Patent · US Active

Close coupled gearbox assembly for a tip turbine engine

US7959406B2 · kind B2 · utility

8Cited by
110References
3Claims
0Family size

Assignee

Inventors

Key dates

Filing dateDec 1, 2004
Grant dateJun 14, 2011
Priority date
Expiry dateNov 13, 2027

Classification

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

Abstract

A gearbox assembly (90) closely couples a fan-turbine rotor assembly (25) and an axial compressor rotor (46) to reduce the overall engine length and minimizes the number of engine bearings.

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