Patent · US Active

Systems and methods for reducing noise from jet engine exhaust

US7966826B2 · kind B2 · utility

18Cited by
34References
22Claims
0Family size

Assignee

Inventors

Key dates

Filing dateFeb 14, 2007
Grant dateJun 28, 2011
Priority date
Expiry dateJul 22, 2027

Classification

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

Abstract

Jet engine nozzles with projections (e.g., chevrons) and injected flow, and associated systems and methods are disclosed. A method in accordance with one embodiment includes generating a first flow of gas with a jet engine, delivering the first flow through a nozzle having a trailing edge perimeter that includes multiple projections extending in an aft direction, and injecting a pressurized second flow of fluid into the first flow proximate to the projections. In other embodiments, other mixing enhancement devices (e.g., vortex generators) are carried by the projections. It is expected that the combination of the projections and the mixing enhancement devices will reduce engine exhaust noise levels below the levels achievable with either projections or injected flow individually.

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