Internally cooled spoke

A turbine engine comprising:

• a combustor;
• a first spool comprising a high pressure compressor connected to a high pressure turbine;
• a second spool comprising a low pressure compressor connected to a low pressure turbine;
• and
• a mid-turbine frame located axially between the high pressure turbine and the low pressure turbine, the mid-turbine frame having an outer frame case connected to an inner frame case via a plurality of cooled spokes, wherein each of the plurality of cooled spokes has a radially outer end and a radially inner end and is hollow within a spoke wall for supplying cooling airflow from outside the outer frame case to the inner frame case, wherein the inner frame case includes a manifold defined by an outer diameter annular portion, an inner diameter annular portion, first and second radial portions of the inner frame case that extend radially between the outer diameter annular portion and the inner diameter annular portion, and wherein a radially inner end of the spoke wall of each of the plurality of cooled spokes meets the outer diameter annular portion of the manifold at an opening in the outer diameter annular portion extending from a radially outer surface of the outer diameter annular portion and a radially inner surface of the outer diameter annular portion, and terminates between the radially outer surface of the outer diameter annular portion and the radially inner surface of the outer diameter annular portion to define an airflow path from each of the plurality of cooled spokes into the manifold that allows the manifold to receive and combine the cooling airflow from the plurality of cooled spokes.