General Electric Company

Other

Formica Corporation

Robert Paul Fairbanks

Stephen Mark Whiteker

Lee Alan Blanton

Richard Thomas Price

Gregory Joseph Meibers

Warren Rosal Ronk

Matthew Bernard Buczek

Kevin Francis O'Brien

Kurt A Weiss

Jeremy P Miller

Charles M Mulcahy

Kenneth Allan Nilsson

Merrill Glos

William F Whetstone

A catheterization procedure training apparatus operable to provide a user training on the delivery of a catheterization process wherein the apparatus further allows the utilization of interventional devices. The catheterization procedure training apparatus includes a tubing network being hollow and fluidly coupled wherein the tubing network is configured to be sized and shaped so as to physically be proportionally representative of at least a portion of the blood vessels within a human circulatory system. A ventricle chamber is operably coupled to the tubing network. The tubing network further includes at least one opening having a union wherein the union is configured to be operably coupled to an exchangeable insertion point adapter. The exchangeable insertion point adapter includes a stem portion and a wall portion integrally formed and is configured to provide repetitive sealable use of a needle therethrough.

Catheterization procedure training apparatus

A method for fabricating a reinforced matrix composite comprising the step of providing a composite preform having a fibrous structure and applying matrix material onto the preform in locations along the preform. A barrier material is applied to at least a portion of the coated preform to direct the flow of matrix material into the preform. The composite preform is heated to a temperature sufficient to render the matrix material viscous and insufficient to cure the matrix material. The pressure to the interior of the composite preform is reduced, while the pressure to the barrier material is increased. The temperature is maintained to flow the matrix material into the composite preform and to force gases from the fibrous structure. The composite preform is then cured and cooled to form a reinforced matrix composite having a low void content and a substantially uniform matrix distribution.

Method for fabricating reinforced composite materials

A reinforced matrix composite containment duct for gas turbine engines comprising a reinforced matrix composite containment duct having high strength integral flanges and pre-stressed reinforcing fibers, the reinforced matrix composite having uniform distribution of matrix material; and the reinforced matrix composite having less than or equal to 2.5% void space.

Reinforced matrix composite containment duct

A mold tool for forming a reinforced matrix composite part for a gas turbine engine, comprising a body. The body comprises a body surface capable of receiving a first portion of a composite preform. A first endplate and second endplate are attached to the body and include a substantially planar surface disposed perpendicular to the body surface. A first and second set of plates are attached to the first and second endplate adjacent to the body surface and have a geometries that includes a first and second cavity bounded by the first and second plate and first and second endplate. The first and second cavities have a volume sufficient to receive a second portion of a composite preform. The second cavity is in fluid communication with the first cavity, which is in fluid communication with a vacuum source.

Apparatus for fabricating reinforced composite materials

A deep embossed high pressure decorative laminate having a plurality of integral tiles with various surface textures bordered by deep embossed portions. Each tile of the laminate has a peripheral thickness greater than the thickness of the non-peripheral portions of the tile. Preferably, each tile has a concave profile along its upper surface when viewed in cross section. A method of producing artwork necessary for the deep embossed high pressure decorative laminate of the present invention comprises assembling a first layer of fibrous sheets impregnated with a thermosetting resin, a second layer comprising a plurality of adjacent tiles comprising a plurality of fibrous sheets impregnated with a thermosetting resin, wherein the tiles were previously pressed and heated, and a third layer comprising a plurality of shims. The assembly is then pressed and heated against a rigid substrate whereby the second layer forms a substantially convex shape on the upper surface of each tile, thus imparting substantially concave impressions on the first layer. The first layer is subsequently removed from the second and third layers, and grooves are formed in the first layer, preferably by machining.

Deep embossed tile design postformable high pressure decorative laminate and method for producing same

A plurality of layers of nonfully cured composite material are joined by a unique combination of steps including debulking and precuring the layers using vacuum followed by pressure and heating. Then spaced apart holes through the layers are generated with a pointed tool using ultrasonic energy which at least softens and smooths the hole wall. The layers are stitched through the holes prior to final curing.

Method for joining composite materials

A method for joint reinforcement of dissimilar materials and products made by such method. The method includes the steps of spray coating a contact adhesive on the contact area between a substrate and covering material sheets, providing a reinforcement interleave of fibrous glass between the joint area of covering material sheets and the substrate, and applying a second adhesive on the reinforcement interleave such that the second adhesive is extruded through the seam when the covering material sheets are applied to the substrate.

Method for joint reinforcement of dissimilar materials

The present invention relates to a novel composite adhesive used to adhere coating materials onto a substrate wherein the substrate material and the coating material have significantly different expansion properties, e.g., thermoplastic coating materials onto cellulose based substrate materials. The composite adhesive comprises both a rigid adhesive such as an epoxy or acrylic and a laminating adhesive such as a rubber based contact cement. In a preferred embodiment of the invention, a spline material is also rigidly adhered to the coating material so as to reinforce the bond between substrate and coating, especially where two pieces of coating material are attached at a seam. In another preferred embodiment the composite adhesive and/or spline material is used in preparing composite articles such as counters, sinks, furniture, profile edging, chemical resistant lab tops, showers, etc.

Growing community of inventors

Cincinnati, OH, United States of America

Robert Paul Fairbanks