Mechanical joint for a gas turbine engine
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United States of America Patent
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Jun 11, 2013
Issued Date -
N/A
app pub date -
Jun 15, 2009
filing date -
Jun 15, 2009
priority date (Note) -
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Abstract
A mechanical joint for a gas turbine engine includes:(a) an annular first component having an annular, radially-extending first flange; (b) an annular second component having an annular, radially-extending second flange abutting the first flange; (c) a plurality of generally radially-extending radial channels passing through at least one of the first and second flanges; (d) a plurality of generally axially-extending channels extending through the first flange and communicating with respective ones of the radial channels; and (e) a plurality of fasteners clamping the first and second flanges together.
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