Serpentine platform cooling structures

Patent metadata

Field	Value
Publication number	US-10054055-B2
Application number	US-201514946279-A
Country	US
Kind code	B2
Filing date	Nov 19, 2015
Priority date	Nov 19, 2015
Publication date	Aug 21, 2018
Grant date	Aug 21, 2018

Abstract

A platform is disclosed. The platform may include an airfoil section with a cooling passage and a platform. The platform may have various cooling features, such as a platform cooling apparatus. The platform cooling apparatus may have a cooling passage forming a channel disposed at least partially through the platform and the platform cooling apparatus may have an inflow channel in fluidic communication with the channel and the cooling passage so that cooling air may travel from the cooling cavity of the blade airfoil section and into the platform cooling apparatus. Moreover, the platform cooling apparatus may have a cooling cover apparatus at least partially fluidically sealing the platform cooling apparatus.

First claim

What is claimed is:

1. A platform comprising:
a platform cooling apparatus comprising a cooling passage comprising a channel disposed at least partially through the platform and configured to conduct cooling air,
wherein the cooling passage comprises a serpentine portion comprising a first plurality of folded channels comprising at least one turn;
wherein the platform cooling apparatus further comprises an outflow aperture comprising an orifice extending in fluidic communication between the cooling passage of the platform cooling apparatus and through at least a portion of the platform and in fluidic communication with a surrounding ambient environment immediately proximate to a surface of the rotor blade;
a cooling cover apparatus at least partially fluidically sealing the platform cooling apparatus; and
a defined gap comprising an opening between the cooling cover apparatus and the platform
whereby the cooling air may escape from the cooling passage.

2. The platform according to claim 1 , wherein the platform cooling apparatus further comprises:
an inflow channel configured to receive the cooling air from a cooling cavity of an airfoil section and convey it to the cooling passage.

3. The platform according to claim 2 , further comprising heat transfer enhancement features disposed within the cooling passage.

4. The platform according to claim 1 , wherein the folded channels comprise parallel folded channels and wherein the at least one turn comprises a 180-degree turn.

5. The platform according to claim 2 , further comprising
a rib disposed between the folded channels.

6. The platform according to claim 5 , wherein the cooling passage further comprises a terminal portion comprising an end of the cooling passage forming a terminus of the cooling passage.

7. The platform according to claim 6 , wherein the platform cooling apparatus further comprises outflow apertures disposed through the terminal portion of the cooling passage and connecting the cooling passage in fluidic communication with a surrounding ambient environment immediately proximate to a surface of the platform.

8. The platform according to claim 5 , further comprising a retention mechanism to retain the cooling cover apparatus in mechanical communication with the platform proximate to the platform cooling apparatus.

9. The platform according to claim 8 , wherein the retention mechanism comprises an integral formation comprising an integral joining of the cooling cover apparatus to the platform.

10. The platform according to claim 8 , wherein the cooling cover apparatus comprises a cover plate comprising a plate structure disposed radially inward of the platform cooling apparatus and configured to at least partially fluidically seal the platform cooling apparatus.

11. The platform according to claim 10 , wherein the retention mechanism comprises a weld.

12. The platform according to claim 11 , wherein the weld comprises a perimeter weld comprising welding extending around all edges of the cover plate.

13. The platform according to claim 11 , wherein the weld comprises a platform edge weld comprising welding extending along a single edge of the cover plate.

14. The platform according to claim 11 ,
wherein the weld comprises a rib weld comprising welding extending along the rib of the platform cooling apparatus and joining the rib to the cover plate.

15. A rotor blade comprising:
a blade airfoil section comprising a cooling cavity; and
a platform comprising:
a platform cooling apparatus comprising a cooling passage comprising a channel disposed at least partially through the platform and comprising an inflow channel in fluidic communication with the cooling cavity and the cooling passage;

wherein the cooling passage further comprises an outflow aperture comprising an orifice extending in fluidic communication between the cooling passage of the platform cooling apparatus and through at least a portion of the platform and in fluidic communication with a surrounding ambient environment immediately proximate to a surface of the rotor blade;
a cooling cover apparatus at least partially fluidically sealing the platform cooling apparatus; and
a defined gap comprising an opening between the cooling cover apparatus and the platform whereby the cooling air may escape from the cooling passage.

16. A rotor blade according to claim 15 , wherein the platform further comprises heat transfer enhancement features disposed within the cooling passage.

17. A method of forming a platform comprising:
forming a platform cooling apparatus comprising a cooling passage comprising a channel disposed at least partially through the platform and configured to conduct cooling air,
wherein the cooling passage comprises a serpentine portion comprising a first plurality of folded channels comprising at least one turn;
wherein the cooling passage further comprises an outflow aperture comprising an orifice extending in fluidic communication between the cooling passage of the platform cooling apparatus and through at least a portion of the platform and in fluidic communication with a surrounding ambient environment immediately proximate to a surface of the rotor blade; and
forming a cooling cover apparatus at least partially fluidically sealing the platform cooling apparatus, wherein the cooling cover apparatus at least partially defines a gap comprising an opening between the cooling cover apparatus and the platform whereby the cooling air may escape from the cooling passage.

Assignees

• United Technologies Corp
• United Technologies Corp

Inventors

• Spangler Brandon W
• Pietraszkiewicz Edward F

Classifications

• F01D5/18

  Hollow blades, {i.e. blades with cooling or heating channels or cavities (structure of hollow blades in general F01D5/147)}; Heating, heat-insulating or cooling means on blades · CPC title

• F02C7/18 Primary

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

• F01D5/08

  Heating, heat-insulating or cooling means {(specially adapted for radial flow machines or engines F01D5/04)} · CPC title

• F01D5/187 Primary

  Convection cooling · CPC title

• F05D2260/205

  Cooling fluid recirculation, i.e. after cooling one or more components is the cooling fluid recovered and used elsewhere for other purposes · CPC title