Patent · US Active

Combustion chamber of a combustor for a gas turbine

US9885480B2 · kind B2 · utility

0Cited by

3References

12Claims

0Family size

Assignee

Siemens Aktiengesellschaft · DE

Inventors

Magnus Hasselqvist · Finspång, SE
Frank Rubensdorffer · Hällestad, SE

Key dates

Filing date	Dec 21, 2012
Grant date	Feb 6, 2018
Priority date	—
Expiry date	Aug 19, 2033

Classification

Technology area (CPC F)Mechanical Engineering; Lighting; Heating
CPC primaryF23R2900/03043
WIPO fieldEngines, pumps, turbines
WIPO sectorMechanical engineering

Abstract

A combustion chamber of a combustor for a gas turbine is provided. A combustion chamber includes a plurality of segments arranged annularly about an axis of the combustion chamber, each segment comprising a radial inner wall portion and a radial outer wall portion, a first section comprising an opening for the installation of a burner, and a second section at which at least one airfoil extends between the radial inner wall portion and radial outer wall portion of the segment.

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