公开(公告)号：US11692486B2

公开(公告)日：2023-07-04

申请号：US17843833

申请日：2022-06-17

Applicant: Raytheon Technologies Corporation

Inventor： Stephen K. Kramer ,  Brian Knisely ,  Eric DeShong ,  Shawn Siroka ,  Ivan Monge-Concepcion

IPC: F02C7/16 ,  B22F12/00 ,  F02C3/14 ,  F23R3/00 ,  F23R3/06 ,  B33Y50/00 ,  B22F5/00

CPC classification number: F02C7/16 ,  B22F12/00 ,  F02C3/14 ,  F23R3/002 ,  F23R3/06 ,  B22F2005/005 ,  B33Y50/00 ,  F05D2230/21 ,  F05D2240/35 ,  F23R2900/00018 ,  F23R2900/03044

Abstract: Methods for manufacturing combustor panels of gas turbine engines and combustor panels are described. The methods include defining a particle deposit near-steady state for at least a portion of a combustor panel, the particle deposit near-steady state representative of a build-up of particles on the at least a portion of the combustor panel during use, generating a template based on the defined particle deposit near-steady state, wherein the template includes one or more augmentation elements based on the representative of build-up of particles, and forming a combustor panel based on the template, wherein the formed combustor panel includes one or more augmentation elements defined in the template.