Patent · US Active

Axially segmented guide vane mount for a gas turbine

US8870526B2 · kind B2 · utility

1Cited by
19References
8Claims
0Family size

Assignee

Inventors

Key dates

Filing dateSep 10, 2009
Grant dateOct 28, 2014
Priority date
Expiry dateMay 12, 2031

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF01D25/246
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A stator blade carrier for a gas turbine is provided. The stator blade carrier includes a plurality of axial segments. At least one axial segment is designed as a tubular lattice structure. This allows a simpler design technically and a more flexible adaptation to the temperature profile present on the stator blade carrier to maintain operational safety.

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