General Electric Company

John A Ravenhall

Thomas Carl Mesing

Bruce Clark Busbey

Brian Michael Davis

Jack W Baldwin

A fiber reinforced composite article is made by providing a plurality of layers of first, substantially dry, unimpregnated reinforcing fibers, sometimes called in-plane fibers. Such layers are stacked into a preform of a stack of layers. While in the dry, unimpregnated condition, a plurality of spaced apart second reinforcing members are inserted into the preform at an angle, for example transversely, to the stack of layers. In this condition, the preform is impregnated with a matrix about the first reinforcing fibers and the second reinforcing members. The article product comprises the plurality of stacked layers of the first reinforcing fibers and the plurality of the spaced apart second reinforcing members disposed beside or adjacent the first reinforcing fibers, with a substantially solid matrix disposed about the reinforcing fibers and members.

Method for making a fiber reinforced composite article and product

A preferred embodiment of said present invention is a gas turbine engine blade root shim for use between a composite blade root and a wall of a slot for receiving the root in a rotor of the engine. An exemplary embodiment of the shim includes a longitudinally extending base having distal first and second transversely spaced apart ends, first and second longitudinally extending legs acutely angled inwardly towards the base from the first and second ends, and first and second low coefficient of friction coatings on first and second outwardly facing surfaces of the first and second legs, respectively. Among coatings suitable for use in the present invention are polytetrafluoroethylene powder dispersed in a resin binder and other coatings which include polytetrafluoroethylene.

Composite blade root attachment

A platform for a turbofan gas turbine engine that does not limit the rotation capability of adjacent fan blades in the event one of the fan blades is impacted by a foreign object. The platform includes a structural body portion and an integrally formed flowpath surface portion. The structural body portion has a contour that matches that of the adjacent fan blades. The flowpath surface portion defines a pair of wings that extend laterally beyond the structural body portion. The wings are frangible so as to break off if an adjacent fan blade rotates in response to an ingestion event. The platform is made from a composite material using a resin transfer molding process.

Growing community of inventors

Hamilton, OH, United States of America

John A Ravenhall