ENHANCED THERMALLY CONDUCTIVE PIVOT BUSHING
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United States of America Patent
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Issued Date -
Feb 18, 2016
app pub date -
Aug 12, 2014
filing date -
Aug 12, 2014
priority date (Note) -
Abandoned
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Abstract
An aircraft pivot joint bushing has enhanced thermal conductivity due to the bushing having an inner cylindrical portion which has a first thermal dissipating capacity, and an outer cylindrical portion on the inner cylindrical portion which has a second thermal dissipating capacity, where the second thermal dissipating capacity is less than the first thermal dissipating capacity.
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