Exhaust diffuser and method for manufacturing an exhaust diffuser

Patent metadata

Field	Value
Publication number	US-9631518-B2
Application number	US-201214237872-A
Country	US
Kind code	B2
Filing date	Aug 1, 2012
Priority date	Aug 19, 2011
Publication date	Apr 25, 2017
Grant date	Apr 25, 2017

Abstract

An exhaust diffuser and method for manufacturing an exhaust diffuser is provided. An exhaust diffuser for a torque-generating turbine, in particular a torque-generating gas turbine is provided, the exhaust diffuser having an inner member, and the inner member having an outer surface. The outer member having an inner surface, and the inner member and the outer member forming an annular channel at least a first supporting strut connecting the inner member and the outer member, the supporting strut extending essentially radially from the inner surface to the outer surface, the supporting strut having a middle section, the middle section having a first airfoil and an outer section having a second airfoil, and the second airfoil having a higher angle of incidence than the first airfoil. Furthermore, it is described a method for manufacturing an exhaust diffuser.

First claim

The invention claimed is:

1. An exhaust diffuser for a torque-generating turbine, the exhaust diffuser comprising:
an inner member having an outer surface and an outer member having an inner surface, the inner member and the outer member forming an annular channel,
a first supporting strut connecting the inner member and the outer member, the first supporting strut extending essentially radially from the inner surface to the outer surface,
a second supporting strut, wherein the first supporting strut and the second supporting strut form a mirror twin-strut with an in flow-direction narrowing channel therein between;
the first supporting strut and the second supporting strut comprising a middle section having a first airfoil, an outer section having a second airfoil and an inner section having a third airfoil,
the second airfoil having a higher angle of incidence than the first airfoil, and
the third airfoil having a lower angle of incidence than the second airfoil.

2. The exhaust diffuser for a torque-generating turbine of claim 1 , wherein a difference between the angle of incidence of the third airfoil and the angle of incidence of the second airfoil is between 0° and 40°.

3. The exhaust diffuser for a torque-generating turbine of claim 1 , wherein the first airfoil has a smaller thickness than the second airfoil and/or the third airfoil.

4. The exhaust diffuser for a torque-generating turbine of claim 1 , wherein the first airfoil has a smaller leading edge radius than the second airfoil and/or the third airfoil.

5. The exhaust diffuser for a torque-generating turbine of claim 1 , wherein the first airfoil has a smaller camber than the second airfoil and the third airfoil.

6. The exhaust diffuser for a torque-generating turbine of claim 1 , wherein the exhaust diffuser has an even number of first supporting struts and/or second supporting struts.

7. The exhaust diffuser for a torque-generating turbine of claim 1 , wherein the exhaust diffuser has an odd number of first supporting struts and/or second supporting struts.

8. The exhaust diffuser for a torque-generating turbine of claim 1 , wherein the exhaust diffuser has eight or fewer first supporting struts and/or second supporting struts.

9. The exhaust diffuser for a torque-generating turbine of claim 1 , having four or fewer twin-struts.

10. The exhaust diffuser for a torque-generating turbine of claim 1 , wherein a difference between the angle of incidence of the third airfoil and the angle of incidence of the second airfoil is between 5° and 30°.

11. The exhaust diffuser for a torque-generating turbine of claim 1 , wherein a difference between the angle of incidence of the third airfoil and the angle of incidence of the second airfoil is between 5° and 20°.

12. The exhaust diffuser for a torque-generating turbine of claim 1 , wherein the exhaust diffuser comprises six or fewer first supporting struts and/or second supporting struts.

13. The exhaust diffuser for a torque-generating turbine of claim 1 , comprising three or fewer twin-struts.

14. The exhaust diffuser for a torque-generating turbine of claim 1 , wherein the torque-generating turbine is a torque-generating gas turbine.

15. An exhaust diffuser for a torque-generating turbine, the exhaust diffuser comprising:
an inner member having an outer surface and an outer member having an inner surface, the inner member and the outer member forming an annular channel,
a plurality of supporting struts in an annular ring, each supporting strut connecting the inner member and the outer member, and each supporting strut extending essentially radially from the inner surface to the outer surface,
wherein every supporting strut in the annular ring comprises a middle section comprising a first airfoil, an outer section comprising a second airfoil, an inner section comprising a third airfoil, wherein the second airfoil comprises a positive angle of incidence that is greater than an angle of incidence of the first airfoil, wherein the third airfoil comprises a negative angle of incidence, and
wherein each supporting strut comprises a minor symmetric twin-strut that defines an in flow-direction narrowing channel there between.

Assignees

• Wong Li Shing
• Siemens Ag

Inventors

• Wong Li Shing

Classifications

• F01D5/145 Primary

  Means for influencing boundary layers or secondary circulations (for compressors F04D29/68) · CPC title

• F01D25/162

  Bearing supports · CPC title

• F05D2220/321

  for a special turbine stage · CPC title

• Y02T50/673

  Cross-Sectional Technologies · mapped topic

• F01D5/146

  of blades with tandem configuration, split blades or slotted blades · CPC title