Patent · US Active

Gas turbine engine with low stage count low pressure turbine

US8511605B2 · kind B2 · utility

7Cited by
44References
16Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMay 31, 2012
Grant dateAug 20, 2013
Priority date
Expiry dateJul 7, 2032

Classification

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

Abstract

A gas turbine engine includes a spool along an engine centerline axis which drives a gear train, said spool includes a low stage count low pressure turbine.

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