Gasturbinentriebwerk

Details

Veröffentlichungs-Nr.

EP4793170

Anmeldetag

3. Februar 2026

Veröffentlichung

19. August 2026

Rechtsraum

EP

IPC

B64C11/14

Abstract

A gas turbine engine (100, 200, 300, 400, 420, 440, 500) defining an axial direction and a radial direction includes a spinner (112, 404, 504) defining a spinner duct (410, 506) and a spinner inlet (408, 506) to the spinner duct (410, 506), a turbomachine (110, 402, 502) comprising a compressor section (114), a combustion section (116), and a turbine section (118) arranged in serial flow order, the turbomachine (110, 402, 502) defining a fan duct (172), a fan duct (172) inlet to the fan duct (172), a core duct (142), and a core inlet (124) to the core duct (142), and a primary fan (152) driven by the turbomachine (110, 402, 502), wherein the spinner inlet (408, 506) is upstream of the primary fan (152).

Anmelder

Firma

General Electric Company

Land

🇺🇸 USA

Fachgebiete