Invention Grant
- Patent Title: Coating occlusion resistant effusion cooling holes for gas turbine engine
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Application No.: US17317589Application Date: 2021-05-11
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Publication No.: US11674686B2Publication Date: 2023-06-13
- Inventor: Nagaraja Rudrapatna , Rodolphe Dudebout
- Applicant: HONEYWELL INTERNATIONAL INC.
- Applicant Address: US NC Charlotte
- Assignee: HONEYWELL INTERNATIONAL INC.
- Current Assignee: HONEYWELL INTERNATIONAL INC.
- Current Assignee Address: US NC Charlotte
- Agency: Lorenz & Kopf LLP
- Main IPC: F23R3/00
- IPC: F23R3/00 ; F02C7/18

Abstract:
A coating occlusion resistant effusion cooling hole to form a film of a cooling fluid on a surface of a wall. The cooling hole extends along a longitudinal axis. The cooling hole includes an inlet section defined so as to be spaced apart from the surface. The inlet section is to receive the cooling fluid. The cooling hole includes a metering section fluidly coupled downstream of the inlet section. The cooling hole includes an outlet section fluidly coupled downstream of the metering section. The outlet section includes an overhang portion, a recessed portion, a first sidewall and a second sidewall. The first sidewall and the second sidewall interconnect the overhang portion with the recessed portion along a portion of the outlet section, and the first sidewall and the second sidewall converge and diverge in a plane transverse to the longitudinal axis.
Public/Granted literature
- US20220364727A1 COATING OCCLUSION RESISTANT EFFUSION COOLING HOLES FOR GAS TURBINE ENGINE Public/Granted day:2022-11-17
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