Abstract: A method of attaching a composite member to a structure is provided. The method includes forming a laminate of fabric impregnated with resin; applying an adhesive to an area of the structure needing repair; positioning the impregnated laminated on the adhesive applied the area of the structure needing repair; applying a single vacuum enclosure over the laminate and the adhesive; applying heat at a first temperature to the impregnated laminate; applying a partial vacuum at a first vacuum pressure within the single vacuum enclosure to the impregnated laminate to degas the resin in the impregnated laminate and form a degassed laminate; and curing the degassed laminate and adhesive on the area of the structure needing repair by applying heat at a second temperature and by applying vacuum at a second vacuum pressure within the single vacuum enclosure, the second vacuum pressure greater than the first vacuum pressure.

Abstract: A method of attaching a composite member to a structure. The method including forming a laminate of fabric impregnated with resin; applying heat at a first temperature to the impregnated laminate; applying vacuum at a first pressure to the impregnated laminate to degas the resin and form a degassed, impregnated laminate; positioning the degassed, impregnated laminate on a structure; and curing the degassed, impregnated laminate on the substrate by applying heat at a second temperature and by applying vacuum at a second pressure.

Abstract: A method of attaching a composite member to a structure. The method including forming a laminate of fabric impregnated with resin; applying heat at a first temperature to the impregnated laminate; applying vacuum at a first pressure to the impregnated laminate to degas the resin and form a degassed, impregnated laminate; positioning the degassed, impregnated laminate on a structure; and curing the degassed, impregnated laminate on the substrate by applying heat at a second temperature and by applying vacuum at a second pressure.

Abstract: A device and method to repair a structural component. The device includes a plug that bonds to the structural component. The plug includes a flange and a solid shank extending from the flange, the solid shank being disposable in an opening of the structural component. The device further includes disc that bonds to the structural component such that, when bonded, the disc covers the solid shank of the plug. The method includes bonding the plug to the structural component such that the solid shank of the plug is disposed in the opening of the structural component. The method further includes bonding the disc to the structural component.

Abstract: A method of attaching a composite member to a structure. The method including forming a laminate of fabric impregnated with resin; applying heat at a first temperature to the impregnated laminate; applying vacuum at a first pressure to the impregnated laminate to degas the resin and form a degassed, impregnated laminate; positioning the degassed, impregnated laminate on a structure; and curing the degassed, impregnated laminate on the substrate by applying heat at a second temperature and by applying vacuum at a second pressure.

Abstract: A device and method to repair a structural component. The device includes a plug that bonds to the structural component. The plug includes a flange and a solid shank extending from the flange, the solid shank being disposable in an opening of the structural component. The device further includes disc that bonds to the structural component such that, when bonded, the disc covers the solid shank of the plug. The method includes bonding the plug to the structural component such that the solid shank of the plug is disposed in the opening of the structural component. The method further includes bonding the disc to the structural component.

Abstract: An abrasive article is disclosed that is suitable for cleaning, sanding, scraping, or other such process of removing an outer layer or adherent matter. The abrasive article includes a plurality of abrasive particles at least partially embedded in a frozen liquid.

Abstract: A device for repairing a structural component (305) having a first member (401) adapted for bonding to a structural component (305).

Abstract: An abrasive article is disclosed that is suitable for cleaning, sanding, scraping, or other such process of removing an outer layer or adherent matter. The abrasive article includes a plurality of abrasive particles at least partially embedded in a frozen liquid.

Abstract: A device for repairing a structural component (305) having a first member (401) adapted for bonding to a structural component (305).

Abstract: A method and apparatus for precisely locating, aligning, targeting, and marking locations for fastener holes in structures is disclosed. The method and apparatus utilizes laser devices to project laser beams through alignment tools to determine the proper location and orientation of the fastener holes.

Abstract: A method of attaching a composite member to a structure. The method including forming a laminate of fabric impregnated with resin; applying heat at a first temperature to the impregnated laminate; applying vacuum at a first pressure to the impregnated laminate to degas the resin and form a degassed, impregnated laminate; positioning the degassed, impregnated laminate on a structure; and curing the degassed, impregnated laminate on the substrate by applying heat at a second temperature and by applying vacuum at a second pressure.

Abstract: A method and apparatus for precisely locating, aligning, targeting, and marking locations for fastener holes in structures is disclosed. The method and apparatus utilizes laser devices to project laser beams through alignment tools to determine the proper location and orientation of the fastener holes.