Anordnungen für ein Flugzeugantriebssystem

Details

Veröffentlichungs-Nr.

EP4733553

Anmeldetag

24. Oktober 2025

Veröffentlichung

29. April 2026

Rechtsraum

EP

Abstract

An assembly for an aircraft propulsion system (20) includes a propulsor rotor (42) and a guide vane structure (88). The guide vane structure (88) includes a plurality of guide vanes (90). The guide vane structure (88) is disposed axially next to the propulsor rotor (42). The guide vanes (90) include a first guide vane. The first guide vane includes a camber line (98), a leading edge (100), a trailing edge (102), an inner end (94), an outer end (96), at least one leading edge section (106) and a trailing edge section (108). The first guide vane extends longitudinally along the camber line (98) from the leading edge (100) to the trailing edge (102). The leading edge section (106) forms a respective portion of the leading edge (100) and is arranged radially along the trailing edge section (108) between the inner end (94) and the outer end (96). The trailing edge section (108) forms the trailing edge (102). The leading edge section (106) is configured to translate longitudinally along the camber line (98).

Anmelder

Firma

RTX Corporation

Land

🇺🇸 USA