Airfoil assembly and method of forming same
A composite component includes an inner core formed from a first composite material having discontinuous fibers. An outer sleeve is formed from a second composite material different from the first, and having continuous fibers. The outer sleeve generally surrounds and is bonded or otherwise connected to the inner core. The component is made by injecting or otherwise introducing thermoplastic fiber composite material including chopped or otherwise discontinuous fibers into a mold to form the inner core having a first portion with smooth surfaces and integrally joined to a second portion with bumps and ridges. The injected thermoplastic fiber composite material is cured and then removed from the mold. A layup including one or more surface plies of a thermoset continuous fiber composite material is then applied to the smooth first portion of the core. The surface plies then are compressed and cured in a mold.
1. A process for fabricating a partly-sleeved composite structure, the process comprising: introducing into a mold a thermoplastic fiber composite material including chopped or otherwise discontinuous fibers to form an inner core including a first smooth surface portion integrally joined with a second portion having a platform comprising bumps and ridges; curing the thermoplastic fiber composite material in the mold; removing the thermoplastic fiber composite material from the mold; applying over the first smooth portion of the inner core a layup including a surface ply of a thermoset continuous fiber composite material; and curing the surface ply in a mold to form a sleeve over the inner core; wherein the sleeve does not extend over the platform comprising the bumps and ridges.
2. A process as claimed in claim 1 , wherein the composite structure is an airfoil for a combustive power plant.
3. A process for fabricating an airfoil for a combustive power plant, the process comprising: introducing thermoplastic fiber composite material including chopped or otherwise discontinuous fibers into a mold to form the core and platforms of an airfoil assembly; curing the thermoplastic fiber composite material in the mold; removing the thermoplastic fiber composite material from the mold; applying to the core, without surrounding the platform, a layup including a surface ply of a thermoset continuous fiber composite material; and curing the surface ply in a mold.
4. A process for fabricating a partly-sleeved composite structure, the process comprising: introducing into a mold a thermoplastic short fiber composite material to form a unitary body including a smooth surfaced core and a platform joined to the core, the platform surfaces including bumps and ridges; curing the unitary body in the mold; removing the unitary body from the mold; applying over the core a layup including a surface ply of a thermoset continuous fiber composite material; and curing the surface ply in a mold to form a sleeve over the core; wherein the sleeve does not extend over the platform.