Rotorzusammenbauten für ein Gasturbinentriebwerk

Details

Veröffentlichungs-Nr.

EP3851638

Aktenzeichen

EP21152157

Anmeldetag

18. Januar 2021

Veröffentlichung

28. Juli 2021

Rechtsraum

EP

IPC

F01D5/30F01D5/08// F01D5/28C04B35/80

Abstract

A rotor assembly is provided for a gas turbine engine. This rotor assembly includes a first rotor disk (180A), a second rotor disk (180B), a plurality of rotor blades (104) and a plurality of vanes (234). The first rotor disk is configured to rotate about a rotational axis (102). The second rotor disk is configured to rotate about the rotational axis. The rotor blades are arranged circumferentially around the rotational axis. Each of the rotor blades is axially between and mounted to the first rotor disk and the second rotor disk. The vanes are arranged circumferentially around the rotational axis. The vanes include a first vane (234) that is integral with the first rotor disk and projects axially to the second rotor disk.

Anmelder

Firmen

RTX Corporation
Raytheon Technologies Corporation

Land

🇺🇸 USA

Fachgebiete