Patent · US Active

Gas turbine exhaust sound suppressor and associated methods

US7717229B2 · kind B2 · utility

9Cited by
34References
23Claims
0Family size

Assignee

Inventor

Key dates

Filing dateMay 9, 2008
Grant dateMay 18, 2010
Priority date
Expiry dateJul 16, 2028

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF02K1/827
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

The gas turbine exhaust sound suppressor, or exhaust silencer, and method are for a gas turbine and reduce low frequency exhaust flow noise while avoiding the creation of additional acoustical standing waves, e.g. from wake shedding at certain predictable frequencies. A plurality of elongated flow obstruction members, e.g. pipes or airfoils, extend within the exhaust passage to reduce acoustic waves within the exhaust flow, and at least some of the elongated flow obstruction members have different widths. Each of the elongated flow obstruction members is positioned at a respective angle within a predetermined angular range transverse to the flow direction, with the predetermined angular range being greater than or equal to 10 degrees from normal to the flow direction.

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