresponding outer radial surface of a corrosion-resistant liner;heating the housing to increase a diameter of the inner radial surfac

1. A method for protecting an inner radial surface of a housing of a turbomachine from corrosion, comprising: tapering the inner radial surface of the housing and a corresponding outer radial surface of a corrosion-resistant liner;heating the housing to increase a diameter of the inner radial surface of the housing;inserting the corrosion-resistant liner at least partially into the housing; andattaching the corrosion-resistant liner to the inner radial surface of the housing a solid-state bonding process. 2. The method of claim 1, wherein the heating the housing comprises enlarging the diameter of the inner radial surface so that the outer radial surface of the corrosion-resistant liner slidably fits therein. 3. The method of claim 2, wherein the heating the housing comprises: placing the housing in a furnace at a temperature of between about 700° F. and about 900° F.; andincreasing the temperature of the furnace to between about 1200° F. and about 2100° F. 4. The method of claim 3, wherein the heating the housing further comprises heating the housing for between about 30 minutes and about 90 minutes per inch of a cross-sectional thickness thereof. 5. The method of claim 3, further comprising: removing the housing from the furnace; andprotecting an environment around the housing to avoid oxidizing the inner radial surface of the housing. 6. The method of claim 1, wherein the attaching the corrosion-resistant liner to the inner radial surface of the housing comprises forge welding the corrosion-resistant liner to the inner radial surface. 7. The method of claim 6, wherein the forge welding the corrosion-resistant liner to the inner radial surface comprises press forging the corrosion-resistant liner to the inner radial surface. 8. The method of claim 6, wherein the forge welding the corrosion-resistant liner to the inner radial surface comprises applying a pressure of from about 0.1 MPa to about 100 MPa to the corrosion-resistant liner using a hydraulic press forge. 9. The method of claim 1, wherein attaching the corrosion-resistant liner to the inner radial surface of the housing comprises explosive cladding the corrosion-resistant liner to the inner radial surface. 10. The method of claim 1, further comprising grit blasting the inner and outer radial surfaces to an RMS roughness of about 64 micro-inches or less, prior to heating the housing. 11. A method for protecting a turbomachine from corrosion, comprising: tapering an annular inner surface of a housing to define first and second inner diameters;tapering an annular outer surface of a corrosion-resistant liner to define first and second outer diameters, the first outer diameter and the first inner diameter being substantially the same size, and the second outer diameter and the second inner diameter being substantially the same size;enlarging the first and second inner diameters, comprising: placing the housing in a furnace at a temperature of from about 700° F. to about 900° F.;heating the furnace to an increased temperature of from about 1200° F. to about 2100° F.; andholding the housing in the furnace for about 1 hour per inch of a cross-sectional thickness of the housing;removing the housing from the furnace while protecting the housing in a protective atmosphere;inserting the corrosion-resistant liner at least partially into the housing such that the first outer diameter is substantially aligned with the first inner diameter; andfixing the corrosion-resistant liner to the housing by explosive cladding or by hot press forging the corrosion-resistant liner to the annular inner surface by applying a pressure of from about 0.1 MPa to about 100 MPa to the corrosion-resistant liner using a hydraulic press forge. 12. The method of claim 11, further comprising: tapering an inner nozzle surface of a nozzle body;heating the nozzle body in the furnace;removing the nozzle body from the furnace;inserting a tapered corrosion-resistant nozzle liner into the nozzle body;fixing the corrosion-resistant nozzle liner to the inner nozzle surface by explosive cladding or by hot press forging the corrosion-resistant nozzle liner to the inner nozzle surface by applying a pressure of from about 0.1 MPa to about 100 MPa to the corrosion-resistant liner using a press forge; andattaching the nozzle body to the housing proximal a radial aperture defined therein.