Keyed brake disk assembly
Friction disks, such as rotors and stators, including floating cores are disclosed. The friction disks may include a carrier plate and a wear liner coupled to each side of the core. The floating core may be located between the wear liners. The floating core may include a key which is located within a key notch in the carrier plate. The key may prevent the floating core from rotating relative to the carrier plate.
1. A friction disk comprising:
a carrier plate;
a first wear liner coupled to the carrier plate;
a second wear liner coupled to the carrier plate; and
a floating core located between the first wear liner and the second wear liner, wherein the floating core comprises a floating core key located within a key notch in the carrier plate.
2. The friction disk of claim 1 , wherein the floating core key is configured to prevent rotational movement of the floating core relative to the carrier plate.
3. The friction disk of claim 1 , wherein the floating core comprises a carbon composite.
4. The friction disk of claim 1 , wherein the carrier plate comprises at least one of silicon carbide, a silicon carbide composite, and titanium.
5. The friction disk of claim 1 , wherein the friction disk comprises at least one of a rotor and a stator for an aircraft braking system.
6. An aircraft brake system comprising:
a rotor comprising a rotor carrier plate, a first rotor wear liner, a second rotor wear liner, and a floating rotor core located between the first rotor wear liner and the second rotor wear liner, wherein the floating rotor core is located radially inward of the rotor carrier plate; and
a stator comprising a stator carrier plate, a first stator wear liner, a second stator wear liner, and a floating stator core located between the first stator wear liner and the second stator wear liner.
7. The aircraft brake system of claim 6 , wherein the floating stator core is located radially outward of the stator carrier plate.
8. The aircraft brake system of claim 6 , wherein the floating rotor core comprises a floating rotor core key, and wherein the floating stator core comprises a floating stator core key.
9. The aircraft brake system of claim 6 , wherein at least one of the floating rotor core and the floating stator core are configured to damp vibrations in the aircraft brake system.
10. The aircraft brake system of claim 6 , wherein the floating rotor core is free to move in an axial direction between the first rotor wear liner and the second rotor wear liner.
11. The aircraft brake system of claim 6 , wherein an inner surface of the floating rotor core is flush with an inner surface of the first rotor wear liner and an inner surface of the second rotor wear liner.
12. A friction disk comprising:
a carrier plate;
a first wear liner coupled to the carrier plate;
a second wear liner coupled to the carrier plate; and
a floating core located between the first wear liner and the second wear liner, wherein the floating core comprises a floating core key, wherein the floating core key is configured to prevent rotational movement of the floating core relative to the carrier plate.
13. The friction disk of claim 12 , wherein the carrier plate comprises a key notch.
14. An aircraft brake system comprising:
a rotor comprising a rotor carrier plate, a first rotor wear liner, a second rotor wear liner, and a floating rotor core located between the first rotor wear liner and the second rotor wear liner; and
a stator comprising a stator carrier plate, a first stator wear liner, a second stator wear liner, and a floating stator core located between the first stator wear liner and the second stator wear liner, wherein the floating stator core is located radially outward of the stator carrier plate.
15. The aircraft brake system of claim 14 , wherein the floating rotor core is located radially inward of the rotor carrier plate.