Patent · US Active

Fundamental gear system architecture

US10221770B2 · kind B2 · utility

53Cited by
161References
21Claims
0Family size

Assignee

Inventor

Key dates

Filing dateFeb 26, 2014
Grant dateMar 5, 2019
Priority date
Expiry dateFeb 26, 2034

Classification

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

Abstract

A fan drive gear system for a gas turbine engine includes a gear system that provides a speed reduction between a fan drive turbine and a fan and a mount flexibly supporting portions of the gear system. A lubrication system supporting the fan drive gear system provides lubricant to the gear system and removes thermal energy produced by the gear system. The lubrication system includes a capacity for removing thermal energy equal to less than about 2% of power input into the gear system.

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