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Airfoil Cooling Circuit And Corresponding Airfoil
Abstract: An airfoil cooling circuit for a gas turbine engine having at least one internal cavity with a lobed cross sectional shape.
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Notices, Deadlines & Correspondence
Notices, Deadlines & Correspondence
Patent Information
Application #
Filing Date
13 November 2014
Publication Number
36/2016
Publication Type
INA
Invention Field
MECHANICAL ENGINEERING
Status
Email
Parent Application
Applicants
GENERAL ELECTRIC COMPANY
1 River Road
Schenectady NY 12345
Inventors
1. BERGHOLZ Robert Frederick
6380 Aviation Way
MD: W206
West Chester OH 45069