Friction disks with floating wear linings

Patent metadata

Field	Value
Publication number	US-9587691-B2
Application number	US-201514606511-A
Country	US
Kind code	B2
Filing date	Jan 27, 2015
Priority date	Jan 27, 2015
Publication date	Mar 7, 2017
Grant date	Mar 7, 2017

Abstract

Friction disks, such as rotors and stators, including floating wear liners are disclosed. The friction disks may include a core and a floating wear liner configured to contact a contact surface of the core. The cores may include a retention ring that is substantially concentric with the core and extends axially beyond the plane of the contact surface. The retention ring may radially constrain the floating wear liner in a position aligned with the contact surface to provide frictional contact with the core during braking.

First claim

What is claimed is:

1. A friction disk comprising:
a friction disk core comprising:
a spine comprising a first contact surface of the spine that defines a first contact surface plane; and
a first retention ring comprising an annular feature, the first retention ring disposed substantially concentrically with the friction disk core and extending axially relative to the first contact surface plane, wherein the first retention ring has a first retention ring wall that is substantially parallel with a friction disk core axis; and

a first floating wear liner rotatable about the friction disk core axis with respect to the friction disk core, the first floating wear liner comprising:
a first wear surface configured to contact the first contact surface;
a second wear surface opposite the first wear surface;
an interior axial wall defining an interior diameter;
and an exterior axial wall defining an outside diameter;

wherein the interior axial wall and the exterior axial wall extend between the first wear surface and the second wear surface, and wherein the interior axial wall is radially spaced a distance apart from and has a configuration complementary to the first retention ring wall.

2. The friction disk of claim 1 , wherein the first retention ring has a substantially rectangular cross section.

3. The friction disk of claim 1 , wherein the friction disk core comprises a first material, the first floating wear liner comprises a second material, and wherein the first material is different than the second material.

4. The friction disk of claim 1 , wherein the friction disk is a stator, wherein the first retention ring is a stator retention ring, wherein the first retention ring wall is an outer wall of the stator retention ring, and wherein the interior axial wall of the first floating wear liner is configured to receive the outer wall of the stator retention ring.

5. The friction disk of claim 1 , wherein the friction disk is a rotor, wherein the first retention ring is a rotor retention ring, wherein the first retention ring wall is an inner wall of the rotor retention ring, and wherein the inner wall of the rotor retention ring is configured to receive the exterior axial wall of the first floating wear liner.

6. The friction disk of claim 1 , further comprising:
a second floating wear liner, and
wherein the friction disk core further comprises:
a second contact surface of the spine that defines a second contact surface plane; and
a second retention ring comprising an annular feature, the second retention ring disposed substantially concentrically with the friction disk core and extending axially relative the second contact surface plane, wherein the second retention ring has a second retention ring wall that is substantially parallel with the friction disk core axis.

7. The friction disk of claim 6 , wherein the first retention ring and the second retention ring have a substantially similar configuration, and wherein the first wear liner and the second wear liner are interchangeable.

8. The friction disk of claim 1 , wherein the distance is between about 0.005 inches and about 0.01 inches.

9. A multi-disk brake system comprising:
a plurality of adjacent stator-rotor pairs, each one of the adjacent stator-rotor pairs comprising a stator core and a rotor core; and
a floating wear liner disposed between the rotor core and the stator core in at least one of the plurality of adjacent stator-rotor pairs, wherein the floating wear liner is rotatable about a core axis of the stator core and the rotor core;
wherein at least one of the stator cores and the rotor cores comprises a retention ring; and
wherein the floating wear liner is radially spaced a distance apart from the retention ring and is radially constrained within the multi-disk brake system by the retention ring.

10. The multi-disk brake system of claim 9 , wherein the system comprises a plurality of wear liners disposed between one of the plurality of adjacent stator-rotor pairs, and wherein one of the plurality of wear liners is the floating wear liner.

11. The multi-disk brake system of claim 10 , wherein the floating wear liner can move axially and rotationally with respect to the at least one of the stator cores and the rotor cores comprising the retention ring.

12. The multi-disk brake system of claim 11 , wherein the floating wear liner distributes friction between two wear surfaces of the floating wear liner in response to aircraft braking.

13. The multi-disk brake system of claim 11 , wherein the floating wear liner produces a reduced relative rotational velocity at each of two wear surfaces of the floating wear liner in response to aircraft braking relative to a rotational velocity of a fixed rotating component.

14. The multi-disk brake system of claim 10 , wherein the plurality of wear liners includes a plurality of the floating wear liners.

15. The multi-disk brake system of claim 14 , wherein the system comprises a plurality of stators and a plurality of rotors, each of the plurality of stators comprising one of the plurality of the floating wear liners, and each of the plurality of rotors comprising one of the plurality of wear liners fixed to the rotor.

16. The multi-disk brake system of claim 9 , wherein the distance is between about 0.005 inches and about 0.01 inches.

Assignees

• Goodrich Corp

Inventors

• Kirkpatrick Christopher T

Classifications

• F16D65/126

  the material being of low mechanical strength, e.g. carbon, beryllium; Torque transmitting members therefor · CPC title

• F16D69/0408

  specially adapted for plane linings · CPC title

• F16D2055/0095

  Plural rotors with different properties, e.g. to influence working conditions like wear or temperature · CPC title

• F16D65/127 Primary

  characterised by properties of the disc surface; Discs lined with friction material · CPC title

• F16D2200/0052

  Carbon · CPC title