Patent · US Active

Turbofan mounting system

US8313293B2 · kind B2 · utility

4Cited by
36References
17Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMay 15, 2009
Grant dateNov 20, 2012
Priority date
Expiry dateJan 22, 2031

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF02K3/06
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A gas turbine engine has a rear mounting assembly incorporating a mounting apparatus attached to a bypass duct wall with a link device for transferring core portion related inertia-induced loads, from an MTF of the core portion in a short circuit across an annular bypass air passage to the bypass duct wall.

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