Patent · US Active

Burner component of a burner, and burner of a gas turbine having a burner component of this type

US12050012B2 · kind B2 · utility

0Cited by
11References
18Claims
0Family size

Assignee

Inventors

Key dates

Filing dateDec 10, 2020
Grant dateJul 30, 2024
Priority date
Expiry dateDec 10, 2040

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF23D2900/14003
  • WIPO fieldThermal processes and apparatus
  • WIPO sectorMechanical engineering

Abstract

A burner component of a burner. The burner has a flow channel, in which combustion air flows in a flow direction from upstream to downstream. The burner component includes a wall portion, which adjoins the flow channel; a plurality of injection nozzles, which are arranged in the wall portion; and a plurality of vortex generators, which are arranged on the wall portion. The vortex generators have a concavely curved sloped surface rising in the flow direction to improve the distribution of the fuel in the combustion air.

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