C - Chemistry – Metallurgy – 08 – K
Patent
C - Chemistry, Metallurgy
08
K
C08K 3/04 (2006.01)
Patent
CA 2730910
Disclosed herein is a composite part for an airplane engine comprising polymer selected from polyimide, polyamide-imide, polyether imides, polybenzimidazole, or blends thereof, and carbonaceous filler, which in combination provides thermal stability and wear resistance. Optionally, the composite may comprise particulate.
La présente invention concerne une pièce composite pour un moteur d'avion comprenant un polymère choisi parmi le polyimide, le polyamide-imide, les polyéther-imides, le polybenzimidazol, ou des mélanges de ceux-ci, et une charge carbonée qui, en combinaison, génère une stabilité thermique et une résistance à l'usure. En option, le composite peut comprendre une particule.
Dauer John C.
Krizan Timothy D.
Prellwitz Martin W.
E. I. Du Pont de Nemours And Company
Torys Llp
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