General Electric Company

Curt Brian Curtis

Ming Xie

Warren Rosal Ronk

Lee Alan Blanton

Michael Braley

Scott Roger Finn

Frank Worthoff

Stephen Mark Whiteker

Michael Dominic Schulte

Edward Atwood Rainous

Qi Zhu

Randall Maurice Prather

Daniel Elmer King

Brian Dominic Stephens

Eric Joseph Aho

George Han

Deepali Bhate

Lori Renee McGrath

Jeffrey Lawrence Sulikowski

Paul Edward Wilkerson

Ernest R Broughton

Scott Alan Garten

James Timothy Sanchez

Lori Renee Mcgrath

Collar support assemblies are provided. For example, a collar support assembly for an airfoil comprises a collar that includes a first surface shaped complementary to a fillet of the airfoil and a planar second surface. The first surface is disposed adjacent the fillet of the airfoil. The collar support assembly further comprises a shim material disposed between the second surface and an airfoil support structure and a filler material inserted between the first surface and the fillet of the airfoil to provide a tight fit between the collar and the airfoil. In other embodiments, the collar support assembly comprises a pair of collars and supports an airfoil doublet. The airfoil doublets may be part of an outlet guide vane assembly of a gas turbine engine, and methods for assembling outlet guide vane assemblies also are provided.

Collar support assembly for airfoils

Processes for producing near net-shape panels and panels formed thereby. The processes include forming a preform to comprise a stack of multiple plies that contain an uncured expandable foam material. The preform has regions that differ from each other by the number and/or volume of the plies therein. The preform and its plies are then cured within a restricted volume to produce a near net-shape panel. The curing step causes the expandable foam material to expand, and the restricted volume is sized so that the number and volume of the plies within the regions of the preform cause zones within the panel to have different densities and/or thicknesses.

Near net-shape panels and processes therefor

Articles having substantially cylindrical bodies including a plurality of circumferential layers, each layer having at least one ply of material, the material comprising a weave fabric, a non-crimp fabric, or a combination thereof.

Substantially cylindrical composite articles and fan casings

A containment case comprises a composite core, with an inner surface, and at least one ceramic layer integrated with the composite core. The at least one ceramic layer is bonded to the inner surface of the composite core with a resin. In another embodiment, a containment case comprises a composite core, with an inner surface, and a hybrid material comprising at least one ceramic material and at least one non-ceramic material. The hybrid material is disposed on the inner surface of the composite core. The hybrid material is bonded to the inner surface of the composite core with a resin. A method of fabricating a containment case includes the steps of disposing one or more layers of ceramic fabric on an inner surface of a composite core, infusing the composite core and the one or more layers of ceramic fabric with resin, and curing the resin.

Containment cases and method of manufacture

Methods for making articles having a substantially cylindrical body including providing a substantially cylindrical tool, providing at least one ply of a material, the material being a weave fabric, a non-crimp fabric, or a combination thereof, wrapping the at least one ply of material about the tool to produce an article preform having a plurality of circumferential layers, applying a resin to the article preform, and curing the article preform to produce an article having a substantially cylindrical body.

Methods for making substantially cylindrical articles and fan casings

Methods for making a structure having an integral mounting flange involving providing a primary composite structure having a circumference, applying at least one circumferentially oriented core fiber about the circumference of the primary composite structure, applying at least one layer of attachment fibers to operably connect the core fiber to the primary composite structure about the circumference to obtain an integral mounting flange preform, and curing the mounting flange preform to obtain an integral mounting flange.

Methods for making structures having mounting flanges

Tethered flange corners including at least one ply of barrier fibers and at least one fiber tow wrapped about the barrier fibers. Also included are flanges having a tethered corner containing at least one ply of barrier fibers, at least one fiber tow wrapped about the barrier fibers, at least one ply of filler fibers applied over the fiber tow, and at least one ply of flange fibers applied over the filler fibers. Additionally included are articles incorporating a composite structure having a flange with a tethered corner containing at least one ply of barrier fibers and at least one fiber tow wrapped about the barrier fibers.

Tethered corners and flanges and articles comprising the same

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Nesbit, MS, United States of America

Curt Brian Curtis