Patent · US Active

Turbine blade and gas turbine equipped with a turbine blade

US7963746B2 · kind B2 · utility

2Cited by
9References
10Claims
0Family size

Assignee

Inventors

Key dates

Filing dateSep 21, 2009
Grant dateJun 21, 2011
Priority date
Expiry dateSep 21, 2029

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF05D2240/80
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

The invention relates to a turbine blade comprising a vane that runs along a blade axis and a platform region, located at the root of the vane having a platform that extends transversally to the blade axis. The aim of the invention is to configure a delimitation of a flow channel of a gas turbine in the simplest possible manner. Therefore, the platform is configured by an elastic sheet metal part that rests on the vane. Said part leads to a gas turbine comprising a flow conduit that runs along an axis of the gas turbine, said conduit having an annular cross-section for a working medium and a second vane stage that is situated downstream of a first vane stage, which runs along the axis.

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