Patent · US Active

Turbulator structure on combustor liner

US10378767B2 · kind B2 · utility

5Cited by
13References
7Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJan 12, 2016
Grant dateAug 13, 2019
Priority date
Expiry dateDec 6, 2037

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF23R2900/03045
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A method of manufacturing a hot gas wall for a gas turbine is described. The method is carried out on a hot gas wall having a wall part with a front side and a back side, the wall part being for exposure to a hot fluid on the front side, and the hot gas wall also having a turbulator structure. In an exemplary embodiment, a turbulator structure is attached to the wall by placing a braze foil on the back side of the wall part, placing a turbulator structure on the braze foil, and brazing to attach the turbulator structure to the wall part. In another embodiment, the turbulator structure is attached by passing a current through the turbulator structure part and the wall part to resistance weld the turbulator structure part to the wall part.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.