Composite structure repair process
AssigneeNorthrop Grumman Corporation
InventorCarl Andrew Reis
Life of this patent
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AssigneeNorthrop Grumman Corporation
InventorCarl Andrew Reis
Estimating the term…
A method for repairing a multi-layered damage area in a multi-layered composite structure. The method first includes obtaining depth measurement data, and obtaining topographical measurement data by laser scanning the surface of the damage area. This depth measurement data and topographical measurement data are inputted into a microprocessor along with thickness data of each layer. All inputted information is correlated among itself to thereby internally produce a three-dimensional damage area display-replica and interpolate a two-dimensional pattern of each layer of the damage area and of the surface of the damage area. The damage area is removed by first projecting a two-dimensional laser pattern of the damage area thereat on the surface of the structure, and thereafter manually removing the area to produce a void. Repair is accomplished by projecting onto respective replacement material a two-dimensional laser image pattern of each layer and manually cutting that layer according to the appropriate pattern. The cut layers then are arranged in accord with construction of the removed damage area to form a plug that is placed within the void.
A method for repairing a multi-layered damage area in a multi-layered composite structure, said damage area having a surface, a width dimension and a depth dimension and disposed on a surface of the composite structure, the method comprising:
Dependencies are inferred from the claim text.