Flugzeugluftsystem mit Verstärkungsverdichter(n)

Details

Veröffentlichungs-Nr.

EP4790251

Anmeldetag

9. Februar 2026

Veröffentlichung

12. August 2026

Rechtsraum

EP

IPC

F02C7/14, F02C7/18, F02C7/32

Abstract

A system is provided for an aircraft. This aircraft system includes a turbine engine and an air system. The turbine engine includes a flowpath, a compressor section, a combustor section and a turbine section. The flowpath extends through the compressor section, the combustor section and the turbine section from an airflow inlet into the flowpath to a combustion products exhaust from the flowpath. The air system includes an air circuit, a first boost compressor, a second boost compressor and a heat exchanger. A circuit inlet into the air circuit is fluidly coupled to the flowpath upstream of the combustor section. The air circuit projects out from the circuit inlet and extends through the first boost compressor, the second boost compressor and the heat exchanger.

Anmelder

Firma

RTX Corporation

Land

🇺🇸 USA

Fachgebiete