Ceramic matrix composite tooling for chemical vapor infiltration process
A tooling assembly suitable for use in infiltrating a fibrous preform comprises a first perforated plate having an outer surface and an oppositely disposed inner surface defining a plate thickness therebetween, and a plurality of tapered holes extending through the thickness. Each hole of the plurality of tapered holes has a first diameter at the outer surface and a second diameter at the inner surface, and the first diameter is greater than the second diameter.
1. A tooling assembly suitable for use in infiltrating a fibrous preform, the tooling assembly comprising:
a plurality of perforated plates, each of the plurality of perforated plates formed from graphite and comprising:
an outer surface and an oppositely disposed inner surface defining a plate thickness therebetween; and
a plurality of tapered holes extending through the thickness;
wherein the tooling assembly is configured to enclose the fibrous preform such that the inner surface of each of the plurality of perforated plates faces the fibrous preform and to maintain a shape of the fibrous preform during a chemical vapor infiltration process;
wherein each hole of the plurality of tapered holes has a first diameter at the outer surface and a second diameter at the inner surface; and
wherein the first diameter is greater than the second diameter.
2. The tooling assembly of claim 1 , wherein each of the plurality of perforated plates has a planar geometry.
3. The tooling assembly of claim 1 , wherein the first diameter is 1.1 to 4 times greater than the second diameter.
4. The tooling assembly of claim 1 , wherein each hole of the plurality of tapered holes has a frustoconical cross-sectional geometry.
5. The tooling assembly of claim 4 , wherein each hole of the plurality of tapered holes comprises a continuous linear sidewall extending between the outer surface and the inner surface of the first perforated plate.
6. The tooling assembly of claim 1 , wherein each hole of the plurality of tapered holes has a stepped cross-sectional geometry.
7. The tooling assembly of claim 6 , wherein each hole of the plurality of tapered holes comprises a sidewall extending between the outer surface and the inner surface of the first perforated plate, and wherein the sidewall comprises a first shoulder portion.
8. The tooling assembly of claim 7 , wherein the sidewall comprises a second shoulder portion.
9. The tooling assembly of claim 1 , wherein the thickness of each of the plurality of perforated plates ranges from 0.25 in (6.35 mm) to 1.0 in (25.4 mm).
10. The tooling assembly of claim 1 , wherein each of the plurality of perforated plates has a geometry complimentary to a geometry of the fibrous preform.
11. A method of forming a tooling assembly suitable for use in infiltrating a fibrous preform, the method comprising:
forming a plurality of perforated plates from graphite, each of the plurality of perforated plates comprising:
an outer surface and an oppositely disposed inner surface defining a plate thickness therebetween; and
a plurality of tapered holes extending through the thickness;
wherein the tooling assembly is configured to enclose the fibrous preform such that the inner surface of each of the plurality of perforated plates faces the fibrous preform and wherein each of the plurality of perforated plates has a geometry complimentary to a geometry of the fibrous preform;
wherein each hole of the plurality of tapered hole has a first diameter at the outer surface and a second diameter at the inner surface; and
wherein the first diameter is greater than the second diameter.
12. The method of claim 11 , wherein forming the plurality of perforated plates comprises forming each hole of the plurality of tapered holes using a drilling technique.
13. The method of claim 12 , wherein each hole of the plurality of tapered holes comprises a continuous linear sidewall extending between the outer surface and the inner surface of the first perforated plate.
14. The method of claim 12 , wherein forming the plurality of perforated plates further comprises counterboring each hole.
15. The method of claim 14 , wherein each hole of the plurality of tapered holes comprises a sidewall extending between the outer surface and the inner surface of the first perforated plate, and wherein the sidewall comprises a first shoulder portion.
16. The method of claim 15 and further comprising: further counterboring each hole such that the sidewall comprises a second shoulder portion.
17. A tooling assembly suitable for use in infiltrating a fibrous preform, the tooling assembly comprising:
a plurality of perforated plates, each perforated plate formed from graphite and comprising:
an outer surface and an oppositely disposed inner surface defining a plate thickness therebetween; and
a plurality of tapered holes extending through the thickness;
wherein the tooling assembly is configured to enclose the fibrous preform such that the inner surface of each of the plurality of perforated plates faces the fibrous preform, and wherein each of the plurality of perforated plates has a geometry complimentary to a geometry of the fibrous preform;
wherein each hole of the plurality of tapered holes has a first diameter at the outer surface and a second diameter at the inner surface;
wherein the first diameter is greater than the second diameter; and
wherein for at least one of the plurality of perforated plates, each hole of the plurality of tapered holes has a stepped cross-sectional geometry.