Anordnung für Gasturbinenmotor

Details

Veröffentlichungs-Nr.

EP4793171

Anmeldetag

11. Februar 2026

Veröffentlichung

19. August 2026

Rechtsraum

EP

Abstract

An assembly (200) for a gas turbine engine (100), the gas turbine engine (100) defining an axial direction and a radial direction, the assembly (200) including a hub shaft (202) configured to support a fan blade (154) of the gas turbine, a propellor shaft (204) configured to connect to a gearbox (155), the propellor shaft (204) disposed aft of the hub shaft (202) in the axial direction, a connector (206) fixing the hub shaft (202) to the propellor shaft (204), and a bearing (208) disposed on the hub shaft (202) forward of the connector (206) in the axial direction.

Anmelder

Firmen

General Electric Company
GE Aerospace Poland Sp. z o.o.

Land

🇺🇸 USA