Composite assembly with integrated composite joints
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United States of America Patent
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-
Jun 15, 2004
Issued Date -
N/A
app pub date -
Sep 13, 2002
filing date -
Sep 13, 2002
priority date (Note) -
Expired
status (Latency Note)
Importance
Abstract
An aircraft composite assembly 10 is provided, including a first composite member 12, at least one first flange joint 26 comprising a first plurality of plies 24 cured to the first composite member 12, a second composite member 30, and at least one second flange joint 38 comprising a second plurality of plies 36 cured to the second composite member 30. The at least one second flange joint 38 is bonded to the at least one first flange joint 26 such that the first composite member 12 is affixed to the second composite member 30.
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Cited Art Landscape
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