Patent · US Active

Gas turbine internal manifold mounting arrangement

US8171738B2 · kind B2 · utility

16Cited by
14References
14Claims
0Family size

Assignee

Inventors

Key dates

Filing dateOct 24, 2006
Grant dateMay 8, 2012
Priority date
Expiry dateJul 31, 2029

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T29/4932
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A mounting system supporting and positioning an internal fuel manifold of a gas turbine engine includes at least a heat shield surrounding a fuel inlet of the fuel manifold, the heat shield bearing at least a portion of a load to support the fuel manifold.

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