Methods and apparatus for making ceramic matrix composite lined automotive parts and fiber reinforced ceramic matrix composite automotive parts

Claim 1

A method of forming a breakage and erosion-resistant ceramic liner for a part comprising the steps of: a) forming a liner of a cast monolithic ceramic material containing pores; b) filling the pores with a pre-ceramic polymer resin; and c) firing the liner filled with the pre-ceramic polymer resin for a time and at a temperature sufficient to convert the polymer resin to a ceramic within the pores thereby forming a reinforced ceramic composite.

Claim 2

A method of forming a breakage and erosion-resistant ceramic liner for a part comprising the steps of: a) forming a liner of a cast monolithic ceramic material containing pores; b) filling the pores with a pre-ceramic polymer resin; and c) firing the liner filled with the pre-ceramic polymer resin for a time and at a temperature sufficient to convert the polymer resin to a ceramic within the pores thereby forming a reinforced ceramic composite.

Claim 6

A method of forming a metal part having a breakage and erosion resistant ceramic liner comprising the steps of: a) forming a metal part having a mating surface for receiving the liner; b) forming a liner of a cast monolithic ceramic material containing pores; c) filling the pores with a pre-ceramic polymer resin; d) firing the liner saturated with the pre-ceramic polymer resin for a time and at a temperature sufficient to convert the resin to a ceramic within the pores thereby forming a reinforced ceramic composite; and, e) bonding the ceramic liner to the mating surface of the metal part.

Claim 7

A method of forming a metal part having a breakage and erosion resistant ceramic liner comprising the steps of: a) forming a metal part having a mating surface for receiving the liner; b) forming a liner of a cast monolithic ceramic material containing pores; c) filling the pores with a pre-ceramic polymer resin; d) firing the liner saturated with the pre-ceramic polymer resin for a time and at a temperature sufficient to convert the resin to a ceramic within the pores thereby forming a reinforced ceramic composite; and, e) bonding the ceramic liner to the mating surface of the metal part.

Claim 11

A method of forming a metal part having a breakage resistant ceramic liner comprising the steps of: a) forming a liner of a cast monolithic ceramic material containing pores; b) filling the pores with a pre-ceramic polymer resin; c) firing the liner saturated with the pre-ceramic polymer resin for a time and at a temperature sufficient to convert the polymer resin to a ceramic within the pores thereby forming a reinforced ceramic composite; d) positioning the liner within a mold for the metal part with the mating surface of the liner facing into a portion of the mold to be occupied by metal forming the part; and, e) filling the mold with molten metal to form the part in combination with the liner.

Claim 12

A method of forming a metal part having a breakage resistant ceramic liner comprising the steps of: a) forming a liner of a cast monolithic ceramic material containing pores; b) filling the pores with a pre-ceramic polymer resin; c) firing the liner saturated with the pre-ceramic polymer resin for a time and at a temperature sufficient to convert the polymer resin to a ceramic within the pores thereby forming a reinforced ceramic composite; d) positioning the liner within a mold for the metal part with the mating surface of the liner facing into a portion of the mold to be occupied by metal forming the part; and, e) filling the mold with molten metal to form the part in combination with the liner.

Claim 16

A method of making a fiber reinforced ceramic matrix composite engine manifold comprising the steps of: a) forming a first preform in a shape of a lower portion of the manifold from reinforcing fibers employable in fiber reinforced ceramic matrix composites; b) placing the first preform in a cavity of a first mold having the shape of the lower portion of the manifold; c) forcing a liquid pre-ceramic polymer resin through the cavity to fill the cavity and saturate the first preform; d) heating the first mold for a time and at a temperature sufficient to transform the first preform saturated with the liquid pre-ceramic polymer resin to a first polymer composite part; removing the first polymer composite part from the mold; forming a second preform in a shape of an upper portion of the manifold from the reinforcing fibers; g) placing the second preform in a cavity of a second mold having the shape of the upper portion of the manifold; h) forcing the liquid pre-ceramic polymer resin through the cavity to fill the cavity and saturate the second preform; i) heating the second mold for a time and at a temperature sufficient to transform the second preform saturated with the liquid pre-ceramic polymer resin to a second polymer composite part; j) removing the second polymer composite part from the mold; k) fitting the first polymer composite part and the second polymer composite part together along mating edges to form the manifold as a hollow conduit-shaped part; i) firing the polymer composite manifold in an inert atmosphere for a time and at a temperature sufficient to transform the pre-ceramic polymer resin to a ceramic whereby the polymer composite manifold is transformed into a fiber reinforced ceramic matrix composite manifold and the upper portion and the lower portion are fused together along the mating edges; wherein the manifold is an exhaust manifold internally filled with a ceramic foam catalyst substrate structure and prior to said step (g) of placing the second preform in a cavity of a second mold having the shape of the upper portion of the manifold additionally including the steps of: f1) placing the first preform as part of a cavity-defining wall of the second mold; and, f2) placing the ceramic foam catalyst substrate structure in the first preform whereby the first preform and the ceramic foam catalyst substrate structure in combination form part of the cavity of the second wall.

Claim 17

A method of making a fiber reinforced ceramic matrix composite engine manifold comprising the steps of: a) forming a first preform in a shape of a lower portion of the manifold from reinforcing fibers employable in fiber reinforced ceramic matrix composites; b) placing the first preform in a cavity of a first mold having the shape of the lower portion of the manifold; c) forcing a liquid pre-ceramic polymer resin through the cavity to fill the cavity and saturate the first preform; d) heating the first mold for a time and at a temperature sufficient to transform the first preform saturated with the liquid pre-ceramic polymer resin to a first polymer composite part; removing the first polymer composite part from the mold; forming a second preform in a shape of an upper portion of the manifold from the reinforcing fibers; g) placing the second preform in a cavity of a second mold having the shape of the upper portion of the manifold; h) forcing the liquid pre-ceramic polymer resin through the cavity to fill the cavity and saturate the second preform; i) heating the second mold for a time and at a temperature sufficient to transform the second preform saturated with the liquid pre-ceramic polymer resin to a second polymer composite part; j) removing the second polymer composite part from the mold; k) fitting the first polymer composite part and the second polymer composite part together along mating edges to form the manifold as a hollow conduit-shaped part; i) firing the polymer composite manifold in an inert atmosphere for a time and at a temperature sufficient to transform the pre-ceramic polymer resin to a ceramic whereby the polymer composite manifold is transformed into a fiber reinforced ceramic matrix composite manifold and the upper portion and the lower portion are fused together along the mating edges; wherein the manifold is an exhaust manifold internally filled with a ceramic foam catalyst substrate structure and prior to said step (g) of placing the second preform in a cavity of a second mold having the shape of the upper portion of the manifold additionally including the steps of: f1) placing the first preform as part of a cavity-defining wall of the second mold; and, f2) placing the ceramic foam catalyst substrate structure in the first preform whereby the first preform and the ceramic foam catalyst substrate structure in combination form part of the cavity of the second wall.