Patent · US Active

Component for a turbine engine with a cooling hole

US10822958B2 · kind B2 · utility

7Cited by

12References

18Claims

0Family size

Assignee

General Electric Company · US

Inventors

Anquan Wang · Mason, US
Ryan Christopher Jones · West Chester, US
Paul Christopher Schilling · Neckargemünd, DE
Craig Alan Gonyou · Blanchester, US

Key dates

Filing date	Jan 16, 2019
Grant date	Nov 3, 2020
Priority date	—
Expiry date	Feb 2, 2039

Classification

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

Abstract

An apparatus and method relating to a cooling hole of a component of a turbine engine. The component can include a wall separating the hot gas fluid flow from the cooling fluid flow and having a heated surface along which the hot gas fluid flow flows and a cooled surface facing the cooling fluid flow and at least one cooling hole comprising at least one inlet at the cooled surface, at least one outlet at the heated surface, with the outlet having a modified outlet shape.

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