Patent · US Active

Engine bearing support

US8511987B2 · kind B2 · utility

24Cited by
10References
13Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJun 15, 2012
Grant dateAug 20, 2013
Priority date
Expiry dateJun 15, 2032

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T29/49236
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A turbofan engine comprises an engine case. A gaspath extends through the engine case. A fan has a circumferential array of fan blades. A fan case encircles the fan blades radially outboard of the engine case. A plurality of fan case vanes extend outward from the engine case to the fan case. A front frame assembly includes a plurality of vanes extending radially across the gaspath. A transmission couples a shaft to a fan shaft to drive the fan. A bearing assembly couples the shaft to the front frame assembly. A bearing support extends aftward and radially inward from the front frame assembly to the bearing assembly.

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