Bremssystem für ein Flugzeugrad

Details

Veröffentlichungs-Nr.

EP3753793

Aktenzeichen

EP19461545

Anmeldetag

21. Juni 2019

Veröffentlichung

22. Februar 2023

Erteilung

22. Februar 2023

Rechtsraum

EP

IPC

B60T5/00F16D65/48F16D65/12F16D65/78

Abstract

A braking system (4) for an aircraft wheel (2) comprises first and second brake rotor discs (20a, 20b) axially spaced along an axis (A) and rotationally coupled to the wheel (2), a stator disc (24) arranged axially between the first and second rotor discs (20a, 20b), and a heat shield (34) mounted to at least one of the first and second rotor discs (20a, 20b). Radially outer portions (30) of the first and second rotor discs (20a, 20b) extend radially outwardly of the stator disc (24) to define a gap (32) between the radially outer portions (30) of the first and second rotor discs (20a, 20b). The heat shield (34) extends at least partially over or into the gap (32).

Anmelder

Firma

Goodrich Corporation

Land

🇺🇸 USA

Fachgebiete