Patent · US Active

Gas turbine engine combustor with integrated combustor vane

US9404654B2 · kind B2 · utility

7Cited by
42References
19Claims
0Family size

Assignee

Inventors

Key dates

Filing dateSep 26, 2012
Grant dateAug 2, 2016
Priority date—
Expiry dateOct 9, 2033

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/60
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A combustor section for a gas turbine engine includes a combustor vane which extends at least partially into a combustion chamber.

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