Anordnungen für ein Turbinentriebwerk

Details

Veröffentlichungs-Nr.

EP4752333

Anmeldetag

2. Oktober 2025

Veröffentlichung

3. Juni 2026

Rechtsraum

EP

IPC

F01D9/06, F01D5/18

Abstract

A turbine engine (24) assembly includes an airfoil (102), a first baffle (104) and a second baffle (106). The first baffle (104) is disposed in a cavity (128) in the airfoil (102). The first baffle (104) extends spanwise from a first baffle base end (146) to a first baffle tip end (148) disposed at an airfoil tip end (110). The second baffle (106) is disposed in the cavity (128) longitudinally between and next to the first baffle (104) and an airfoil interior wall (121). The second baffle (106) extends spanwise from a second baffle base end (166) to a second baffle tip end (168) disposed at the airfoil tip end (110).

Anmelder

Firma

RTX Corporation

Land

🇺🇸 USA