Gas turbine combustion chamber with defined fuel input for the improvement of the homogeneity of the fuel-air mixture

US7086234B2 · kind B2 · utility

Assignee

• ROLLS-ROYCE DEUTSCHLAND LTD & CO KG · DE

Inventors

• Thomas Doerr · Berlin, DE
• Waldemar Lazik · Berlin, DE

Key dates

• Filing date: May 5, 2003
• Grant date: Aug 8, 2006
• Expiry date: May 5, 2023

Classification

• Technology area (CPC Y): Emerging Cross-Sectional Technologies
• CPC primary: Y02T50/60
• WIPO field: Engines, pumps, turbines
• WIPO sector: Mechanical engineering

Abstract

A gas turbine combustion chamber with a burner 7, includes means for the supply of fuel and an atomizer 6, wherein the means for the supply of fuel are provided such that the fuel is injected in areas with maximum airflow velocity.