Turbine engine and particle separators therefore

Patent metadata

Field	Value
Publication number	US-11033845-B2
Application number	US-201515314536-A
Country	US
Kind code	B2
Filing date	May 29, 2015
Priority date	May 29, 2014
Publication date	Jun 15, 2021
Grant date	Jun 15, 2021

Abstract

A turbine engine having a bypass fluid conduit coupled to the turbine section includes at least one particle separator located within the bypass fluid conduit to separate particles from a bypass fluid stream prior to the bypass stream reaching the turbine section for cooling. A centrifugal separator for removing particles from a fluid stream includes an angular velocity increaser, a particle outlet, an angular velocity decreaser downstream of the angular velocity increaser, and a bend provided between the angular velocity increaser and the angular velocity decreaser.

First claim

What is claimed is:

1. A turbine engine comprising:
a fan providing an ambient air stream through the turbine engine;
a compressor section which receives the ambient air stream and emits a compressed stream;
a combustion section which receives the compressed stream and emits a combustion stream which is at a higher temperature than the compressed stream;
a turbine section which receives the combustion stream and emits an exhaust stream which is at a lower temperature than the combustion stream;
a rotatable drive shaft coupling a portion of the turbine section with a portion of the compressor section and defining a rotational axis for the turbine engine;
a bypass fluid conduit coupling either the fan or the compressor section to the turbine section while bypassing at least the combustion section to supply either a portion of the ambient air stream or a portion of the compressed stream, respectively, to the turbine section to define a bypass stream;
at least one particle separator fixedly located in the turbine engine for non-rotation relative to the rotational axis and further located within the bypass fluid conduit wherein the at least one particle separator comprises a separation chamber having:
a separator inlet receiving the bypass stream;
a separator outlet fluidly coupled with the turbine section to form a reduced-particle stream that is provided to the turbine section for cooling; and
a particle outlet receiving a concentrated-particle stream comprising the separated particles;

at least one stationary vane located within the turbine section, wherein the at least one stationary vane includes a root and a tip at least partially defining an interior; and
a conduit passing through the interior of the at least one stationary vane from the tip to the root and isolated from the interior, wherein the conduit is in fluid communication with the particle outlet for receiving the concentrated-particle stream from the at least one particle separator.

2. The turbine engine according to claim 1 , wherein the particle separator further comprises:
a particle concentrator located within the bypass fluid conduit and concentrating at least some of the particles entrained in the bypass stream from one portion of the bypass stream into another portion of the bypass stream to functionally provide the bypass stream with a concentrated-particle stream and the reduced-particle stream; and
a flow splitter having the particle outlet downstream of the particle concentrator and located to receive at least a portion of the concentrated-particle stream to split the at least a portion of the concentrated-particle stream from the reduced-particle stream.

3. The turbine engine according to claim 2 , wherein the particle concentrator comprises an angular velocity increaser.

4. The turbine engine according to claim 2 , wherein the particle concentrator comprises a turn in the bypass fluid conduit.

5. The turbine engine according to claim 4 , wherein the turn effects at least a 45 degree change of direction of the bypass stream.

6. The turbine engine according to claim 4 , wherein the turn comprises a continuous portion, or a winding portion, of the bypass fluid conduit.

7. The turbine engine according to claim 1 and further comprising an inducer having an inducer inlet fluidly coupled with the at least one particle separator to receive the reduced-particle stream and an inducer outlet supplying the reduced-particle stream to the turbine section.

8. The turbine engine according to claim 1 , wherein the interior of the at least one vane is in fluid communication with the separator outlet for cooling by the reduced-particle stream from the at least one particle separator.

9. The turbine engine according to claim 1 , wherein the turbine section comprises at least two turbine stages, with an inter-stage cavity between the at least two turbine stages, and wherein the conduit is in fluid communication with the inter-stage cavity to supply the concentrated-particle stream to the inter-stage cavity.

10. The turbine engine according to claim 1 , wherein the bypass fluid conduit comprises at least one baffle configured to force the bypass stream to turn to separate particles from the bypass stream prior to the bypass stream reaching the at least one vane.

11. The turbine engine according to claim 10 , wherein the bypass fluid conduit is fluidly coupled to the compressor section, and the compressor section comprises at least one particle collector configured to collect the particles separated by the at least one baffle.

12. The turbine engine according to claim 10 , wherein the at least one baffle defines a substantially 180° turn for the bypass stream, or comprises multiple baffles.

13. A centrifugal separator for removing particles from a bypass fluid stream in a fluid conduit that bypasses a combustion section of a turbine engine, comprising:
a body having a wall defining a through passage, with a separator inlet configured to receive the bypass fluid stream and a separator outlet configured to couple with a turbine section of the turbine engine to form a reduced-particle stream that is provided to the interior of at least one stationary vane in the turbine section for cooling;
an angular velocity increaser located within the through passage downstream of the separator inlet and configured to increase the angular velocity of the bypass fluid stream entering the separator inlet as the bypass fluid stream passes through the through passage;
a particle outlet configured to receive a concentrated-particle stream containing particles urged toward the wall and to direct the concentrated-particle stream to a conduit within and isolated from the interior of the at least one stationary vane, the conduit being in fluid communication with an exterior of the at least one stationary vane to cool the exterior;
an angular velocity decreaser located within the through passage, downstream of the angular velocity increaser and upstream of the separator outlet, and configured to decrease the angular velocity of the reduced-particle stream prior to passing through the separator outlet; and
a bend provided in the body between the angular velocity increaser and the angular velocity decreaser.

14. The centrifugal separator of claim 13 , wherein the angular velocity increaser and the angular velocity decreaser respectively increase and decrease the angular velocity of the bypass fluid stream by substantially opposite amounts.

15. The centrifugal separator of claim 13 , wherein at least one of the angular velocity increaser and the angular velocity decreaser comprises a plurality of stationary vanes.

16. The centrifugal separator of claim 15 , wherein the plurality of stationary vanes are circumferentially spaced relative to a centerline of the through passage.

17. The centrifugal separator of claim 13 , wherein the particle outlet comprises an outlet passage having an inlet opening adjacent the wall, wherein the angular velocity decreaser is located downstream of the outlet passage.

18. The centrifugal separator of claim 17 , wherein the wall defines a diameter D, and the inlet opening is located 1-20 D downstream from the angular velocity increaser.

19. The centrifugal separator of claim 18 , wherein the outlet passage extends radially inwardly into the through passage between 1%-20% of the diameter D in a downstream direction.

20. The centrifugal separator of claim 18 , wherein the inlet opening defines a radial segment R of 1%-10% of the diameter D.

Assignees

• Gen Electric

Inventors

• Stone Timothy Deryck
• Laskowski Gregory Michael
• Proctor Robert
• Stover Curtis
• Manning Robert Francis
• Correia Victor Hugo Silva
• Buhler Jared Peter
• Murray Robert Carl
• Bourassa Jr Corey
• Pritchard Byron Andrew
• Ratzlaff Jonathan Russell

Classifications

• F01D9/065

  Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids (see also F01D25/16, F01D25/24 and F01D25/26) · CPC title

• F02C7/052

  with dust-separation devices · CPC title

• Y02T50/60

  Efficient propulsion technologies, e.g. for aircraft · CPC title

• F02C7/18

  the medium being gaseous, e.g. air {(F02C7/125 takes precedence)} · CPC title

• F05D2260/607

  Preventing clogging or obstruction of flow paths by dirt, dust, or foreign particles · CPC title