Method of manufacturing recuperator air cells

Patent metadata

Field	Value
Publication number	US-9845729-B2
Application number	US-201314048186-A
Country	US
Kind code	B2
Filing date	Oct 8, 2013
Priority date	Oct 8, 2013
Publication date	Dec 19, 2017
Grant date	Dec 19, 2017

Abstract

A method of manufacturing a recuperator segment uses metal tubes deformed into air cells in a waved configuration. The air cells are stacked one to another to form a double skinned recuperator segment providing cold air passages through the respective air cells and hot gas passages through spaces between adjacent air cells.

First claim

The invention claimed is:

1. A method of manufacturing a heat recuperator segment, comprising:
a) providing a plurality of metal tubes having an initial cross-sectional area;
b) in a pressing process plastically deforming each of the plurality of metal tubes, including flattening each metal tube into an air cell having a flattened cross-sectional area different from the initial cross-sectional area, each air cell having top and bottom skins to define opposed closed sides and opposed open ends, each of the air cells defining a double skinned wall having a waved configuration including a plurality of wave tops and wave bottoms alternately formed in two directions;
c) stacking the air cells one upon another to form a stacked double skinned wall configuration of the recuperator segment such that the wave bottoms of one of the air cells are supported on the wave tops of an adjacent one of the air cells, thereby providing cold air passages defined in the respective air cells and extending through the recuperator segment, and thereby forming hot gas passages through the recuperator segment between the adjacent air cells; and
d) retaining the stacked air cells in position.

2. The method as defined in claim 1 wherein step (b) is conducted such that the wave tops and wave bottoms are alternately positioned in both transverse and longitudinal directions of the tube.

3. The method as defined in claim 1 wherein step (b) is conducted such that one of the wave tops is positioned adjacent four of the of the wave bottoms, and one of the wave bottoms is positioned adjacent four of the wave tops.

4. The method as defined in claim 1 wherein step (b) is conducted by first pressing each metal tube into a substantially flat form having an elliptical cross-section and then further deforming the tube of substantially flat form into the waved configuration.

5. The method as defined in claim 1 wherein step (b) is conducted by pressing each tube such that the top and bottom skins are positioned against each other, the top and bottom skins thereby simultaneously forming a required corrugated shape, and then internally pressurizing the tube to re-position the top and bottom skins to be spaced apart from each other in a predetermined dimension in order to form the air cell having the waved configuration.

6. The method as defined in claim 1 wherein step (b) is conducted by deforming each tube into the waved configuration such that the wave tops and wave bottoms are substantially flat.

7. The method as defined in claim 6 wherein step (c) is conducted by placing the substantially flat wave bottoms of at least one air cell upon the substantially flat wave tops of an adjacent one of the air cells.

8. The method as defined in claim 1 further comprising a step of selecting tube diameters to meet a required surface area of each air cell.

9. The method as defined in claim 1 further comprising a step of selecting tubes having a tube wall thickness in a range between 0.0254 mm (0.001 inches) and 0.203 mm (0.008 inches).

10. The method as defined in claim 1 further comprising a step of preparing the tubes to have a length to meet a required length of the recuperation segment.

Assignees

• Pratt & Whitney Canada

Inventors

• Eleftheriou Andreas
• Alecu Daniel
• Menheere David

Classifications

• F28F1/02

  Tubular elements of cross-section which is non-circular (F28F1/08, F28F1/10 take precedence) · CPC title

• F28D7/0041

  the conduits for only one medium being tubes having parts touching each other or tubes assembled in panel form (F28D7/0008, F28D7/0058 take precedence) · CPC title

• F02C7/08 Primary

  Heating air supply before combustion, e.g. by exhaust gases · CPC title

• F28D2021/0026

  for combustion engines, e.g. for gas turbines or for Stirling engines · CPC title

• F28D7/082

  with serpentine or zig-zag configuration · CPC title