The Boeing Company

Mcdonnell Douglas Corporation

Creed E Blevins

Michael Leslie Hand

Michael J Robinson

Robert A DiChiara

Shu-Yau Wu

Francis J Samalot Rivera

John S Mills

Ben YoungSon Won

Marvin Luke

Orlando Torres

Daniel Madrid Ortega

Luisa F Gutierrez

Charles Douglas Hall

A heat sink for use in induction welding includes a number of tiles, wherein the tiles are electrically non-conductive and have a thermal diffusivity of greater than about 25 mm2/sec. A joint flexibly joins the tiles together.

Induction welding using a heat sink and/or cooling

A heat sink for use in induction welding includes a flexible backing and a number of tiles disposed on the flexible backing in a single layer, wherein the tiles are electrically non-conductive and thermally conductive.

A low pressure duct configured to channel a gas within a structure includes a tubular body formed from a polymer foam material, and a first plurality of strands adhered to a surface of the tubular body along a plurality of paths. The plurality of paths includes a first set of paths oriented longitudinally along the tubular body. The first set of paths are spaced apart from each other around a circumference of the tubular body. The plurality of paths also includes a second set of paths oriented circumferentially around the tubular body. The second set of paths are spaced apart longitudinally along the tubular body.

Crack-resistant polymer foam ducts and method of installing same

A composite resin tank includes a wall joined to a dome along a joint. A softening strip is located in the joint.

Composite tank having joint with softening strip

A composite resin tank includes a wall joined to a dome along a joint. A softening strip is used to control stress in the joint.

Method of making a device for controlling stress in joints at cryogenic temperatures

Method of making a composite tank having joint with softening strip

A temporary control fin stop system employs a housing coupled to a vehicle. At least one tang is coupled to the housing and positioned to engage a trailing edge of a fin. The tang is ablatively erodible at a predetermined temperature induced by a flight profile of the vehicle to allow unconstrained motion of the fin.

Passive control fin stops for air launched boosted (two stage) high speed vehicles

A method for embedding piezoelectric ceramic transducers in thermoplastic composites. The piezoelectric ceramic transducer to be embedded in a graphite/PEEK composite is first bonded with two fine silver wires for electrical connection, one on each major surface. The bonding agent is a high temperature conductive adhesive compound, such as a silver/glass frit. The fusing of the frit bonding agent is done in an over at a high temperature (i.e. 600.degree. F. or higher) for 5 to 10 minutes. Bonds are applied at several discrete spots on the zig zag wire which relieves thermal stresses induced during cooling due to a mismatch of the coefficient of thermal expansion between the ceramic material and the wire. After the connecting wires are attached, the wires and transducer are wrapped with several plies of insulating glass/PEEK cloth to prevent electrical shorting between the two silver wires through the graphite/PEEK host. The insulating glass cloth and tube sheaths are impregnated with PEEK resin to improve the bonding to the surrounding structural materials. To compensate for non-uniform stresses and prevent the composite plate from warping or distorting during the consolidation process, a compensating layer made from several plies of the same glass/PEEK cloth used to wrap the ceramic transducer is placed under the cutouts on the opposite side of the plate/ply structure. When the consolidation is completed, the piezoelectric ceramic transducer is electrically poled with a high electric field (dependent on the specific ceramic material) at a temperature of around 200 to 350 degrees Fahrenheit, which repoles the ceramic transducer.

Method for embedding piezoelectric transducers in thermoplastic

This invention consists of a method for embedding piezoelectric ceramic transducers in thermoplastic composites. The piezoelectric ceramic transducer to be embedded in a graphite/PEEK composite is first bonded with two fine silver wires for electrical connection, one on each major surface. The bonding agent is a high temperature conductive adhesive compound, such as a silver/glass frit. The fusing of the frit bonding agent is done in an over at, a high temperature (i.e. 600.degree. F. or higher) for 5 to 10 minutes. Bonds are applied at several discrete spots on the zig zag wire which relieves thermal stresses induced during cooling due to a mismatch of the coefficient of thermal expansion between the ceramic material and the wire. After the connecting wires are attached, the wires and transducer are wrapped with several plies of insulating glass/PEEK cloth to prevent electrical shorting between the two silver wires through the graphite/PEEK host. The insulating glass cloth and tube sheaths are impregnated with PEEK resin to improve the bonding to the surrounding structural materials. To compensate for non-uniform stresses and prevent the composite plate from warping or distorting during the consolidation process, a compensating layer made from several plies of the same glass/PEEK cloth used to wrap the ceramic transducer is placed under the cutouts on the opposite side of the plate/ply structure. When the consolidation is completed, the piezoelectric ceramic transducer is electrically poled with a high electric field (dependent on the specific ceramic material) at a temperature of around 200 to 350 degrees Fahrenheit, which repoles the ceramic, transducer.

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Aliso Viejo, CA, United States of America

Creed E Blevins