SCARF REPAIR APPARATUS, SYSTEM, AND METHOD

Disclosed herein is a duplicator assembly (122) for forming a first void (144), which can be layered, in a laminated material of a part (102) that matches a second void (142) in a scarf repair guide (120). The duplicator assembly (122) comprises an arm (134) that comprises a first end portion (146)...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	Morse, Steve J, Lazar, Michael A, Henderson, James H, Hengy, David J, Ridgeway, Larry D
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING AIRCRAFT AVIATION COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOTDIRECTED TO A PARTICULAR RESULT CONTROL OR REGULATING SYSTEMS IN GENERAL CONTROLLING COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR DETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g.ARRANGEMENTS FOR COPYING OR CONTROLLING FUNCTIONAL ELEMENTS OF SUCH SYSTEMS GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR MACHINE TOOLS MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OFPARTICULAR DETAILS OR COMPONENTS METAL-WORKING NOT OTHERWISE PROVIDED FOR MILLING MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS PERFORMING OPERATIONS PHYSICS REGULATING SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR SHAPING OR JOINING OF PLASTICS TRANSPORTING WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
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Beschreibung
Zusammenfassung:	Disclosed herein is a duplicator assembly (122) for forming a first void (144), which can be layered, in a laminated material of a part (102) that matches a second void (142) in a scarf repair guide (120). The duplicator assembly (122) comprises an arm (134) that comprises a first end portion (146) and a second end portion (148). The first end portion (146) is spaced apart from the second end portion (148). The duplication assembly (122) also comprises a probe (136) that is fixed to the first end portion (146) of the arm (134) and configured to trace the second void (142) in the scarf repair guide (120). The duplication assembly (122) further comprises a milling tool (140) that is fixed to the second end portion (148) of the arm (134) such that the milling tool (140) is co-movably coupled with the probe (136) via the arm (134).