Internally cooled spoke
A turbine engine includes a compressor section, a combustor section in fluid communication with the compressor section, a high pressure turbine in fluid communication with the combustor, a low pressure turbine in fluid communication with the high pressure turbine, and a mid turbine frame located axially between the high pressure turbine and the low pressure turbine. The mid turbine frame includes an outer frame case, an inner frame case, and a plurality of hollow spokes that distribute loads from the inner frame case to the outer frame case. The spokes are hollow to allow cooling airflow to be supplied through the spokes to the inner frame case.
1. A turbine engine that extends along an axis, the turbine engine comprising:
a compressor;
a combustor in fluid communication with the compressor;
a first turbine section in fluid communication with the combustor;
a second turbine section in fluid communication with the first turbine section;
a fan;
a first shaft interconnecting the compressor and the first turbine section;
a second shaft interconnecting the fan and the second turbine section, the second shaft being connected to the fan through a geared architecture and a portion of the second shaft extending through a center of the first shaft;
a mid-turbine frame located axially between the first turbine section and the second turbine section, 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, a radially inner end, and a hollow center 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 with a first cylindrical face oriented towards the axis, an inner diameter annular portion with a second cylindrical face oriented away from the axis, and first and second radial portions of the inner frame case that extend radially from the outer diameter annular portion to the inner diameter annular portion; and
each of the plurality of cooled spokes terminates radially between a radially outer surface of the outer diameter annular portion and a radially inner surface of the outer diameter annular portion to thereby allow the manifold to receive and combine airflow from the plurality of cooled spokes
a first bearing connected to the first shaft and supported by the mid-turbine frame; and
a second bearing connected to the second shaft and supported by the mid-turbine frame, wherein the second bearing is positioned axially aft of and radially outward of the first bearing.
2. The turbine engine of claim 1 , wherein the plurality of cooled spokes includes three or more cooled spokes evenly distributed around the inner frame case.
3. The turbine engine of claim 1 , wherein the outer frame case includes a plurality of bosses located on an outer surface of the outer frame case for attachment to each of the plurality of cooled spokes.
4. A mid-turbine frame located in a gas turbine engine axially aft of a first turbine and fore of a second turbine, the gas turbine engine extending along an axis and including a fan, a compressor, a first shaft interconnecting the compressor and the first turbine, a second shaft interconnecting the fan and the second turbine, the second shaft being connected to the fan through a geared architecture, a first bearing connected to the first shaft and supported by the mid-turbine frame, and a second bearing connected to the second shaft and supported by the mid-turbine frame, wherein the second bearing is positioned axially aft of and radially outward of the first bearing, the mid-turbine frame comprising:
an outer frame case;
an inner frame case; and
a plurality of hollow spokes that each have a radially outer end, a radially inner end, and a hollow center, the plurality of hollow spokes being attached between the outer frame case and the inner frame case to distribute force from the inner frame case to the outer frame case, wherein cooling airflow flows through the plurality of hollow spokes to the inner frame case, wherein the inner frame case includes a manifold defined by an outer diameter annular wall with a first cylindrical face oriented towards the axis and a second cylindrical face oriented away from the axis, an inner diameter annular wall with a third cylindrical face oriented away from the axis, and first and second radial walls of the inner frame case that extend radially between the outer diameter annular wall and the inner diameter annular wall, and wherein a radially inner end of each of the plurality of hollow spokes meets the outer diameter annular wall at an opening in the outer diameter annular wall of the manifold and terminates between the first cylindrical face and the second cylindrical face of the outer diameter annular wall to thereby allow the manifold to receive and combine cooling airflow provided via the plurality of hollow spokes.
5. The mid-turbine frame of claim 4 , wherein the the plurality of hollow spokes includes three or more hollow spokes evenly distributed around the inner frame case.
6. The mid-turbine frame of claim 4 , wherein the outer frame case includes a plurality of bosses located on an outer surface of the outer frame case for attachment to each of the plurality of hollow spokes.