Patent · US Active

Method for rinsing a fuel system of a gas turbine and associated fuel system

US9175606B2 · kind B2 · utility

4Cited by
9References
7Claims
0Family size

Assignee

Inventors

Key dates

Filing dateApr 30, 2009
Grant dateNov 3, 2015
Priority date
Expiry dateJan 1, 2032

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T137/0424
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A method for flushing a section of a fuel system of a burner of a gas turbine is provided. The method includes the steps of providing a feed line for feeding fuel from a fuel source to the burner, providing a first feed point close to the burner and a second feed point remote from the burner in the feed line in each case for feeding a medium into the feed line, feeding the medium via the first feed point, and discharging, via the burner, the fuel which is in the feed line between the first feed point and the burner, and also feeding the medium via the second feed point, and discharging, via the first feed point, the fuel which is in the feed line between the second feed point and the first feed point.

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