Luftkreislauf für Flugzeugantriebssystem

Details

Veröffentlichungs-Nr.

EP4814281

Anmeldetag

25. März 2026

Veröffentlichung

30. September 2026

Rechtsraum

EP

IPC

F02C6/08, F02C9/18

Abstract

An assembly includes a compressor section (33), a core flowpath (40), a bypass flowpath (42), a flowpath wall and an air circuit (124). The flowpath wall forms an inner peripheral boundary of the bypass flowpath (42). The flowpath wall includes a wall base (92) and a wall protrusion (94). The wall base (92) extends axially along and circumferentially about the axis. The wall protrusion (94) projects radially out from the wall base (92). The wall protrusion (94) extends axially along the axis from a protrusion first end to a protrusion second end. The protrusion first end is upstream of the protrusion second end along the bypass flowpath (42). The air circuit (124) extends from a circuit inlet (126) to a circuit outlet (128). The circuit inlet (126) is fluidly coupled to the core flowpath (40). The circuit outlet (128) is fluidly coupled to the bypass flowpath (42). The circuit outlet (128) is formed in the wall protrusion (94) axially between the protrusion first end and the protrusion second end.

Anmelder

Firma

RTX Corporation

Land

🇺🇸 USA

Fachgebiete