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 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.

The invention relates to compositions comprising at least one first and one second component; —the first component K1 comprising at least one di(aminobenzoate) ester A1 of formula (I) with an average molecular weight of 500 g/mol to 2000 g/mol, preferably 600 g/mol to 1500 g/mol and particularly preferred between 650 g/mol and 1300 g/mol, G being a divalent group derived from poly(tetramethylene oxide) diol, and —the second component K2 comprising at least one aromatic polyisocyanate B1 with an average molecular weight of 160 g/mol to 1100 g/mol, preferably 500 g/mol to 800 g/mol.

The invention relates to compositions comprising at least one first and one second component; —the first component K1 comprising at least one di(aminobenzoate) ester A1 of formula (I) with an average molecular weight of 500 g/mol to 2000 g/mol, preferably 600 g/mol to 1500 g/mol and particularly preferred between 650 g/mol and 1300 g/mol, G being a divalent group derived from poly(tetramethylene oxide) diol, and —the second component K2 comprising at least one aromatic polyisocyanate B1 with an average molecular weight of 160 g/mol to 1100 g/mol, preferably 500 g/mol to 800 g/mol.

The present disclosure is directed to a system and method for repairing an abradable material coated on a casing of a gas turbine engine. The system includes an articulating guide configured to fit into an access port of the gas turbine engine. Further, the articulating guide has a proximal end and a distal end. The system also includes a repair tool configured at a distal end of the articulating guide. The repair tool includes a body having a proximal end and a shaped distal end, with the shaped distal end extending away from the body. Thus, the shaped distal body is configured to trench out an area of the abradable material comprising a defect. The system also includes a filler material for filling the trenched out area.

A method for repairing composite components includes installing a plug within a feature defined by a composite component, with the plug being formed from one or more neutral materials. Furthermore, the method includes infiltrating the composite component with an infiltrant to densify a repair region of the composite component, with the plug blocking a flow of the infiltrant into the feature. Moreover, after infiltrating the composite component, the method includes removing the plug from the feature.

Provided is a puncture repair kit container that includes a container body including a holding portion that holds puncture repair liquid and an opening portion provided in one end of the holding portion, a cap mounted on the opening portion, a hose connected to a connecting portion provided in the cap, and an engaging portion that is provided in an outer surface of the cap and that engages the hose in an unused state by causing the hose to extend along a periphery of the cap.

Provided is a puncture repair kit container that includes a container body including a holding portion that holds puncture repair liquid and an opening portion provided in one end of the holding portion, a cap mounted on the opening portion, a hose connected to a connecting portion provided in the cap, and an engaging portion that is provided in an outer surface of the cap and that engages the hose in an unused state by causing the hose to extend along a periphery of the cap.

An apparatus and methods include infusing the flowable matrix material into a space in the composite laminate through the use of a formed hole extending at least partially through the composite laminate. In addition, the apparatus and methods include infusing the flowable matrix material into a space in the composite laminate in a stepwise manner in order to obtain more complete filling of such space.

An apparatus and methods include infusing the flowable matrix material into a space in the composite laminate through the use of a formed hole extending at least partially through the composite laminate. In addition, the apparatus and methods include infusing the flowable matrix material into a space in the composite laminate in a stepwise manner in order to obtain more complete filling of such space.