Aktuatorsysteme mit Gemeinsamer Redundanz

EP4215762 Art A1 26. Juli 2023

Anmelder: Hamilton Sundstrand Corporation 🇺🇸

Details

Veröffentlichungs-Nr.
EP4215762
Aktenzeichen
EP23152952
Anmeldetag
23. Januar 2023
Veröffentlichung
26. Juli 2023
Rechtsraum
EP
IPC
F15B20/00F15B11/16
Offizieller Volltext

Abstract

An actuator system can include a first actuator (101a), a second actuator (101b), a first actuator control device (103a) configured to control the first actuator, a second actuator control device (103b) configured to control the second actuator, a shared redundant actuator control device (103c), and at least one transfer device (105) operatively connected to the first, second, and shared redundant actuator control devices. The at least one transfer device can be configured to be operated to select between a first control mode where the first actuator control device is operatively connected to the first actuator to control the first actuator and the second actuator control device is operatively connected to the second actuator to control the second actuator, a second control mode where the shared redundant actuator control device is operatively connected to the first actuator to control the first actuator and the second actuator control device is operatively connected to the second actuator to control the second actuator, and a third control mode where the first actuator control device is operatively connected to the first actuator to control the first actuator and the shared redundant actuator control device is operatively connected to the second actuator to control the second actuator.

Anmelder

Firma
Hamilton Sundstrand Corporation
Land
🇺🇸 USA
🇺🇸 Hamilton Sundstrand

US-amerikanisches Unternehmen der Luft- und Raumfahrtindustrie, das Flugzeugsysteme wie Umweltkontroll-, Energie- und Antriebssysteme entwickelt; heute Teil von Collins Aerospace innerhalb von RTX.

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