Patent · US Active

Rotor blade for an axial flow turbomachine and mounting for such a rotor blade

US8951016B2 · kind B2 · utility

1Cited by
8References
10Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJun 17, 2010
Grant dateFeb 10, 2015
Priority date
Expiry dateSep 18, 2031

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF01D5/3007
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A rotor blade for an axial flow turbomachine, preferably a turbine, and to a mounting for such a rotor blade is provided. In the rotor blade, the two opposing lateral walls of the blade base are continuously curved along their extension between platform and bottom side of the blade base in order to reduce the mechanical load in the blade base and that of the walls supporting the blade base of a rotor.

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