Patent · US Active

Gas turbine engine fuel injector

US11840961B2 · kind B2 · utility

0Cited by
31References
14Claims
0Family size

Assignee

Inventors

Key dates

Filing dateDec 2, 2020
Grant dateDec 12, 2023
Priority date
Expiry dateFeb 15, 2041

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF23R2900/00005
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

The subject matter of this specification can be embodied in, among other things, a fuel injector for a gas turbine engine includes a fuel injector housing, and an elongated fuel tube held in position in said housing by spaced apart joints and including an undulating tube surface along at least a portion of its length between said joints, said undulating tube surface being in contact with another surface disposed in said housing at one or more locations of said undulating tube surface.

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