Internally cooled spoke

Patent metadata

Field	Value
Publication number	US-9316117-B2
Application number	US-201213361480-A
Country	US
Kind code	B2
Filing date	Jan 30, 2012
Priority date	Jan 30, 2012
Publication date	Apr 19, 2016
Grant date	Apr 19, 2016

Abstract

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.

First claim

The invention claimed is:

1. A turbine engine comprising:
a combustor;
a first turbine section in fluid communication with the combustor;
a second turbine section in fluid communication with the first turbine section; and
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 an outer end and an 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, a first inner diameter annular portion, a second inner diameter annular portion, first and second radial portions of the inner frame case that extend radially between the outer diameter annular wall and the first and second inner diameter annular portions, respectively, and the inner end of each of the plurality of cooled spokes, and wherein the spoke wall of each of the cooled spokes meets the outer diameter annular portion of the manifold around an opening in the outer diameter annular portion of the manifold and terminates between an outer surface of the outer diameter annular portion and an inner surface of the outer diameter annular portion to define an airflow path from each of the cooled spokes into the manifold that allows the manifold to receive and combine airflow from the plurality of cooled spokes.

2. The turbine engine of claim 1 , wherein the mid-turbine frame 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 mid-turbine frame comprising:
an outer frame case;
an inner frame case; and
a plurality of hollow spokes each having a spoke wall with an outer end and an inner end, the spoke wall 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, a first inner diameter annular wall, a second inner diameter annular wall, and first and second axial walls of the inner frame case that extend radially between the outer diameter annular wall and the first and second inner diameter annular walls, respectively, and the inner end of each of the plurality of cooled spokes; and
wherein the spoke wall of each of the hollow spokes meets the outer diameter annular portion of the manifold around an opening in the outer diameter annular portion of the manifold and terminates between an outer surface of the outer diameter annular wall and an inner surface of the outer diameter annular wall to define an airflow path from each of the hollow spokes into the manifold that allows the manifold to receive and combine cooling airflow provided via the plurality of hollow spokes.

5. The turbine engine of claim 4 , wherein the mid-turbine frame includes three or more hollow spokes evenly distributed around the inner frame case.

6. The turbine engine 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.

Assignees

• Sanchez Paul K
• Parekh Kalpendu J
• Daniels William A
• Tu John S
• United Technologies Corp

Inventors

• Sanchez Paul K
• Parekh Kalpendu J
• Daniels William A
• Tu John S

Classifications

• F02C7/12

  Cooling of plants (of component parts, see the relevant subclasses, e.g. F01D; cooling of engines in general F01P) · CPC title

• F01D25/12

  Cooling · CPC title

• F01D25/246

  Fastening of diaphragms or stator-rings · CPC title

• F02C7/20

  Mounting or supporting of plant; Accommodating heat expansion or creep · CPC title

• F05D2220/36

  specially adapted for the fan of turbofan engines · CPC title