Flugzeugluftsystem mit Elektrischem Verdichter

Details

Veröffentlichungs-Nr.

EP4790249

Anmeldetag

6. Februar 2026

Veröffentlichung

12. August 2026

Rechtsraum

EP

Abstract

An aircraft system includes a turbine engine (24) and an air system (36). The turbine engine (24) includes a compressor section (45), a combustor section (46) and a turbine section (47). A flowpath extends through the compressor section (45), the combustor section (46) and the turbine section (47). A first rotating structure includes a first compressor rotor disposed in the compressor section (45). A second rotating structure includes a second compressor rotor disposed in the compressor section (45) along the flowpath between the first compressor rotor and the combustor section (46). The air system (36) includes an air circuit (136) and an electric boost compressor (138). A circuit inlet (146) into the air circuit (136) is fluidly coupled to the flowpath and disposed along the second compressor rotor. The air circuit (136) projects out from the circuit inlet (146) and extends through the electric boost compressor (138).

Anmelder

Firma

RTX Corporation

Land

🇺🇸 USA