Keyed brake disk assembly
US-2015129369-A1 · May 14, 2015 · US
US9315261B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9315261-B2 |
| Application number | US-201313927963-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jun 26, 2013 |
| Priority date | Jun 26, 2013 |
| Publication date | Apr 19, 2016 |
| Grant date | Apr 19, 2016 |
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Official abstract text for this publication.
Friction disks, such as rotors and stators, including keyed wear liners are disclosed. The friction disks may include a core and a replaceable wear liner coupled to each side of the core. The wear liners may include a plurality of keys which engage key notches in the core. The key notches may prevent the wear liners from rotating with respect to the core in response to a shear force, such as a force applied during braking.
Opening claim text (preview).
What is claimed is: 1. A stator comprising: a core comprising: a spine; an inner core having a thickness greater than the spine; a lug in the inner core; and a key notch recessed into a radially outer portion of the inner core, wherein the core is a single integral component comprising the spine, the inner core, and the lug; and a first wear liner coupled to the spine, the first wear liner comprising an annular ring and a stator key, wherein the stator key mates with the key notch in the inner core. 2. The stator of claim 1 , further comprising a second wear liner coupled to the spine opposite the first wear liner. 3. The stator of claim 2 , wherein a combined thickness of the first wear liner, the spine, and the second wear liner is greater than the thickness of the inner core. 4. The stator of claim 1 , wherein the first wear liner comprises a coned disc shape. 5. The stator of claim 1 , wherein the first wear liner is at least one of bonded to the core and riveted to the core. 6. The stator of claim 1 , wherein the core comprises a first material, the first wear liner comprises a second material, and wherein the first material is different than the second material. 7. The stator of claim 1 , wherein the stator key engages a core key in the inner core to prevent rotation of the first wear liner. 8. The stator of claim 1 , wherein the first wear liner comprises a first remanufactured wear liner bonded to a second remanufactured wear liner. 9. A friction disk comprising: a core comprising a spine and a plurality of lugs, the plurality of lugs having a plurality of notches recessed in a radially outer portion of the plurality of lugs, the plurality of lugs having a thickness greater than a thickness of the spine, wherein the core is a single integral component comprising the spine and the plurality of lugs; and a wear liner comprising a wear surface, a mating surface, and a plurality of keys located adjacent to at least one of an inner surface and an outer surface of the wear liner, wherein the plurality of keys are located within the plurality of notches. 10. The friction disk of claim 9 , wherein the wear liner is coupled to the core by at least one of a bond and a rivet. 11. The friction disk of claim 9 , wherein the wear liner comprises a substantially uniform thickness. 12. The friction disk of claim 9 , wherein the friction disk comprises at least one of a rotor and a stator in an aircraft brake.
characterised by properties of the disc surface; Discs lined with friction material · CPC title
outer circumference · CPC title
Braking members; Mounting thereof (friction linings or attachment thereof F16D69/00) · CPC title
interlocking · CPC title
comprising an annular disc secured to a hub member; Discs characterised by means for mounting · CPC title
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