Patent · US Active

Stator casing cooling system

US9790810B2 · kind B2 · utility

2Cited by
4References
21Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJun 14, 2013
Grant dateOct 17, 2017
Priority date
Expiry dateOct 12, 2034

Classification

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

Abstract

In a gas turbine for aeronautic engines, a stator body delimited by an outer lateral surface is cooled by an air cooling device having a plurality of circumferential tubes for distributing air on the outer lateral surface; each circumferential tube having a plurality of outlets for guiding respective cooling airflows towards the outer lateral surface and into a respective circumferential channel obtained between two groups of circumferential channels adjacent to each other and lapped by the flow of air leaving the circumferential channel.

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