Complex laminated composites may be repaired by removal of individual damaged plies through peeling in order to exploit the weaker interlaminar properties of these composites. Upon removal of the individual damaged plies through peeling, replacement plies may be added to restore the laminated composite. In addition, when damage extends through the thickness of a laminated composite, a plug may be used to allow plies to be replaced while maintaining contour within the repair region. A caul plate also may be used to stiffen and maintain the contour of a repair region while peeling and removing plies from the repair region.

A method of repairing a core stiffened structure, including removing a damaged portion of the core stiffened structure; bonding a shelf onto a first core member; bonding a second core member to a shelf; and securing a skin patch over the second core member.

A method for recovering vinyl window frames. The method of recovering vinyl window frames includes identifying damages in an existing vinyl frame having a plurality of planes, wherein the damages exist in at least one plane, measuring the area of the frame to be covered, creating a template of the frame by securing pre-cut plates together with a gap between to allow for bending along the gap, such that the template can conform to the frame, marking cuts to be made to the replacement cover using the template, cutting the replacement cover to duplicate the existing frame, and applying the replacement cover over the existing vinyl frame.

A method for repairing a damaged aircraft fuselage outer skin part, the damaged skin part comprising a static pressure port around which is arranged a stopper fastened to a structure of the fuselage at which a pipe of the static pressure port opens, the method including removing the stopper from the static port, fitting a patch including an opening for housing the stopper, and re-fitting the stopper on an adjustable-thickness spacer. A repair assembly configured to apply the repair method is also provided. Advantageously, it is thus possible to recreate an aerodynamic profile in accordance with the requirements for taking static pressure of the aircraft, with a reduced down-time of the aircraft.

A process for repairing a part made of organic matrix composite material coated with at least one layer of paint includes removing the paint at a damaged area of the part, removing the composite material at the damaged area so as to form a recessed portion, depositing a repair resin in the recessed portion, curing the repair resin, applying at least one layer of paint to the repair area. The repair resin is loaded with magnetically detectable particles.

A tire repair tool includes a housing, an electric motor disposed within a motor housing portion, a battery receiving portion configured to receive a battery pack to power the electric motor, an actuator configured to selectively activate the electric motor, and a chuck rotatably driven by the motor and configured to receive one of a plurality of different tire repair accessories. The tire repair tool further includes a multi-speed gearbox disposed within the motor housing portion having a plurality of different gear ratios, a mode selector operative to adjust the multi-speed gearbox between the plurality of different gear ratios, and an electronic speed control system configured to operate the electric motor at less than its capable maximum operating speed when the gearbox is operated in each of the plurality of different gear ratios to further reduce a rotational speed of the chuck.

Methods for reworking structures and reworked cellular core panels, reworked structures comprising the reworked cellular core panels, and guides and cutting apparatuses for reworking cellular acoustic panels and reworking cellular acoustic and non-acoustic panels are disclosed.

A method for repairing a tire is provided that includes: (a) providing a reamer, a knife, an insertion tool forming a receiving opening, a plugging strip, and vulcanizing fluid; (b) inserting the reamer into a puncture hole of a tire to clear debris; (c) applying the vulcanizing fluid; (d) inserting the plugging strip into the insertion tool; (e) inserting the insertion tool with the plugging strip into the puncture hole to cause the plugging strip to fold into the puncture hole mixed with the vulcanizing fluid to bond the plugging strip and the tire; (f) removing the insertion tool from the puncture hole causing a middle portion of the plugging strip to fold internally forming a four-layer seal within the puncture hole; and (g) cutting the plugging strip from the insertion tool and the excess portions of the plugging strip with the knife.

A method for repairing a tire including: (a) providing a reamer, an insertion tool with a receiving opening, a tri-layer strip, and vulcanizing fluid; (b) inserting the reamer into a puncture hole of a tire to clear debris; (c) applying the vulcanizing fluid; (d) inserting the tri-layer strip into the insertion tool; (e) inserting the insertion tool and tri-layer strip into the puncture hole; wherein the insertion tool extends linearly from a first end of a center base of a first bilateral elongated tool member and a cavity encasing extending from a second end of the center base of the first bilateral elongated tool member in an opposite direction configured for housing a plurality of the tri-layer strips; and (f) removing the insertion tool from the puncture hole causing a center portion of the tri-layer strip to fold forming a four-layer seal within the puncture hole.

A method for repairing a part made of composite material includes producing a recessed section by removing the composite material at a damaged area, producing grooves extending on the two faces of the part from edges of the recessed section, producing orifices in the part opening out into the grooves, tree-dimensional weaving of a filling part fiber preforms including a central section having a shape corresponding to the shape of the recessed section and fiber bundles extending from the central section, placing the filling preforms respectively on either face of the part with the fiber bundles in the grooves on the faces of the part and in the orifices such that the fiber bundles open out into the grooves present on the opposite face of the part, impregnating the filling fiber preforms with a precursor resin of a matrix, transforming the resin into a matrix to obtain a filling part.