Patent · US Active

System and method for fuel blending and control in gas turbines

US9377202B2 · kind B2 · utility

7Cited by
34References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMar 15, 2013
Grant dateJun 28, 2016
Priority date
Expiry dateDec 6, 2034

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/678
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A system includes a gas turbine engine having a combustor, and a fuel blending system. The fuel blending system further includes a first fuel supply configured to supply a first fuel, a second fuel supply configured to supply a second fuel, a first fuel circuit, a second fuel circuit, and a controller. The first fuel circuit may be configured to blend the first fuel and the second fuel to form a first fuel mixture. The second fuel circuit may be configured to blend the first fuel and the second fuel to form a second fuel mixture. The controller may be configured to regulate blending of the first fuel mixture and the second fuel mixture based on a measured composition of the first fuel.

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