CPC F01D 5/284 (2013.01) [F01D 5/141 (2013.01); F01D 5/282 (2013.01); F01D 9/041 (2013.01); C04B 35/64 (2013.01); F01D 5/288 (2013.01); F05D 2240/12 (2013.01); F05D 2260/941 (2013.01); F05D 2300/6033 (2013.01)] | 10 Claims |
1. A component adapted for use in a gas turbine engine, the component comprising
a body comprising ceramic matrix composite material having a peak-stress region and an off-peak stress region, and
a strain concentration feature located at the off-peak stress region and configured to cause stresses to form in the off-peak stress region instead of at the peak-stress region to reduce stress at the peak-stress region.
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