Invention Grant
- Patent Title: Impingement insert for a gas turbine engine
-
Application No.: US17118792Application Date: 2020-12-11
-
Publication No.: US11519281B2Publication Date: 2022-12-06
- Inventor: Sandip Dutta , Benjamin Paul Lacy , Gary Michael Itzel , Zachary John Snider
- Applicant: General Electric Company
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: Dority & Manning, P.A.
- Main IPC: F01D9/06
- IPC: F01D9/06 ; F01D5/18 ; F01D11/08 ; F01D25/14

Abstract:
The present disclosure is directed to a turbomachine that includes a hot gas path component having an inner surface and defining a hot gas path component cavity. An impingement insert is positioned within the hot gas path component cavity. The impingement insert includes an inner surface and an outer surface and defines an impingement insert cavity and a plurality of impingement apertures fluidly coupling the impingement insert cavity and the hot gas path component cavity. A plurality of pins extends from the outer surface of the impingement insert to the inner surface of the hot gas path component.
Public/Granted literature
- US20210270141A1 IMPINGEMENT INSERT FOR A GAS TURBINE ENGINE Public/Granted day:2021-09-02
Information query