Patent · US Active

Flexible support structure for a geared architecture gas turbine engine

US9133729B1 · kind B1 · utility

35Cited by
23References
11Claims
0Family size

Assignee

Inventors

Key dates

Filing dateSep 20, 2012
Grant dateSep 15, 2015
Priority date—
Expiry dateMar 15, 2034

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/60
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A gas turbine engine includes a flex mount for a Fan Drive Gear System defined by a lateral and transverse stiffness relatonship.

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