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A composite transmission housing includes resin transfer molding or vacuum assisted resin transfer molding manufacturing processes combined with discontinuous fiber preforms. The preforms are assembled in a prepared injection and cure mold with additional details and fillers. The preforms are constr

A composite transmission housing includes resin transfer molding or vacuum assisted resin transfer molding manufacturing processes combined with discontinuous fiber preforms. The preforms are assembled in a prepared injection and cure mold with additional details and fillers. The preforms are constructed such that the preforms are assembled into the mold in a specific order to assure proper arrangement. Using a combination of vacuum and pressure, a resin is injected into the mold to completely infuse the assembled preforms. At completion, the mold is heated to the resin cure temperature and held at this temperature for sufficient time to insure complete cure.

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1. A composite airframe structure comprising: a resin transfer molded composite transmission housing formed of a multiple of discontinuous fiber preforms, each of said multiple of discontinuous fiber preforms formed of randomly-oriented fibers, said resin transfer molded composite transmission housi

1. A composite airframe structure comprising: a resin transfer molded composite transmission housing formed of a multiple of discontinuous fiber preforms, each of said multiple of discontinuous fiber preforms formed of randomly-oriented fibers, said resin transfer molded composite transmission housing having at least two adjacent discontinuous fiber preforms with a continuous fiber filler material which interfaces with said at least two adjacent discontinuous fiber preforms, said continuous fiber filler material formed of an oriented fiber material. 2. The structure as recited in claim 1, wherein said transmission housing comprises an upper transmission housing and a lower transmission housing. 3. The structure as recited in claim 1, wherein at least one of said discontinuous fiber preforms comprise a beehive preform. 4. The structure as recited in claim 1, wherein at least one of said discontinuous fiber preforms comprise a rib preform. 5. The structure as recited in claim 1, wherein at least one of said discontinuous fiber preforms comprise a bearing build-up preform. 6. The structure as recited in claim 1, wherein said continuous fiber filler material is between said at least two adjacent discontinuous fiber preforms. 7. The structure as recited in claim 1, wherein said discontinuous fiber preforms comprise over 65 percent of said resin transfer molded composite transmission housing by weight. 8. The structure as recited in claim 1, further comprising an insert which forms an integral part of at least one of said multiple of discontinuous fiber preforms. 9. The structure as recited in claim 1, wherein said at least two adjacent discontinuous fiber preforms are interleaved. 10. The structure as recited in claim 1, wherein at least one of said multiple of discontinuous fiber preforms are formed by a Programmable Powder Preform Process for Aerospace (P4A) process. 11. A main rotor transmission housing assembly for a rotary-wing aircraft comprising: an upper transmission housing formed of a multiple of discontinuous fiber preforms having at least two adjacent discontinuous fiber preforms each of said multiple of discontinuous fiber preforms formed of randomly-oriented fibers, said upper transmission housing having at least two adjacent discontinuous fiber preforms with a continuous fiber filler material which interfaces with said at least two adjacent discontinuous fiber preforms, said continuous fiber filler material formed of an oriented fiber material; anda lower transmission housing formed of said chopped fiber having a multiple of discontinuous fiber preforms having at least two adjacent discontinuous fiber preforms, each of said multiple of discontinuous fiber preforms formed of randomly-oriented fibers, said lower transmission housing having at least two adjacent discontinuous fiber preforms with a continuous fiber filler material which interfaces with said at least two adjacent discontinuous fiber preforms, said continuous fiber filler material formed of an oriented fiber material, said lower transmission housing matable with said upper transmission housing. 12. The assembly as recited in claim 11, further comprising a sump housing mateable with said lower transmission housing, said sump housing formed of a multiple of discontinuous fiber preforms having at least two adjacent discontinuous fiber preforms each of said multiple of discontinuous fiber preforms formed of randomly-oriented fibers, said sump housing having at least two adjacent discontinuous fiber preforms with a continuous fiber filler material which interfaces with said at least two adjacent discontinuous fiber preforms, said continuous fiber filler material formed of an oriented fiber material. 13. A composite airframe structure comprising: a resin transfer molded composite transmission housing formed of a multiple of discontinuous fiber performs, each of said multiple of discontinuous fiber preforms formed of randomly-oriented fibers, said resin transfer molded composite transmission housing having at least two discontinuous fiber preforms with a continuous fiber filler material which interfaces with said at least two discontinuous fiber preforms, said continuous fiber filler material formed of an oriented fiber material, said multiple of discontinuous fiber performs forming over 65 percent of said resin transfer molded composite transmission housing by weight.