- Schenectady NY, US Jacob Romeo Rendon - Cedar Park TX, US Duane Allan Busch - Loveland OH, US Ryan Christopher Jones - Cincinnati OH, US Paul Christopher Schilling - Waynesville OH, US Zachary Daniel Webster - Mason OH, US Tingfan Pang - West Chester OH, US Gregory Terrence Garay - West Chester OH, US Steven Robert Brassfield - Cincinnati OH, US
International Classification:
F01D 5/08
Abstract:
An apparatus and method relating to a cooling hole of a component of a turbine engine. The cooling hole can extend from an inlet to an outlet to define a passage. The cooling hole can include a laid back section where a coating can be applied. The method can include forming the cooling hole in the component and applying the coating to the component to maintain a specific geometry.