Gas-turbine exhaust cone
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United States of America Patent
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Nov 13, 2012
Grant Date -
Jan 12, 2012
app pub date -
Jul 11, 2011
filing date -
Jul 12, 2010
priority date (Note) -
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Abstract
A gas-turbine exhaust cone includes a cone shaped outside cone 1 closed in a flow direction, an inside cone 2 arranged in the outside cone 1 over at least part of the length of the exhaust cone, with the inside cone 2 being connected to the outside cone 1 via at least one helical partition wall 3, thereby forming an interspace 4 between the outside cone 1 and the inside cone 2. The interspace 4 is connected to inlet openings 5 at its inflow side and opens at an exit side 6 towards an interior 7 of the outside cone 1. A dampening element 8 is arranged in the outside cone 1 adjacent to the exit side 6 of the interspace 4.
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