Bypassventil

Details

Veröffentlichungs-Nr.

EP4397842

Aktenzeichen

EP24150788

Anmeldetag

8. Januar 2024

Veröffentlichung

31. Juli 2024

Rechtsraum

EP

IPC

F01D25/20F01M1/02F04D29/063

Abstract

A fluid system (200) for an aircraft engine (256) can include a pumped fluid circulation circuit (262) including a fluid tank, the fluid circulation circuit (262) configured to circulate a fluid through at least a part of the aircraft engine (256) and means, in the fluid circulation circuit (262), for selectively directing the fluid of the fluid circulation circuit (262) as a function of a pressure of fluid in the fluid circulation circuit (262) to one of a part of the aircraft engine (256), and a fluid bypass (264) in the fluid circulation circuit (262) that is fluidly upstream of the part.

Anmelder

Firma

PRATT & WHITNEY CANADA CORP.

Land

🇨🇦 Kanada

Fachgebiete