Systems and methods for assembling aircraft wing skins
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United States of America Patent
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Jan 30, 2018
Issued Date -
N/A
app pub date -
Apr 9, 2015
filing date -
Apr 9, 2015
priority date (Note) -
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status (Latency Note)
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Abstract
In one embodiment, a system includes a first end effector configured to press a selected area of an aircraft wing skin panel against a corresponding area of an underlying wing support structure with a downward force, drill a hole within the selected area, the hole extending through the skin panel and the support structure, and insert an elongated shaft of a fastener into the hole. The system includes a mechanism configured to locate the first end effector relative to the selected area. The system can further include a second end effector configured to press the corresponding area of the support structure against the selected area of the skin panel with an upward force that is opposite in direction to the downward force, and a mechanism configured to locate the second end effector relative to the corresponding area of the support structure.
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