| CPC F16D 65/126 (2013.01) [B29C 70/54 (2013.01); B29C 70/68 (2013.01); C04B 35/62873 (2013.01); C04B 35/62884 (2013.01); C04B 35/83 (2013.01); C23C 16/045 (2013.01); F16D 69/023 (2013.01); B29K 2307/04 (2013.01); B29K 2707/04 (2013.01); B29K 2709/02 (2013.01); B29L 2031/16 (2013.01); C04B 2235/422 (2013.01); C04B 2235/5248 (2013.01); C04B 2235/5252 (2013.01); C04B 2235/614 (2013.01); F16D 2065/1328 (2013.01); F16D 2200/0047 (2013.01); F16D 2200/0065 (2013.01); F16D 2200/0091 (2013.01)] | 4 Claims |

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1. A method of making a carbon fiber-carbon matrix composite part, comprising:
densifying a fibrous preform by chemical vapor infiltration (CVI) to form a densified fibrous preform;
forming a first opening in a first wear surface of the densified fibrous preform; and
inserting a first wear plug in the first opening, wherein the first wear plug includes:
a graphite rod;
a binder, and
a first wear particulate, the first wear particulate including at least one of graphite powder, a mixture of graphite powder and ceramic powder, or carbon pitch particulate.
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