Patent · US Active

Cooled airfoil structure

US10494929B2 · kind B2 · utility

0Cited by
17References
17Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJul 21, 2015
Grant dateDec 3, 2019
Priority date
Expiry dateMay 26, 2037

Classification

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

Abstract

An airfoil structure for a gas turbine engine includes an airfoil that includes a suction side cooling circuit with at least two segments that are connected by at least one impingement passage.

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