Patent · US Active

Vane assemblies for gas turbine engines

US9951639B2 · kind B2 · utility

14Cited by
30References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateFeb 10, 2012
Grant dateApr 24, 2018
Priority date
Expiry dateOct 2, 2033

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T29/49245
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

Vane assemblies for gas turbine engines and methods for assembling vane assemblies are disclosed. The vane assemblies may include at least one shroud having at least one vane-receiving portion, at least one vane having at least one end portion received in the vane-receiving portion, and at least one sealing member having an uncompressed cross-section that is substantially circular. The sealing member(s) are disposed between and in contact with the end portion of the vane and the vane-receiving portion of the shroud.

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