Turbomachine flow divider and related turbomachine

Patent metadata

Field	Value
Publication number	US-9334746-B2
Application number	US-201213692541-A
Country	US
Kind code	B2
Filing date	Dec 3, 2012
Priority date	Dec 3, 2012
Publication date	May 10, 2016
Grant date	May 10, 2016

Abstract

Various embodiments include a turbomachine flow divider. In various particular embodiments, a flow divider for connecting with a first inner diaphragm ring and a second inner diaphragm ring of a turbomachine includes: a body section; and a pair of axially extending flanges extending from the body section, each of the axially extending flanges for engaging with the first inner diaphragm ring and the second inner diaphragm ring, respectively, wherein the flow divider is formed substantially of a rolled plate metal or a sheet metal.

First claim

We claim:

1. A turbomachine diaphragm section comprising:
a first diaphragm stage in a first turbomachine section, the first diaphragm stage having a first inner diaphragm ring and a first outer diaphragm ring;
a second diaphragm stage in a second turbomachine section opposing the first turbomachine section, the second diaphragm stage having a second inner diaphragm ring and a second outer diaphragm ring;
a flow divider connected with the first inner diaphragm ring and the second inner diaphragm ring for dividing flow of a working fluid into each of the first diaphragm stage and the second diaphragm stage, the flow divider including:
a body section having a substantially planar radially outer surface; and
a pair of axially extending flanges extending from the body section, each axially extending flange engaging with the first inner diaphragm ring and the second inner diaphragm ring, respectively,
wherein the flow divider has a radially inner surface, opposite the substantially planar radially outer surface, extending between the body section and the pair of axially extending flanges; and

a set of key members proximate a horizontal joint surface of the flow divider between at least one of the pair of axially extending flanges and at least one of the first inner diaphragm ring or the second inner diaphragm ring,
wherein the radially inner surface is coplanar with a radially inner surface of each of the set of key members, and wherein a portion of each of the set of key members is radially exposed adjacent the radially inner surface.

2. The turbomachine diaphragm section of claim 1 , wherein the first inner diaphragm ring and the second inner diaphragm ring each include a slot housing a portion of a key member from the set of key members.

3. The turbomachine diaphragm section of claim 2 , wherein the first inner diaphragm ring and the second inner diaphragm ring each include a step engaging one flange from the pair of axially extending flanges of the flow divider.

4. The turbomachine diaphragm section of claim 1 , wherein the flow divider includes a rolled plate metal or a sheet metal.

5. The turbomachine diaphragm section of claim 4 , wherein in the case that the flow divider includes sheet metal, the sheet metal has a thickness of at least 5 centimeters.

6. The turbomachine diaphragm section of claim 1 , wherein the radially inner surface is free of machining.

7. The turbomachine diaphragm section of claim 1 , wherein the set of key members restricts rotation of the flow divider relative to the first diaphragm stage and the second diaphragm stage.

8. A dual-flow turbomachine comprising:
a first section having a first diaphragm stage with a first inner diaphragm ring and a first outer diaphragm ring;
a second section opposing the first section, the second section having a second diaphragm stage with a second inner diaphragm ring and a second outer diaphragm ring;
a flow divider connected with the first inner diaphragm ring and the second inner diaphragm ring for dividing flow of a working fluid into each of the first diaphragm stage and the second diaphragm stage, the flow divider including:
a body section having a substantially planar radially outer surface; and
a pair of axially extending flanges extending from the body section, each axially extending flange engaging with the first inner diaphragm ring and the second inner diaphragm ring, respectively,
wherein the flow divider has a radially inner surface, opposite the substantially planar radially outer surface, extending between the body section and the pair of axially extending flanges; and

a set of key members proximate a horizontal joint surface of the flow divider between at least one of the pair of axially extending flanges and at least one of the first inner diaphragm ring or the second inner diaphragm ring,
wherein the radially inner surface is coplanar with a radially inner surface of each of the set of key members, and wherein a portion of each of the set of key members is radially exposed adjacent the radially inner surface.

9. The dual-flow turbomachine of claim 8 , wherein the first inner diaphragm ring and the second inner diaphragm ring each include a slot housing a portion of a key member from the set of key members.

10. The dual-flow turbomachine of claim 9 , wherein the first inner diaphragm ring and the second inner diaphragm ring each include a step engaging one flange from the pair of axially extending flanges of the flow divider.

11. The dual-flow turbomachine of claim 8 , wherein the flow divider includes a rolled plate metal or a sheet metal.

12. The dual-flow turbomachine of claim 11 , wherein, in the case that the flow divider includes sheet metal, the sheet metal has a thickness of at least 5 centimeters.

13. The dual-flow turbomachine of claim 8 , wherein the radially inner surface is free of machining.

14. The dual-flow turbomachine of claim 8 , wherein the set of key members restricts rotation of the flow divider relative to the first diaphragm stage and the second diaphragm stage.

15. The dual-flow turbomachine of claim 8 , further comprising:
a first set of nozzles extending between the first inner diaphragm ring and the first outer diaphragm ring; and
a second set of nozzles extending between the second inner diaphragm ring and the second outer diaphragm ring,
wherein the flow divider is positioned to divert the working fluid to each of the first set of nozzles and the second set of nozzles.

Assignees

• Gen Electric

Inventors

• Sankolli Prashant Prabhakar
• Burdgick Steven Sebastian

Classifications

• F01D9/047 Primary

  Nozzle boxes · CPC title

• F05D2230/26

  by rolling · CPC title

• F05D2220/31

  in steam turbines · CPC title

• F01D9/041 Primary

  using blades (F01D5/148 takes precedence) · CPC title

• F01D25/24

  Casings (modified for heating or cooling F01D25/14); Casing parts, e.g. diaphragms, casing fastenings (casings for rotary machines or engines in general F16M {; special arrangements in stators dealing with breaking-off of part of rotor F01D21/045}) · CPC title