Patent · US Active

Injectors for gas turbine combustion chamber

US10527287B2 · kind B2 · utility

2Cited by
3References
8Claims
0Family size

Assignee

Inventors

Key dates

Filing dateApr 6, 2017
Grant dateJan 7, 2020
Priority date
Expiry dateApr 6, 2037

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF23R3/56
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

An injector for a gas turbine combustion chamber, includes a fluid feed system; an injector body extending along a longitudinal axis; an injection head arranged on the injector body and configured to spray the fluid in a direction that is inclined relative to the longitudinal axis; and an actuator configured to turn the injector selectively about the longitudinal axis so as to vary the direction in which the fluid is sprayed; wherein the actuator is configured to enable the orientation of the injector to be varied by turning about the longitudinal axis through an amplitude less than or equal to 90°.

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