Patent · US Active

Integral flange connection fuel nozzle body for gas turbine

US8661823B2 · kind B2 · utility

0Cited by
19References
9Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJan 5, 2010
Grant dateMar 4, 2014
Priority date
Expiry dateJan 6, 2032

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF05D2240/128
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A fuel nozzle for a gas turbine includes a fuel nozzle body or endcover. The fuel nozzle body or endcover includes at least one seal surface. The fuel nozzle also includes at least one flexible hose and at least one flange connected to the flexible hose. The at least one flange is fastened to the fuel nozzle body at the at least one seal surface.

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