Patent · US Active

Combustion chamber for a gas turbine

US10024540B2 · kind B2 · utility

0Cited by

2References

10Claims

0Family size

Assignee

Siemens Aktiengesellschaft · DE

Inventors

Peter Kaufmann · Munich, DE
Werner Krebs · Wetter (Ruhr), DE

Key dates

Filing date	Jan 24, 2008
Grant date	Jul 17, 2018
Priority date	—
Expiry date	Jun 27, 2031

Classification

Technology area (CPC Y)Emerging Cross-Sectional Technologies
CPC primaryY02E20/34
WIPO fieldEngines, pumps, turbines
WIPO sectorMechanical engineering

Abstract

A combustion chamber for a gas turbine is provided. The combustion chamber comprises at least one first and one second jet carrier, of which at least one is provided for injecting an operating gas in the combustion chamber such that waste gas formed in the flame zone thereof is circulated to a mixing zone of the first jet carrier. In order to achieve a compact combustion chamber, the jet carriers are positioned in relation to each other such that waste gas from the flame zone of the first jet carrier flows directly to the mixing zone of the second jet carrier.

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