Tip leakage flow directionality control

Patent metadata

Field	Value
Publication number	US-9951629-B2
Application number	US-201314143102-A
Country	US
Kind code	B2
Filing date	Dec 30, 2013
Priority date	Jul 3, 2012
Publication date	Apr 24, 2018
Grant date	Apr 24, 2018

Abstract

An airfoil according to an exemplary aspect of the present disclosure includes, among other things, a suction sidewall and a pressure sidewall, each sidewall extending spanwise from an airfoil base and extending chordwise between a leading edge and a trailing edge. A tip wall extends chordwise from the leading edge to the trailing edge and joining respective outer spanwise ends of the suction and pressure sidewalls. A tip leakage control channel is recessed into the tip wall, the tip leakage control channel including a control channel floor that extends between a first control channel vane sidewall and a second control channel vane sidewall established by a corresponding tip leakage control vane. An internal cooling cavity is disposed between the suction sidewall and the pressure sidewall and a channel cooling aperture feeds airflow from the internal cooling cavity to the tip leakage control channel.

First claim

What is claimed is:

1. An airfoil, comprising:
a suction sidewall and a pressure sidewall, each sidewall extending spanwise from an airfoil base and extending chordwise between a leading edge and a trailing edge;
a tip wall extending chordwise from said leading edge to said trailing edge and joining respective outer spanwise ends of said suction and pressure sidewalls, including a tip rib extending chordwise along a pressure side of said tip wall;
a tip shelf disposed at a junction between said pressure sidewall and said tip rib;
a plurality of curved tip leakage control channels recessed into said tip wall, each of said plurality of curved tip leakage control channels including a control channel floor that extends between a first control channel vane sidewall and a second control channel vane sidewall established by a corresponding curved tip leakage control vane, each of said curved tip leakage control vanes contiguous with a suction side surface of said tip rib, said plurality of curved tip leakage channels extending toward said trailing edge while extending toward said suction sidewall;
an internal cooling cavity disposed between said suction sidewall and said pressure sidewall; and
a channel cooling aperture that feeds airflow from said internal cooling cavity to at least one of said curved tip leakage control channels.

2. The airfoil as recited in claim 1 , wherein said channel cooling aperture includes a curvature.

3. The airfoil as recited in claim 1 , wherein said channel cooling aperture opens through said control channel floor.

4. The airfoil as recited in claim 1 , wherein said channel cooling aperture divides said control channel floor into a first surface that is elevated relative to a second surface.

5. The airfoil as recited in claim 4 , wherein said first surface extends from a tip rib suction side of a tip rib of said tip wall and said second surface extends from said suction sidewall.

6. The airfoil as recited in claim 1 , wherein said channel cooling aperture extends to an outlet of said tip leakage control channel.

7. The airfoil as recited in claim 1 , wherein said tip wall includes a tip outer surface having a first surface and an angled surface.

8. The airfoil as recited in claim 7 , wherein said first surface extends from said tip shelf to a tip rib suction side of said tip wall.

9. The airfoil as recited in claim 7 , wherein said angled surface extends radially inwardly from said first surface into said tip leakage control channel.

10. The airfoil as recited in claim 1 , comprising a grooved BOAS radially outward of said tip wall.

11. The airfoil as recited in claim 1 , wherein at least one of said curved tip leakage control channels includes an inlet having a first chordwise width and an outlet having a second chordwise width that is different from said first chordwise width.

12. The airfoil as recited in claim 1 , wherein at least one of said curved tip leakage control channels includes an inlet having a channel entrance interior angle relative to said pressure sidewall and an outlet having a channel exit interior angle relative to said suction sidewall, and said channel entrance interior angle is different from said channel exit interior angle.

13. The airfoil as recited in claim 1 , wherein at least one of said curved tip leakage control vanes includes a leading portion forming a leading interior angle relative to said pressure sidewall and a trailing portion forming a trailing interior angle relative to said suction sidewall, and said trailing interior angle is different from said leading interior angle.

14. An airfoil, comprising:
a suction sidewall and a pressure sidewall, each sidewall extending spanwise from an airfoil base and extending chordwise between a leading edge and a trailing edge;
a tip wall extending chordwise from said leading edge to said trailing edge and joining respective outer spanwise ends of said suction and pressure sidewalls, including a tip rib extending chordwise along a pressure side of said tip wall;
a tip leakage control channel recessed into said tip wall and having an inlet and an outlet, said tip leakage control channel including a floor that extends between a first control channel vane sidewall and a second control channel vane sidewall established by corresponding curved tip leakage control vanes, each of said curved tip leakage control vanes contiguous with and extending from a suction side surface of said tip rib, said curved tip leakage control channel extending toward said trailing edge while extending toward said suction sidewall; and
an airfoil sidewall microcircuit formed in either said suction sidewall or said pressure sidewall, said airfoil sidewall microcircuit configured to feed airflow to said inlet of said tip leakage control channel, wherein said outlet is disposed at a suction side of said tip wall.

15. The airfoil as recited in claim 14 , wherein said airfoil sidewall microcircuit includes at least one curved portion configured to alter a flow direction of said airflow within said airfoil sidewall microcircuit.

16. The airfoil as recited in claim 15 , wherein said at least one curved portion communicates said airflow parallel to a control channel floor of said tip leakage control channel toward said outlet, wherein said control channel floor extends between said pressure sidewall and said suction sidewall.

17. The airfoil as recited in claim 14 , comprising an internal cooling cavity disposed between said suction sidewall and said pressure sidewall.

18. The airfoil as recited in claim 14 , wherein said airfoil sidewall microcircuit is formed in said suction sidewall.

19. The airfoil as recited in claim 14 , wherein said tip wall includes a tip shelf disposed at a junction between said pressure sidewall and said tip rib.

20. The airfoil as recited in claim 19 , comprising a cooling aperture connecting between said tip shelf and an internal cooling cavity.

21. An airfoil, comprising:
a suction sidewall and a pressure sidewall, each sidewall extending spanwise from an airfoil base and extending chordwise between a leading edge and a trailing edge;
a tip wall extending chordwise from said leading edge to said trailing edge and joining respective outer spanwise ends of said suction and pressure sidewalls and including a tip rib extending chordwise along a pressure side of said tip wall;
a tip shelf disposed at a junction between said pressure sidewall and said tip wall;
a tip leakage control channel recessed into said tip wall and having an inlet and an outlet, said tip leakage control channel including a floor that extends between a first control channel vane sidewall and a second control channel vane sidewall established by corresponding curved tip leakage control vanes, each of said curved tip leakage control vanes contiguous with and extending from a suction side surface of said tip rib, said curved tip leakage control channel extending toward said trailing edge while extending toward said suction sidewall;
an internal cooling cavity disposed between said suction sidewall and said pressure sidewall;
a channel cooling aperture in fluid communication with said internal cooling cavity; and
an airfoil sidewall microcircuit formed in either said suction sidewall or said pressure sidewall, wherein said channel cooling aperture feeds airflow to said inlet of said tip leakage control channel and said airfoil sidewall microcircuit feeds airflow to a tip shelf cooling aperture of said tip shelf.

22.

Assignees

• Zelesky Mark F
• Aggarwala Andrew S
• United Technologies Corp

Inventors

• Zelesky Mark F
• Aggarwala Andrew S

Classifications

• F01D5/186

  Film cooling (F01D5/187 takes precedence) · CPC title

• Y02T50/676

  Cross-Sectional Technologies · mapped topic

• F01D5/146

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

• F05D2240/307

  related to the tip of a rotor blade · CPC title

• Y02T50/673

  Cross-Sectional Technologies · mapped topic