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A mixed gas containing a precursor gas, an additive gas and a carrier gas is supplied to a preform stored in an electric furnace, and silicon carbide is deposited by chemical vapor deposition or chemical vapor phase impregnation to form a film. The preform includes multiple fiber bundles, and the fi

A mixed gas containing a precursor gas, an additive gas and a carrier gas is supplied to a preform stored in an electric furnace, and silicon carbide is deposited by chemical vapor deposition or chemical vapor phase impregnation to form a film. The preform includes multiple fiber bundles, and the fiber bundles include multiple fibers. This heat-resistant composite material includes a ceramic fiber preform impregnated with silicon carbide, and producing the composite material involves a step in which silicon carbide is deposited between the fibers to integrate the fibers which configure the fiber bundles, and a step in which silicon carbide is deposited between the fiber bundles to integrate the fiber bundles. Hereby, uniformity of embedding and growth rate of the silicon carbide film are both attained.

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1. A method of manufacturing a heat-resistant composite material, the method comprising: treating a preform comprising a plurality of fiber bundles, each fiber bundle having a plurality of fibers, by:wrapping a woven fabric having a predetermined thickness around an outer circumference of the prefor

1. A method of manufacturing a heat-resistant composite material, the method comprising: treating a preform comprising a plurality of fiber bundles, each fiber bundle having a plurality of fibers, by:wrapping a woven fabric having a predetermined thickness around an outer circumference of the preform to provide a wrapped preform;depositing silicon carbide between the fibers of the wrapped preform to integrate the fibers constituting each fiber bundle to provide a fiber-integrated wrapped preform;removing the woven fabric from the fiber-integrated wrapped preform to provide a fiber-integrated preform; anddepositing silicon carbide between the fiber bundles of the fiber-integrated preform to integrate the fiber bundles,wherein said depositing silicon carbide between the fibers of the wrapped preform is accomplished by allowing precursor gas, additive gas, and carrier gas to flow in a reaction furnace accommodating the wrapped preform,wherein said depositing silicon carbide between the fiber bundles of the fiber-integrated preform is accomplished by allowing precursor gas, additive gas, and carrier gas to flow in a reaction furnace accommodating the fiber-integrated preform. 2. The method of manufacturing a heat-resistant composite material according to claim 1, wherein in said depositing silicon carbide between the fibers of the wrapped preform to integrate the fibers constituting each fiber bundle, the ratio C/C0 of concentration C of the precursor gas at the center of the fiber bundles to initial concentration C0 of the precursor gas supplied to the reaction furnace is in a range from 0.2 to 0.3. 3. The method of manufacturing a heat-resistant composite material according to claim 2, wherein the ratio C/C0 is in a range from 0.24 to 0.26. 4. The method of manufacturing a heat-resistant composite material according to claim 1, wherein in said depositing silicon carbide between the fibers of the wrapped preform to integrate the fibers constituting each fiber bundle, a growth temperature of the reaction furnace is in a range from 800 to 1000° C., and a total pressure of the precursor gas, additive gas, and carrier gas in the reaction furnace is in a range of 4 to 6 Torr. 5. The method of manufacturing a heat-resistant composite material according to claim 4, wherein the growth temperature is in a range from 850 to 950° C., and the total pressure is in a range of 4.5 to 5.5 Torr. 6. The method of manufacturing a heat-resistant composite material according to claim 1, wherein in said depositing silicon carbide between the fiber bundles of the fiber-integrated preform to integrate the fiber bundles, the ratio C/C0 of concentration C of the precursor gas at the center of the fiber-integrated preform to the initial concentration C0 of the precursor gas supplied to the reaction furnace is in a range from 0.2 to 0.3. 7. The method of manufacturing a heat-resistant composite material according to claim 6, wherein the ratio C/C0 is in a range from 0.24 to 0.26. 