Abstract: A soundboard for a musical instrument is disclosed the soundboard having at least one layer of material. In some embodiments the material comprising carbon fiber, fibrous laminate material, resin or a plastic matrix and combinations thereof. At least one bracing structure is engaged to the at least one layer of material. The at least one bracing structure comprising at least one layer of honeycomb or shaped core and at least one sheet of material bonded to the honeycomb or shaped core.

Abstract: A soundboard for a musical instrument is disclosed the soundboard having at least one layer of material. In some embodiments the material comprising carbon fiber, fibrous laminate material, resin or a plastic matrix and combinations thereof. At least one bracing structure is engaged to the at least one layer of material. The at least one bracing structure comprising at least one layer of honeycomb or shaped core and at least one sheet of material bonded to the honeycomb or shaped core.

Abstract: A stringed musical instrument comprises a bridge that receives a plurality of strings. The bridge comprises at least one internal pocket. In some embodiments, the bridge comprises a plurality of internal pockets.

Abstract: A soundboard for a musical instrument is disclosed the soundboard having at least one layer of material. In some embodiments the material comprising carbon fiber, fibrous laminate material, resin or a plastic matrix and combinations thereof. At least one bracing structure is engaged to the at least one layer of material. The at least one bracing structure comprising at least one layer of honeycomb or shaped core and at least one sheet of material bonded to the honeycomb or shaped core.

Abstract: A stringed musical instrument comprises a bridge that receives a plurality of strings. The bridge comprises at least one internal pocket. In some embodiments, the bridge comprises a plurality of internal pockets.

Abstract: A soundboard for a musical instrument is disclosed the soundboard having at least one layer of material. In some embodiments the material comprising carbon fiber, fibrous laminate material, resin or a plastic matrix and combinations thereof. At least one bracing structure is engaged to the at least one layer of material. The at least one bracing structure comprising at least one layer of honeycomb or shaped core and at least one sheet of material bonded to the honeycomb or shaped core.

Abstract: A stringed musical instrument comprises a bridge that receives a plurality of strings. The bridge comprises at least one internal pocket. In some embodiments, the bridge comprises a plurality of internal pockets.

Abstract: A stringed musical instrument comprises a bridge that receives a plurality of strings. The bridge comprises at least one internal pocket. In some embodiments, the bridge comprises a plurality of internal pockets.

Abstract: A stringed musical instrument has a molded sound box and neck where the sound box is formed of between 20% to 60% carbon fibers, or other suitable fibers, and a polymeric resin or binder. The composition of materials utilized in the sound box is selected to increase stiffness and to control the tone of the instrument. The sound box includes an adjustable attachment mechanism having a pivot which is used to secure the neck to the sound box. The sound box includes a molded bracing structure having a plurality of braces and a molded bridge having a plurality of pockets which are used to enhance the structure for the sound box and provide a desired tone quality for the stringed instrument. The neck may include a molded neck insert and a molded fingerboard which are used to enhance the stiffness and stability of the neck.

Abstract: A stringed musical instrument has a molded sound box and neck where the sound box is formed of between 20% to 60% carbon fibers, or other suitable fibers, and a polymeric resin or binder. The composition of materials utilized in the sound box is selected to increase stiffness and to control the tone of the instrument. The sound box includes an adjustable attachment mechanism having a pivot which is used to secure the neck to the sound box. The sound box includes a molded bracing structure having a plurality of braces and a molded bridge having a plurality of pockets which are used to enhance the structure for the sound box and provide a desired tone quality for the stringed instrument. The neck may include a molded neck insert and a molded fingerboard which are used to enhance the stiffness and stability of the neck.

Abstract: A stringed musical instrument has a molded sound box and neck where the sound box is formed of between 20% to 60% carbon fibers, or other suitable fibers, and a polymeric resin or binder. The composition of materials utilized in the sound box is selected to increase stiffness and to control the tone of the instrument. The sound box includes an adjustable attachment mechanism having a pivot which is used to secure the neck to the sound box. The sound box includes a molded bracing structure having a plurality of braces and a molded bridge having a plurality of pockets which are used to enhance the structure for the sound box and provide a desired tone quality for the stringed instrument. The neck may include a molded neck insert and a molded fingerboard which are used to enhance the stiffness and stability of the neck.

Abstract: A soundboard for a musical instrument is disclosed the soundboard having at least one layer of material. In some embodiments the material comprising carbon fiber, fibrous laminate material, resin or a plastic matrix and combinations thereof. At least one bracing structure is engaged to the at least one layer of material. The at least one bracing structure comprising at least one layer of honeycomb or shaped core and at least one sheet of material bonded to the honeycomb or shaped core.

