Gasturbinenmotor und Verfahren zur Erzeugung von Klassen davon

Details

Veröffentlichungs-Nr.

EP4711597

Anmeldetag

11. September 2019

Veröffentlichung

18. März 2026

Rechtsraum

EP

IPC

F02C3/04, F02C3/107, F02C6/20F02C6/20(LEFEBVRE GUY et al.)

Abstract

An aircraft engine has a high pressure spool including a high pressure turbine drivingly connected to a high pressure compressor. A low pressure spool including a low pressure compressor is fluidly connected to the high pressure compressor. A low pressure turbine is drivingly connected to the low pressure compressor to drive the low pressure compressor. A load is drivingly connected to the low pressure turbine, the load consisting of one of a propeller and a helicopter rotor. A method of creating classes of an aircraft engine from an engine platform is disclosed.

Anmelder

Firma

Pratt & Whitney Canada Corp.

Land

🇨🇦 Kanada

Fachgebiete