Cooling system for actively cooling a turbine blade

Patent metadata

Field	Value
Publication number	US-11255196-B2
Application number	US-201916537278-A
Country	US
Kind code	B2
Filing date	Aug 9, 2019
Priority date	Aug 13, 2018
Publication date	Feb 22, 2022
Grant date	Feb 22, 2022

Abstract

A cooling system for cooling a turbine blade with a cooling fluid via an internal flow passage formed in the turbine blade extending from an inlet to an outlet edge having a first passage section defining a first flow direction, a second passage section defining a second flow direction, a wall between the first and second passage section and a diverter, between the first and the second passage section. The wall in a region of the diverter forms a pier head which extends into the region of the first passage section and thereby reduces the flow cross section of the flow passage.

First claim

What is claimed is:

1. A cooling system for actively cooling a turbine blade with a cooling fluid comprising:
the turbine blade having an inlet edge and an outlet edge;
an internal flow passage formed in the turbine blade from an inlet to an outlet, which extends from the inlet edge to the outlet edge and comprises:
a first passage section, which defines a first flow direction;
a second passage section, which defines a second flow direction;
a wall located between the first passage section and the second passage section;
a curved diverter, between the first passage section and the second passage section, which is configured to transfer a fluid flow from the first flow direction into the second flow direction; and
a pier head formed by the wall in a region of the diverter, which at least with a pier head section extends into a region of the first passage section that reduces a flow cross section of the internal flow passage,
wherein the curved diverter, between the first passage section and the second passage section comprises an arcuate portion opposite the pier head,
wherein the second passage narrows in the second flow direction from a widest portion in an area of the pier head.

2. The cooling system according to claim 1 , wherein the internal flow passage further comprises:
a third passage section;
a second curved diverter arranged at an end of the second passage section, which opens into the third passage section;
a second wall between the second passage section and third passage section; and
a second pier head formed by the second wall, which extends at least with a pier head section into a region of the second passage section that reduces the flow cross section of the internal flow passage
wherein the second passage has a narrowest portion in an area of the second pier head.

3. The cooling system according to claim 2 , wherein an outer contour of the second pier head viewed in a flow direction extends as follows: commencing from a linearly extending wall of the second passage section with a curvature section, which curves in a direction of the third passage section, merging into a part circle-shaped arc section of opposite curvature, which in turn, at an outlet of the diverter, merges into a linearly extending wall of the third passage section, without the outer contour projecting into the third passage section.

4. The cooling system according to claim 3 , wherein the turbine blade comprises an annular space between a lower blade contour and an upper blade contour, which defines a gas-conducting surface of the turbine blade.

5. The cooling system according to claim 4 , wherein a center of the pier head is arranged in a region which is arranged offset relative to the annular space within the blade contour lower or the upper blade contour.

6. The cooling system according to claim 2 , wherein the second curved diverter is configured to divert the flow direction by substantially 160°.

7. The cooling system according to claim 1 , wherein the pier head viewed in cross section is formed at least in a face-end section one of circular arc-shaped, curved, or drop-shaped and extends in a direction of the first passage section.

8. The cooling system according to claim 1 , wherein the pier head, viewed in cross section, is formed, at least in a face end section, from a plurality of linear and/or polynomial sections and extends in a direction of the first passage section.

9. The cooling system according to claim 1 , wherein an outer contour of the pier head viewed in a flow direction extends as follows: commencing from a linearly extending wall of the first passage section with a curvature section, which curves in a direction of the first passage section, merging into a part circle-shaped arc section of opposite curvature, which in turn, at an outlet of the diverter, merges into a linearly extending wall of the second passage section, without the outer contour projecting into the second passage section.

10. The cooling system according to claim 1 , wherein the internal flow passage further comprises:
the inlet, which forms an opening for receiving the cooling fluid in the internal flow passage; and
the outlet configured as a blowout, which forms an opening for letting the cooling fluid out of the internal flow passage.

11. The cooling system according to claim 1 , wherein the turbine blade, in a region of the inlet edge, comprises a multiplicity of outlet openings configured to let the cooling fluid out of the internal flow passage, which are arranged spaced from one another.

12. The cooling system according to claim 1 , wherein the turbine blade comprises a multiplicity of outlet openings configured to let the cooling fluid out of the internal flow passage, which are arranged spaced from one another.

Assignees

• MTU Aero Engines AG
• Man Energy Solutions Se
• Mtu Aero Engines

Inventors

• Freno Dieter
• Pöhler Thorsten
• Pernleitner Martin
• Storm Paul
• Stavropoulou Electra
• Frank Dirk

Classifications

• F05D2260/202

  by film cooling · CPC title

• F01D5/187

  Convection cooling · CPC title

• F05D2240/304

  related to the trailing edge of a rotor blade · CPC title

• F05D2260/20

  Heat transfer, e.g. cooling · CPC title

• F01D5/18 Primary

  Hollow blades, {i.e. blades with cooling or heating channels or cavities (structure of hollow blades in general F01D5/147)}; Heating, heat-insulating or cooling means on blades · CPC title