Abstract: A stringed musical instrument has a molded sound box and neck where the sound box is formed of between 20% to 60% carbon fibers, or other suitable fibers, and a polymeric resin or binder. The composition of materials utilized in the sound box is selected to increase stiffness and to control the tone of the instrument. The sound box includes an adjustable attachment mechanism having a pivot which is used to secure the neck to the sound box. The sound box includes a molded bracing structure having a plurality of braces and a molded bridge having a plurality of pockets which are used to enhance the structure for the sound box and provide a desired tone quality for the stringed instrument. The neck may include a molded neck insert and a molded fingerboard which are used to enhance the stiffness and stability of the neck.

Abstract: A novel materials technology has been developed and demonstrated for providing a high modulus composite material for use to 1000° F. and above. This material can be produced at 5-20% of the cost of refractory materials, and has higher structural properties. This technology successfully resolves the problem of “thermal shock” or “ply lift,” which limits traditional high temperature laminates (such as graphite/polyimide and graphite/phenolic) to temperatures of 550-650° F. in thicker (0.25″ and above) laminates. The technology disclosed herein is an enabling technology for the nose for the External Tank (ET) of the Space Shuttle, and has been shown to be capable of withstanding the severe environments encountered by the nose cone through wind tunnel testing, high temperature subcomponent testing, and full scale structural, dynamic, acoustic, and damage tolerance testing.

Abstract: An innovative technology for composite overwrapped pressure vessels (COPVs) has been developed which significantly increases cost effectiveness, increases reliability, and reduces weight over state-of-the-art COPVs. This technology combines an innovative thin liner made of a metal having a high modulus of elasticity and a high ductility, a high-performance composite overwrap and a high-performance film adhesive at the overwrap/liner interface. The metal liner can be fabricated from readily available titanium alloy sheet and plate using a combination of spin forming and machining to fabricate components and electron-beam welding for tank assembly. The composite overwrap is filament-wound onto an adhesive-covered titanium liner and the overwrap and adhesive are co-cured in an oven to yield an integrated tank structure.

Abstract: A guitar is described which is essentially made up of a plurality of plies of composite laminates individually selected and arranged together to provide desired sounds.

Abstract: A novel materials technology has been developed and demonstrated for providing a high modulus composite material for use to 1000.degree. F. and above. This material can be produced at 5-20% of the cost of refractory materials, and has higher structural properties. This technology successfully resolves the problem of "thermal shock" or "ply lift," which limits traditional high temperature laminates (such as graphite/polyimide and graphite/phenolic) to temperatures of 550-650.degree. F. in thicker (0.25" and above) laminates. The technology disclosed herein is an enabling technology for the nose for the External Tank (ET) of the Space Shuttle, and has been shown to be capable of withstanding the severe environments encountered by the nose cone through wind tunnel testing, high temperature subcomponent testing, and full scale structural, dynamic, acoustic, and damage tolerance testing.

Abstract: An innovative technology for composite overwrapped pressure vessels (COPVs) has been developed which significantly increases cost effectiveness, increases reliability, and reduces weight over state-of-the-art COPVs. This technology combines an innovative thin liner made of a metal having a high modulus of elasticity and a high ductility, a high-performance composite overwrap and a high-performance film adhesive at the overwrap/liner interface. The metal liner can be fabricated from readily available titanium alloy sheet and plate using a combination of spin forming and machining to fabricate components and electron-beam welding for tank assembly. The composite overwrap is filament-wound onto an adhesive-covered titanium liner and the overwrap and adhesive are co-cured in an oven to yield an integrated tank structure.

Abstract: An aerospace vehicle fuel pressure, or cryogen tank apparatus includes a tank load bearing wall of composite laminate construction that is lined with a film laminate liner that includes at least two metalized layers bonded with adhesive with the metalized coatings facing each other. The liner is bonded to the load bearing wall with an adhesive. The improved tank apparatus is able to withstand extreme pressure and extreme temperature conditions, and while containing cryogens such as liquid helium and liquid hydrogen.

Abstract: An innovative technology for composite overwrapped pressure vessels (COPVs) has been developed which significantly increases cost effectiveness, increases reliability, and reduces weight over state-of-the-art COPVs. This technology combines an innovative thin liner made of a metal having a high modulus of elasticity and a high ductility, a high-performance composite overwrap and a high-performance film adhesive at the overwrap/liner interface. The metal liner can be fabricated from readily available titanium alloy sheet and plate using a combination of spin forming and machining to fabricate components and electron-beam welding for tank assembly. The composite overwrap is filament-wound onto an adhesive-covered titanium liner and the overwrap and adhesive are co-cured in an oven to yield an integrated tank structure.