A method for patching a hole in a composite parent structure. The method comprises: inserting an insert in the hole; placing a composite patch having a multiplicity of curved flexible members on one side of the composite parent structure in a position where a central portion of the composite patch overlies the insert and the flexible members confront opposing portions of the composite parent structure providing adhesive between the composite patch, the insert, and the composite parent structure; pressing the composite patch against the composite parent structure with sufficient pressure to force the flexible members to conform to the shape of the composite parent structure; and while the flexible members are in a stressed state, curing the adhesive in a manner that causes the flexible members to bond to the parent structure.

A method of repairing a first automotive part that includes providing a connector tab and applying a fluidic thermoplastic material to the connector tab and/or the first automotive part to attach the connector tab to the first automotive part. The connector tab comprises: a retainer portion sized to attach to the first automotive part, wherein the retainer portion has a plurality of holes formed therethrough, and wherein the plurality of holes is configured to receive the fluidic thermoplastic material to secure the retainer portion to the first automotive part; and a coupler portion defining a shape corresponding to a portion of the first automotive part, the coupler portion forming a coupler, which is configured to operably engage another coupler of a second automotive part.

A lining drum which has a tubular body having open ends, an inlet for compressed air and an outlet for liner is disclosed. The lining drum has end pieces removably attached to the tubular body for closing the open ends of the tubular body, a rotatable shaft inside the tubular body and a crank for rotating the shaft. The end piece has a spring-loaded flange mounting, wherein bias of springs pushes the flange mounting towards the tubular body and a closed position of the flange mounting, and air pressure inside the lining drum pushes the flange mounting away from the tubular body and towards an open position of the flange mounting.

A moisture detecting bleeder material includes a fiberglass material and a moisture absorption indicator material. The moisture absorption indicator material is a component of the fiberglass material and undergoes a color change from a first color to a second color when exposed to moisture. The color change may be thermally irreversible below a threshold temperature (e.g., below a temperature of 450 F.).

Systems and methods for reinforcing structures with composite reinforcement systems are disclosed herein. According to aspects of the present disclosure, a carrier of a composite reinforcement system for repairing and/or reinforcing a physical structure is disclosed. The carrier includes a plurality of carbon fibers. Each carbon fiber has a longitudinal axis and a length extending in a generally 0 degree direction. The carrier further includes at least one fiberglass fiber having a longitudinal axis and a length extending in a generally 90 degree direction across the plurality of carbon fibers. The plurality of carbon fibers constitute at least about 70 wt % of the carrier and the at least one fiberglass fiber constitutes at most about 30 wt % of the carrier.

Provided is a method of repairing damage on a wind turbine blade with a simple method. The method of repairing a wind turbine blade is a method of repairing a wind turbine blade for a damage portion caused by a lightning strike, including the steps of: generating in advance a repairing member molded in a predetermined flat plate shape and solidified; determining a damage determination range defined in advance for the damage portion; and bonding the repairing member when a result of inspecting the wind turbine blade indicates that the damage portion is within the damage determination range. The step of generating the repairing member may include stacking glass fiber materials to generate the repairing member.

Each cell is pressurized with gas from outside of the cell, the amount of permeation of the gas permeated into each cell is measured, and a cell having the amount of permeation greater than (average value of all cells+A) (wherein A is a predetermined value of ? to 6?, where ? is the standard deviation) is considered to be defective. Alternatively, pressure is reduced for each cell, the degree of vacuum in each cell is measured, and a cell having the degree of vacuum worse than (average value of all cells+A) is considered to be defective. Then, a polymer compound is poured into the defective cells of the monolithic separation membrane structure and cured so that the defective cells are sealed. Alternatively, the polymer compound formed in advance as the sealing member is inserted into the defective cells to seal the defective cells.

A disclosed method is suitable for repairing a blade of a turbomachine rotor, particularly a turbomachine fan, that includes a vane made from an organic-matrix composite and a metallic shield that is bonded to a leading edge of the vane and has a damaged region. The method includes steps of resetting the leading edge of the vane cooling the entire vane, followed by a step of refilling the damaged region by adding a metallic material to this damaged region and melting the material using a laser, and a step of tailoring the damaged region by machining the molten material.

A disclosed method is suitable for repairing a blade of a turbomachine rotor, particularly a turbomachine fan, that includes a vane made from an organic-matrix composite and a metallic shield that is bonded to a leading edge of the vane and has a damaged region. The method includes steps of resetting the leading edge of the vane cooling the entire vane, followed by a step of refilling the damaged region by adding a metallic material to this damaged region and melting the material using a laser, and a step of tailoring the damaged region by machining the molten material.

A custom weld-repair tool, for use in repairing a discrepant weld between workpieces, including an extended portion and a cavity adjacent the extended portions. The discrepant weld includes an insufficient primary portion and the tool is configured to, when the extended portion is in contact with a proximate one of the workpieces, channel welding energy, received at or generated at the tool, to the proximate workpiece via the extended portion, to form or enlarge a weld at a periphery of the primary portion or directly adjacent the primary portion.