Betätigungssystem für einen Schubumkehrer eines Flugzeugantriebssystems

Details

Veröffentlichungs-Nr.

EP3951155

Aktenzeichen

EP21172259

Anmeldetag

5. Mai 2021

Veröffentlichung

16. Juli 2025

Erteilung

16. Juli 2025

Rechtsraum

EP

IPC

F02K1/72F02K1/76

Abstract

An assembly (66) is provided for an aircraft propulsion system (20). This assembly (66) includes a first actuator (68), a second actuator (68) and a linkage system (70, 72). The linkage system (70, 72) is configured to transfer torque between the first actuator (68) and the second actuator (68). The linkage system (70, 72) includes a first linkage shaft (90), a second linkage shaft (90) and a gearbox (92). The first linkage shaft (90) has a first centerline (94). The second linkage shaft (90) has a second centerline (94) offset from the first centerline (94). The gearbox (92) is coupled to and is between the first linkage shaft (90) and the second linkage shaft (90).

Anmelder

Firma

Rohr, Inc.

Land

🇺🇸 USA

Fachgebiete