| CPC F01D 5/186 (2013.01) [F01D 1/12 (2013.01); F01D 5/147 (2013.01); F01D 5/284 (2013.01); F01D 11/12 (2013.01); F01D 11/122 (2013.01); F01D 11/14 (2013.01); F05D 2220/32 (2013.01); F05D 2230/31 (2013.01); F05D 2230/311 (2013.01); F05D 2240/303 (2013.01); F05D 2240/304 (2013.01); F05D 2260/201 (2013.01); F05D 2260/202 (2013.01); F05D 2300/514 (2013.01)] | 20 Claims |

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1. A component for a turbine engine, comprising:
a body with an exterior surface abutting a combustion flowpath for a combustion gas flow through the turbine engine;
a cooling passage defined within the body and supplying cooling air to the component; and
a trench on the exterior surface, comprising:
an undulating surface defining a minimum depth and a maximum depth of the trench with respect to the exterior surface;
a plurality of outlets in the undulating surface; and
a plurality of cooling holes extending from the cooling passage to the corresponding plurality of outlets;
wherein the undulating surface comprises a curved surface defining a cooling wall between two adjacent outlets in the plurality of outlets,
wherein at least one outlet in the plurality of outlets is located at the maximum depth of the trench; and
wherein at least one cooling hole in the plurality of cooling holes comprises a cross-sectional area that increases in a direction toward the plurality of outlets.
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