Patent · US Active

Engine component

US10132166B2 · kind B2 · utility

1Cited by
12References
10Claims
0Family size

Assignee

Inventors

Key dates

Filing dateFeb 27, 2015
Grant dateNov 20, 2018
Priority date
Expiry dateJun 24, 2036

Classification

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

Abstract

An engine component for a gas turbine engine includes a film-cooled substrate having a hot surface facing hot combustion gas flow and a cooling surface facing a cooling fluid flow. A film hole extends through the substrate to an outlet on the hot surface. A flow conditioning structure is provided upstream of the outlet.

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