8. The method of manufacturing a heat-resistant composite material according to claim 1, wherein in said depositing silicon carbide between the fiber bundles of the fiber-integrated preform to integrate the fiber bundles, a growth temperature of the reaction furnace is in a range from 800 to 1000° C., and a total pressure of the precursor gas, additive gas, and carrier gas in the reaction furnace is in a range of 5 to 110 Torr. 9. The method of manufacturing a heat-resistant composite material according to claim 8, wherein the growth temperature is in a range from 850 to 950° C., and the total pressure is in a range of 5 to 105 Torr. 10. The method of manufacturing a heat-resistant composite material according to claim 1, wherein the woven fabric is wound around the outer circumference of the preform to provide the wrapped preform. 11. The method of manufacturing a heat-resistant composite material according to claim 1, wherein the preform is made of woven fabric, and the woven fabric is made of the same material as that of the preform. 12. The method of manufacturing a heat-resistant composite material according to claim 1, wherein the precursor gas used to deposit silicon carbide between the fibers of the wrapped preform and the precursor gas used to deposit silicon carbide between the fiber bundles of the fiber-integrated preform each comprise at least one of methyltrichlorosilane, dimethyldichlorosilane, tetramethylsilane, and trimethylchlorosilane. 13. The method of manufacturing a heat-resistant composite material according to claim 12, wherein the precursor gas used to deposit silicon carbide between the fibers of the wrapped preform comprises methyltrichlorosilane, andthe precursor gas used to deposit silicon carbide between the fiber bundles of the fiber-integrated preform comprises at least one of dimethyldichlorosilane, tetramethylsilane, and trimethylchlorosilane. 14. The method of manufacturing a heat-resistant composite material according to claim 1, wherein the carrier gas used to deposit silicon carbide between the fibers of the wrapped preform, and the carrier gas used to deposit silicon carbide between the fiber bundles of the fiber-integrated preform, each comprise at least one of hydrogen, nitrogen, helium, and argon. 15. The method of manufacturing a heat-resistant composite material according to claim 1, wherein the additive gas used to deposit silicon carbide between the fibers of the wrapped preform, and the additive gas used to deposit silicon carbide between the fiber bundles of the fiber-integrated preform, each comprise at least one of hydrogen chloride, monochloromonomethylsilane, methyldichlorosilane, methyltrichlorosilane, dimethylmonochlorosilane, dimethyldichlorosilane, trimethylmonochlorosilane, monochlorosilane, dichlorosilane, trichlorosilane, tetrachlorosilane, chlorodisilane, dichlorodisilane, hexachlorodisilane, octachlorotrisilane, monochloromethane, dichloromethane, chloroform, tetrachloromethane, monochloroacetylene, dichloroacetylene, monochloroethylene, dichloroethylene, trichloroethylene, tetrachloroethylene, monochloroethane, dichloroethane, trichloroethane, tetrachloroethane, pentachloroethane, hexachloroethane, monochloropropane, dichloropropane, trichloropropane, tetrachloropropane, pentachloropropane, hexachloropropane, heptachloropropane, octachloropropane, and chlorine molecules. 16. The method of manufacturing a heat-resistant composite material according to claim 15, wherein the additive gas used to deposit silicon carbide between the fibers of the wrapped preform, and the additive gas used to deposit silicon carbide between the fiber bundles of the fiber-integrated preform, comprises hydrogen chloride. 17. The method of manufacturing a heat-resistant composite material according to claim 1, wherein the precursor gas used to deposit silicon carbide between the fibers of the wrapped preform, and the precursor gas used to deposit silicon carbide between the fiber bundles of the fiber-integrated preform, comprises methyltrichlorosilane, and the carrier gas used to deposit silicon carbide between the fibers of the wrapped preform, and the carrier gas used to deposit silicon carbide between the fiber bundles of the fiber-integrated preform, comprises hydrogen. 18. The method of manufacturing a heat-resistant composite material according to claim 17, wherein a molar ratio of hydrogen to methyltrichlorosilane is in a range from 1.5 to 2.5. 19. The method of manufacturing a heat-resistant composite material according to claim 18, wherein the molar ratio of hydrogen to methyltrichlorosilane is in a range from 1.9 to 2.1.