Brennkammerauskleidungsplatte mit einer Vielzahl von Wärmeübertragungsrippen für eine Gasturbinenbrennkammer

Details

Veröffentlichungs-Nr.

EP3438537

Aktenzeichen

EP18186910

Anmeldetag

1. August 2018

Veröffentlichung

18. November 2020

Erteilung

18. November 2020

Rechtsraum

EP

IPC

F23R3/00F23R3/60F23R3/06

Abstract

A liner panel (72,74) for use in a combustor (56) of a gas turbine engine (20), including a multiple of heat transfer ribs (150) located in at least one discrete area of the liner panel (72,74). A wall assembly (60,62) within a gas turbine engine (20) including a support shell (68,70), a liner panel (72,74) mounted to the support shell (68,70) via a multiple of studs (100) and a multiple of heat transfer ribs (150) located in at least one discrete area on a cold side (110) of the liner panel (72,74), each of the multiple of heat transfer ribs (150) account for the multiple of studs (100).

Anmelder

Firmen

Raytheon Technologies Corporation
United Technologies Corporation

Land

🇺🇸 USA

Fachgebiete