Steuerungsanordnung für Flugzeugantriebssysteme

Details

Veröffentlichungs-Nr.

EP4810379

Anmeldetag

18. März 2026

Veröffentlichung

23. September 2026

Rechtsraum

EP

Abstract

An aircraft propulsion system assembly includes a propulsion system (20) and a control assembly (26). The propulsion system (20) includes a propulsor (28), an engine (22), and an electrical assembly (24). The engine (22) includes a rotational assembly (44) coupled to the propulsor (28). The electrical assembly (24) includes an electric motor (62) coupled to the propulsor (28). The control assembly (26) includes a propulsor sensor assembly (68), an electric motor sensor (83), channel A control units (70), and a channel B control unit (72). The channel A control units (70) includes an engine control unit (86) for the engine (22) and an electric motor control unit (88) for the electric motor (62). The channel B control unit (72) is connected in signal communication with the propulsor sensor assembly (68), the electric motor sensor (83), the engine control unit (86), and the electric motor control unit (88).

Anmelder

Firma

Pratt & Whitney Canada Corp.

Land

🇨🇦 Kanada