Method for tolerance compensation between two components and a tool for execution of the method
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United States of America Patent
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May 14, 2013
Grant Date -
Sep 30, 2010
app pub date -
Mar 23, 2010
filing date -
Mar 25, 2009
priority date (Note) -
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Abstract
A method for tolerance compensation in an overlap joint between a first and a second body section of adjacent fuselage rings includes introducing a plurality of holes into a first body section corresponding to a pattern of rivets; arranging the first and second body section in an overlapping configuration so as to form an overlap; injecting a filler mass through the plurality of holes into a gap formed in the overlap; and hardening the filler mass.
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