Aircraft interior bushing
Number of patents in Portfolio can not be more than 2000
United States of America Patent
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Feb 19, 2013
Grant Date -
Feb 3, 2011
app pub date -
Jul 28, 2010
filing date -
Jul 29, 2009
priority date (Note) -
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status (Latency Note)
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Abstract
An aircraft interior bushing assembly is disclosed comprising interoperating bushings, each bushing comprising a recessing portion, a radially inner surface operably configured to contact a surface defining a void in a panel, a perimeter portion wherein the perimeter portion is substantially larger than the recessing portion, a support arm receiver, and a support arm coupled to each bushing. Each support arm comprises a first end coupled to the bushing, and a second end comprising a conduit receiver. In one form, the bushing assembly is operably configured to support a conduit at a distance from the radially inner surface of the interoperating bushings to substantially prohibit contact between the conduit and the bushing assembly once the conduit is installed and fixed to the conduit receiver.
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