Particle separator assembly for a turbine engine

Patent metadata

Field	Value
Publication number	US-11090600-B2
Application number	US-201715397797-A
Country	US
Kind code	B2
Filing date	Jan 4, 2017
Priority date	Jan 4, 2017
Publication date	Aug 17, 2021
Grant date	Aug 17, 2021

Abstract

A method and apparatus for a turbine engine having a compressor section, combustion section, and a turbine section in an axial flow arrangement with a cooling circuit in fluid communication with at least one of the compressor section, combustion section, or turbine section. The method and apparatus further including separating particles from a cooling air that flows through the cooling circuit.

First claim

What is claimed is:

1. A turbine engine comprising:
an engine core having a compressor section, combustion section, and a turbine section in an axial flow arrangement;
a cooling air circuit in fluid communication with at least one of the compressor section, combustion section, or turbine section;
a particle separator fluidly coupled to the cooling air circuit;
the particle separator comprising:
a housing defining an airflow passage comprising an inlet and an outlet, and through which passes a primary airflow from the cooling air circuit;
a structural duct disposed within the airflow passage between the inlet and the outlet such that the primary airflow flows outside of the structural duct and a scavenge passage is formed within the structural duct; the structural duct further defining parallel facing, planar walls spaced from each other to form an elongated opening defining a particle drain defining a particle path from the airflow passage outside of the structural duct into the scavenge passage within the structural duct in a different direction from the primary airflow; and
a heat exchanger having at least one fluid channel formed in a wall of the housing and fluidly separate from the airflow passage, the wall defining at least a portion of the airflow passage and the at least one fluid channel having an extent along the airflow passage between the inlet and the outlet that overlaps with an extent of the particle drain along the airflow passage between the inlet and the outlet.

2. The turbine engine of claim 1 wherein the particle separator and the heat exchanger define a monolithic structure.

3. The turbine engine of claim 1 wherein the at least one fluid channel comprises multiple fluid channels.

4. The turbine engine of claim 3 wherein at least some of the multiple fluid channels are of the same length.

5. The turbine engine of claim 3 wherein all of the multiple fluid channels am of the same length.

6. The turbine engine of claim 1 wherein the housing has a body-axis and the housing has a non-constant dimension relative to the body-axis.

7. The turbine engine of claim 6 wherein at least a portion of the housing is a wave form and the body-axis is centrally located with respect to the particle separator and the non-constant dimension is a length measured from the body-axis.

8. The turbine engine of claim 1 wherein the particle separator is fluidly coupled to a modulation apparatus.

9. The turbine engine of claim 1 wherein the structural duct further defines a set of plenums.

10. The turbine engine of claim 9 wherein the structural duct further defines sloping surfaces terminating in the parallel facing, planar walls.

11. The turbine engine of claim 10 wherein the set of plenums defines multiple chambers and the particle drain separates two of the multiple chambers and is fluidly coupled directly to a third chamber.

12. The turbine engine of claim 1 wherein the different direction is a second direction perpendicular to the primary airflow.

13. A particle separator assembly comprising:
a housing including at least one wall defining an airflow passage comprising an inlet and an outlet, and through which passes an airflow;
a structural duct disposed within the airflow passage between the inlet and the outlet such that the airflow flows outside the structural duct and a scavenge passage is formed within the structural duct;
the structural duct further defining parallel facing, planar walls spaced from each other to form an elongated opening defining a particle drain to conduct particles from the airflow passage outside the structural duct into the scavenge passage within the structural duct along a particle path extending in a different direction than the airflow; and
a heat exchanger forming a monolithic structure with the housing, the heat exchanger having a fluid channel fluidly separated from the airflow passage and formed in the at least one wall, the wall defining at least a portion of the airflow passage and the fluid channel having an extent along the airflow passage between the inlet and the outlet that overlaps with an extent of the particle drain along the airflow passage between the inlet and the outlet.

14. The particle separator assembly of claim 13 wherein the fluid channel comprises multiple fluid channels.

15. The particle separator assembly of claim 14 wherein at least some of the multiple fluid channels are of the same length.

16. The particle separator assembly of claim 14 wherein all of the multiple fluid channels are of the same length.

17. The particle separator assembly of claim 13 wherein the housing with a body-axis and the housing has a non-constant dimension relative to the body-axis.

18. The particle separator assembly of claim 17 where the housing is a wave form and the body-axis is centrally located with respect to the particle separator and the non-constant dimension is a length measured from the body-axis.

19. The particle separator assembly of claim 13 wherein the particle separator is fluidly coupled to a modulation apparatus.

20. The particle separator assembly of claim 13 wherein the structural duct further defines a set of plenums.

21. The particle separator assembly of claim 20 wherein the structural duct further defines sloping surfaces terminating in the parallel facing, planar walls.

22. The particle separator assembly of claim 21 wherein the set of plenums defines multiple chambers and the particle drain separates two of the multiple chambers and is fluidly coupled directly to a third chamber.

23. The particle separator assembly of claim 13 wherein the different direction is a second direction perpendicular to the airflow.

Assignees

• Gen Electric

Inventors

• Rambo Jeffrey Douglas

Classifications

• Y02T50/60

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

• B01D50/40

  Combinations of devices covered by groups B01D45/00 and B01D47/00 · CPC title

• F05D2250/232

  conical · CPC title

• F05D2260/607

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

• B04C5/20

  with heating or cooling, e.g. quenching, means · CPC title