Stiffener composite charge application system

A stiffener composite charge placement system is presented. The stiffener composite charge placement system comprises a longitudinal end effector having a first attachment point and a second attachment point; a first rotational arm having a first connector configured to connect to the first attachme...

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Bibliographische Detailangaben
Hauptverfasser:	Ahn, Jonathan Young, Tran, Davis
Format:	Patent
Sprache:	eng
Schlagworte:	AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING AIRCRAFT AVIATION COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULARARTICLES PERFORMING OPERATIONS 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:	A stiffener composite charge placement system is presented. The stiffener composite charge placement system comprises a longitudinal end effector having a first attachment point and a second attachment point; a first rotational arm having a first connector configured to connect to the first attachment point; a first movement system configured to move the first rotational arm within a manufacturing environment; a second rotational arm having a second connector configured to connect to the second attachment point; and a second movement system configured to move the second rotational arm within the manufacturing environment.