Patent · US Active

Fuel injection device for an aircraft gas turbine

US7694899B2 · kind B2 · utility

1Cited by

0References

8Claims

0Family size

Assignee

ROLLS-ROYCE DEUTSCHLAND LTD & CO KG · DE

Inventors

Jeffrey-George Gerakis · Berlin, DE
Leif Rackwitz · Rangsdorf, DE

Key dates

Filing date	Jul 13, 2007
Grant date	Apr 13, 2010
Priority date	—
Expiry date	Jul 13, 2027

Classification

Technology area (CPC F)Mechanical Engineering; Lighting; Heating
CPC primaryF23D11/38
WIPO fieldEngines, pumps, turbines
WIPO sectorMechanical engineering

Abstract

A fuel injection device for fuel injection systems, e.g. for aircraft gas turbines, includes at least one fuel injection opening, through which a continuous flow of fuel 1 is issued, with the fuel injection opening having a non-circular cross-section.

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