Stiffener composite charge application system
AssigneeThe Boeing Company
InventorsJonathan Young Ahn, Davis Tran
Life of this patent
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AssigneeThe Boeing Company
InventorsJonathan Young Ahn, Davis Tran
Estimating the term…
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.
A stiffener composite charge placement system comprising:
A stiffener composite charge placement system comprising:
A method of applying a stiffener composite charge to a cavity of a mandrel, the method comprising:
Dependencies are inferred from the claim text.