Methods systems and apparatuses for reducing or substantially eliminating distortion in a transparent substrate in situ are disclosed.

The present disclosure describes one or more systems, methods, routines and/or techniques for thermal management. One or more systems, methods, routines and/or techniques may provide advice or guidance (e.g., to a repair technician) regarding how to perform a hot bond repair, for example, on an aircraft component that has been damaged. The thermal management advisor may provide advice or guidance regarding how to prepare a repair field prior to running a thermal survey. For example, thermal management advisor may recommend a particular heat blanket, a configuration of the heat blanket, placement of various temperature sensors and other preparation guidance. The thermal management advisor may provide advice or guidance regarding how to alter or manage the repair setup during a thermal survey and during the actual curing process. For example, thermal management advisor may recommend particular temperature sensors or areas of the repair field that should be insulated.

The present disclosure describes one or more systems, methods, routines and/or techniques for thermal management. One or more systems, methods, routines and/or techniques may provide advice or guidance (e.g., to a repair technician) regarding how to perform a hot bond repair, for example, on an aircraft component that has been damaged. The thermal management advisor may provide advice or guidance regarding how to prepare a repair field prior to running a thermal survey. For example, thermal management advisor may recommend a particular heat blanket, a configuration of the heat blanket, placement of various temperature sensors and other preparation guidance. The thermal management advisor may provide advice or guidance regarding how to alter or manage the repair setup during a thermal survey and during the actual curing process. For example, thermal management advisor may recommend particular temperature sensors or areas of the repair field that should be insulated.

A method of bonding materials may comprise defining a bond interface between two materials in a cure zone on a surface of an object and heating the bond interface with sound waves. Heating the bond interface may include applying ultrasonic sound waves to the bond interface.

A method of bonding materials may comprise defining a bond interface between two materials in a cure zone on a surface of an object and heating the bond interface with sound waves. Heating the bond interface may include applying ultrasonic sound waves to the bond interface.

A method for repairing a component constructed in multiple layers from a layer composite material comprises a step of removing material of the layer composite material of the component in the region of damage to the component in order to form a scarfed cutout, such that a scarfed peripheral contour formed from a plurality of layers of the component is formed. Furthermore, fiber-reinforced plastic strips, which exhibit a curable plastic material in an uncured state, are applied in layers in the cutout in order to create a replacement-structure semifinished product that is complementary to and butts against the scarfed peripheral contour of the component. In a further step, the curable plastic material contained in the fiber-reinforced plastic strips is cured in order to create a replacement structure and for joining the replacement structure to the component.

A device for confining a given zone of a part. The device having a first rigid sleeve open to a first end which is capable of being applied around said given zone of the part. The device further having a second flexible and elastic sleeve open to a same first end as the first sleeve and intended to be applied on the part. The second sleeve remotely surrounds the first rigid sleeve so as to form an annular space which is connected to the means for depressing the annular space.

A device for confining a given zone of a part. The device having a first rigid sleeve open to a first end which is capable of being applied around said given zone of the part. The device further having a second flexible and elastic sleeve open to a same first end as the first sleeve and intended to be applied on the part. The second sleeve remotely surrounds the first rigid sleeve so as to form an annular space which is connected to the means for depressing the annular space.

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.

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.