Gas turbine engine geared architecture axial retention arrangement
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United States of America Patent
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Aug 27, 2013
Issued Date -
N/A
app pub date -
Jul 25, 2012
filing date -
Mar 30, 2012
priority date (Note) -
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status (Latency Note)
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Abstract
A support assembly for a geared architecture includes an engine static structure. A flex support is secured to the engine static structure and includes a bellow. A support structure is operatively secured to the flex support. A geared architecture is mounted to the support structure. First members are removably secured to one of the engine static structure and the flex support and second members are removably secured to the support structure. The first and second members are circumferentially aligned with one another and spaced apart from one another during a normal operating condition. The first and second members are configured to be engageable with one another during an extreme event to limit axial movement of the geared architecture relative to the engine static structure.
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