Patent · US Active

Burner inserts for a gas turbine combustion chamber and gas turbine

US9074771B2 · kind B2 · utility

1Cited by
7References
14Claims
0Family size

Assignee

Inventors

Key dates

Filing dateSep 14, 2009
Grant dateJul 7, 2015
Priority date
Expiry dateFeb 16, 2032

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF23R2900/03042
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A burner insert for a gas turbine combustion chamber is provided. The burner insert includes a burner insert wall including a cold side and a hot side, an edge delimiting the burner insert wall. The edge includes an edge bar extending at least partially circumferentially and projecting beyond the cold side. A burner opening for inserting a burner is formed in the burner insert wall.

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