Patent · US Active

Gas turbine rotor with purge blades

US8864471B2 · kind B2 · utility

0Cited by
15References
15Claims
0Family size

Assignee

Inventors

Key dates

Filing dateAug 12, 2011
Grant dateOct 21, 2014
Priority date
Expiry dateMar 13, 2033

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF05D2260/601
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A rotor for a gas turbine engine includes a plurality of turbine blades extending radially outwardly of a rotor body. A plurality of purge blades are positioned to rotate with the rotor body, and to drive air radially outwardly toward the turbine blades.

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