Exhaust diffuser and method for manufacturing an exhaust diffuser

Patent metadata

Field	Value
Publication number	US-9631624-B2
Application number	US-201214237873-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 herein. The exhaust diffuser having an inner member, the 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, at least 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, the first supporting strut having a middle section having a first airfoil and an outer section having a second airfoil, and the second airfoil differing from the first airfoil in shape to be able to handle a higher range of angle of attack. 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 differing from the first airfoil in shape to be able to handle a higher range of angle of attack with respect to the first airfoil, and
wherein: the first airfoil comprises a smaller leading edge radius than the second airfoil and the third airfoil; or the first airfoil comprises a smaller camber than the second airfoil and the third airfoil; or the second airfoil comprises a higher angle of incidence than the first airfoil and the third airfoil comprises a lower angle of incidence than the first airfoil.

2. The exhaust diffuser for a torque-generating turbine of claim 1 , the third airfoil differing from the first airfoil in shape to be able to handle a higher range of angle of attack with respect to the first airfoil.

3. The exhaust diffuser for a torque-generating turbine of claim 2 , the first airfoil having a smaller thickness than the second airfoil and/or the third airfoil.

4. The exhaust diffuser for a torque-generating turbine of claim 2 , the first airfoil having the smaller leading edge radius than the second airfoil and/or the third airfoil.

5. The exhaust diffuser for a torque-generating turbine of claim 2 , the first airfoil having the smaller camber than the second airfoil and/or the third airfoil.

6. The exhaust diffuser for a torque-generating turbine of claim 1 , the second airfoil having the higher angle of incidence than the first airfoil.

7. The exhaust diffuser for a torque-generating turbine of claim 2 , the third airfoil having the lower angle of incidence than the first airfoil.

8. 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.

9. 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.

10. The exhaust diffuser for a torque-generating turbine of claim 1 , comprising eight or fewer first supporting struts and/or second supporting struts.

11. The exhaust diffuser for a torque-generating turbine of claim 1 , wherein the exhaust diffuser has four or fewer twin-struts.

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

13. The exhaust diffuser for a torque-generating turbine of claim 1 , wherein the exhaust diffuser has 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. A torque-generating turbine comprising, in order of a gas flow, a compressor, a combustor, a turbine and the exhaust diffuser as claimed in claim 1 .

16. A torque-generating turbine as claimed in claim 15 and having a stack, the stack located downstream of the exhaust diffuser.

17. A torque-generating turbine as claimed in claim 15 , wherein the turbine has at least two stages, one stage driving the compressor and another stage driving a generator.

Assignees

• Wong Li Shing
• Siemens Ag

Inventors

• Wong Li Shing

Classifications

• F05D2240/12

  Fluid guiding means, e.g. vanes · CPC title

• F01D25/30

  Exhaust heads, chambers, or the like · CPC title

• F04D19/022 Primary

  with concentric rows of vanes; · CPC title

• F05D2220/321

  for a special turbine stage · CPC title

• F01D5/145 Primary

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