Patent · US Active

Inner bypass duct wall attachment

US9194296B2 · kind B2 · utility

3Cited by
18References
18Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJul 25, 2012
Grant dateNov 24, 2015
Priority date
Expiry dateSep 19, 2034

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T29/49245
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A bypass duct of a gas turbine engine has an inner bypass duct wall having a front end portion which is rigidly mounted to an engine core case and a rear end portion which is flexibly mounted to the core case. The flexible mounting between the rear portion of the inner bypass duct wall and the core case allows hot engine areas of the core case to thermally grow and contract relative to the inner bypass duct wall without imposing additional loads on the inner bypass duct wall.

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