An aircraft brake system may include an axle (210) and a brake axle sleeve (216). The brake axle sleeve may have a plurality of recesses (217) asymmetrically disposed about an inner circumference of the brake axle sleeve. The plurality of recesses may attenuate vibrations in the aircraft brake system.
BRAKE AXLE SLEEVE
BREMSACHSENHÜLSE
MANCHON D'ESSIEU DE FREIN
2021-07-07
Patent
Elektronische Ressource
Englisch