Impingement cooling arrangement having a snap-in plate

Patent metadata

Field	Value
Publication number	US-10100737-B2
Application number	US-201313895831-A
Country	US
Kind code	B2
Filing date	May 16, 2013
Priority date	May 16, 2013
Publication date	Oct 16, 2018
Grant date	Oct 16, 2018

Abstract

A cooling arrangement (100), including: a substrate having a pocket (24) defined by a rib side surface (28) and a bottom surface (26); a feature (112) formed in the rib side surface; and an impingement plate (102). In an installed configuration (116) a resilience of the impingement plate enables an interference between the impingement plate and the feature that locks the impingement plate in an installed position (118). An elastic compression of the impingement plate from the installed configuration eliminates the interference.

First claim

The invention claimed is:

1. A cooling arrangement, comprising: a substrate comprising a pocket defined by a rib side surface extending radially outward from a bottom surface; a feature formed in the rib side surface; an impingement plate, wherein in an installed configuration, a resilience of the impingement plate enables an interference between the impingement plate and the feature that locks the impingement plate in an installed position, wherein an elastic compression of the impingement plate from the installed configuration eliminates the interference permitting removal of the impingement plate; wherein the impingement plate comprises a slit to permit the elastic compression; wherein the impingement plate comprise a perimeter portion, an impingement portion, and a transition region connecting the perimeter portion and the impingement portion; wherein the perimeter portion engages with the feature formed in the rib side surface to enable the interference; wherein an average slope of an outer surface of the transition region forms an acute angle with the rib side surface of at least 60 degrees; and wherein the transition region extends from the perimeter portion in a direction radially outward from the bottom surface.

2. The arrangement of claim 1 , wherein a rib comprising the rib side surface further comprises a rib top surface directly exposed to a cooling fluid above the impingement plate.

3. The arrangement of claim 2 , wherein when the impingement plate is in the installed position, a majority of the rib side surface is directly exposed to the cooling fluid.

4. The arrangement of claim 1 , wherein when the impingement plate is in the installed position the perimeter portion is disposed closer to the bottom surface than is the impingement portion.

5. The arrangement of claim 4 , wherein the elastic compression comprises an elastic deformation of the transition region to eliminate the interference.

6. The arrangement of claim 4 , wherein the impingement plate further comprises a compression aid feature.

7. The arrangement of claim 1 , wherein the feature formed in the rib side surface comprises a slot extending along the rib side surface.

8. The arrangement of claim 7 , wherein when in the installed position the perimeter portion of a perimeter of the impingement plate fits in the slot.

9. A gas turbine engine component comprising the cooling arrangement of claim 1 .

Assignees

• Little David A
• Johnson Clifford E
• Siemens Energy Inc

Inventors

• Little David A
• Johnson Clifford E

Classifications

• F02C7/18 Primary

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

• F23R2900/03044

  Impingement cooled combustion chamber walls or subassemblies · CPC title

• F23R2900/03042

  Film cooled combustion chamber walls or domes · CPC title

• F23R3/002

  Wall structures (F23R3/02 and F23R3/007 take precedence) · CPC title

• F05D2260/201

  by impingement of a fluid · CPC title