Stock material or miscellaneous articles – Hollow or container type article – Polymer or resin containing
Patent
1982-12-30
1984-09-04
Bell, James J.
Stock material or miscellaneous articles
Hollow or container type article
Polymer or resin containing
156169, 156173, 156175, 156184, 156195, 428105, 428108, 428109, 428110, 428113, 428377, 428408, 428413, B32B 512
Patent
active
044697309
ABSTRACT:
A composite base structure (70) and end fitting (26) are secured together by a composite joint to form a graphite-epoxy composite nacelle diagonal strut (20). The elongated base structure (70) has a wall (72) formed of a cured epoxy reinforced with layers of graphite fibers (100, 102, 104, 106) extending in elongated and transverse directions. The layers of fibers in the elongated direction (100, 104) and transverse direction (102, 106) extend onto a large diameter end (52) of a conical end portion (46) of an end fitting (26) and terminate on the conical portion adjacent a small diameter end (60). The layers of the elongated and transverse fibers (100, 102, 104, 106) are interlayered with layers (110, 112, 114, 116, 118) of graphite fibers generally circumferentially wrapped on the conical portion (46), the layers on the conical portion being impregnated with the cured epoxy. At the small diameter end of the conical portion (46) a transverse shoulder (60) extends outwardly and the fibers on the conical portion abut the shoulder.
A method of joining an end fitting (26) to a fiber reinforced base structure (70) includes forming an elongated base structure (70) by applying layers of elongated fibers (100, 104) in the elongated or axial direction and applying layers of fibers (102, 106) in a transverse direction on a removable mandrel (90). The layers of fibers in the elongated and transverse directions are extended onto large diameter end of a conical end portion of an end fitting of large diameter end (52). Layers (110, 112, 114, 116, 118) are circumferentially wrapped on the conical portion so as to be interlayered with the layers of elongated and transverse fibers, the fibers being impregnated with an epoxy, and the epoxy being cured. The mandrel (90) is removed after the epoxy is cured.
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Bell James J.
Heberer Eugene O.
The Boeing Company
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