Bearing support structure and a gas turbine engine comprising the bearing support structure
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United States of America Patent
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Sep 28, 2010
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N/A
app pub date -
Sep 13, 2005
filing date -
Oct 6, 2004
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Abstract
A bearing support structure is provided for installation in a gas turbine engine between radially inner first and second bearings adapted to rotatably support a first and a second rotor, respectively, and a radially outer engine frame. The support structure includes a first annular plate-shaped part and an arrangement for supporting the first bearing at one end thereof and a second annular plate-shaped part and an arrangement for supporting the second bearing at one end thereof. The first and second plate-shaped parts are joined together forming a one-piece unit for installation in the gas turbine engine.
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