Flugzeugantriebssystem mit Innenraumbelüftung

Details

Veröffentlichungs-Nr.

EP4775814

Anmeldetag

12. Januar 2026

Veröffentlichung

15. Juli 2026

Rechtsraum

EP

Abstract

An assembly (20) is provided for an aircraft. This assembly (20) includes an engine core (50), an engine case (68), a nacelle wall (166) and an air circuit. The engine core (50) includes a compressor section (45), a combustor section (46) and a turbine section (47). The engine case (68) houses the engine core (50). The nacelle wall (166) is radially outboard of and covers the engine case (68). A compartment (140) is formed by and extends radially between the engine case (68) and the nacelle wall (166). The air circuit includes a manifold disposed within the compartment (140). The air circuit is configured to direct air from an air source into the manifold. The manifold includes a plurality of outlets. The manifold is configured to direct the air into the compartment (140) through the outlets.

Anmelder

Firma

RTX Corporation

Land

🇺🇸 USA