Rotorzusammenbauten für ein Gasturbinentriebwerk

Details

Veröffentlichungs-Nr.

EP3851637

Aktenzeichen

EP21152141

Anmeldetag

18. Januar 2021

Veröffentlichung

14. Juni 2023

Erteilung

14. Juni 2023

Rechtsraum

EP

IPC

F01D5/30F01D5/14// F01D5/28C04B35/80

Abstract

A rotor assembly is provided for a gas turbine engine. This rotor assembly includes a first rotor disk (110A), a second rotor disk (110B), a plurality of rotor blades (34) and a plurality of disk mounts (118). The first rotor disk is configured to rotate about a rotational axis (32). 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 mounted to the first rotor disk and to the second rotor disk. The rotor blades include a first rotor blade (34A). Each of the disk mounts connects the first rotor disk and the second rotor disk together. The disk mounts include a first disk mount (118A) that further supports the first rotor blade.

Anmelder

Firmen

RTX Corporation
Raytheon Technologies Corporation

Land

🇺🇸 USA

Fachgebiete