Patent · US Active

Turbomachine with alternatingly spaced turbine rotor blades

US10781717B2 · kind B2 · utility

0Cited by
30References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateSep 20, 2017
Grant dateSep 22, 2020
Priority date
Expiry dateAug 1, 2038

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF05D2260/40311
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A turbomachine includes a turbine frame and a turbine, the turbine including a first plurality of turbine rotor blades and a second plurality of turbine rotor blades alternatingly spaced along the axial direction and rotatable with one another. The turbomachine also includes a first support member assembly including a first support member supporting the first plurality of turbine rotor blades; a second support member assembly including a second support member supporting the second plurality of turbine rotor blades; a frame support member assembly including a frame support member coupled to and extending from the turbine frame; and a bearing assembly including a first bearing and a second bearing. The first bearing is positioned between the first support member and the second support member, and the second bearing is positioned between the frame support member and one of the first support member or the second support member.

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