Siebanordnung für ein Ölsystem eines Flugzeugmotors

Details

Veröffentlichungs-Nr.

EP4717967

Anmeldetag

25. September 2025

Veröffentlichung

1. April 2026

Rechtsraum

EP

Abstract

An engine oil system (34) includes a conduit (72) and a strainer assembly (74). The conduit (72) forms a portion of an oil flow path (64). The conduit (72) includes a first conduit body (500) and a second conduit body (502). The first conduit body (500) is mounted to the second conduit body (502) at a flange interface (512). The first conduit body (500) and the second conduit body (502) form an internal passage (516) of the conduit (72). The strainer assembly (74) is disposed within the conduit (72) at the flange interface (512). The strainer assembly (74) includes a tubular body (518), a first packing ring (520), a second packing ring (522), and a strainer member (524). The first packing ring (520) forms a first fluid seal between the tubular body (518) and the first conduit body (500). The second packing ring (522) forms a second fluid seal between the tubular body (518) and the second conduit body (502). The strainer member (524) is mounted to the tubular body (518) within the oil flow path (64).

Anmelder

Firma

PRATT & WHITNEY CANADA CORP.

Land

🇨🇦 Kanada