Patent · US Active

Cooling hole with crenellation features

US8707713B2 · kind B2 · utility

9Cited by
49References
22Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJul 9, 2012
Grant dateApr 29, 2014
Priority date
Expiry dateJul 9, 2032

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T29/49323
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A gas turbine engine component includes a wall having first and second wall surfaces and a cooling hole extending through the wall. The cooling hole includes an inlet located at the first wall surface, an outlet located at the second wall surface and a diffusing section in communication with the inlet and extending to the outlet. The diffusing section includes a plurality of crenellation features that encourage lateral spreading of cooling air flowing through the cooling hole.

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