A brake device for installation on an axle of wheels including a piston; a casing accommodating at least the piston; a container; a first cast iron disc and a second cast iron disc, joined to the container; a first brake lining; a first supporting disc on which the first brake lining is located; and a bearing fixed to the central cylindrical wall of the container around the axle. The container and the casing remain fixed without rotating about the axle and the first brake lining together with the first supporting disc are fixed to the axle. The piston is further configured to displace the container together with the two cast iron discs towards the first brake lining until the first cast iron disc makes contact with the first brake lining. The container includes an inner circuit configured to accommodate a coolant.

A clip for coupling a torque plate to an end plate of a disk brake system in accordance with various embodiments includes an inner portion having two parallel elongate members. The clip further includes an outer portion at least partially including a rounded portion that is located outward from the inner portion and has a raised end, wherein the inner portion is entirely in a same plane as the rounded portion of the outer portion, and wherein the raised end extends away from the rounded portion.

A brake wear sensor is disclosed. In various embodiments, the brake wear sensor includes a bias member configured for connection between a stationary portion of a brake mechanism and a heat sink; and a load cell configured to measure a load in the bias member representative of a length of the heat sink.

A heat shield assembly is disclosed. In various embodiments, the heat shield assembly defines a first circumferential side and a second circumferential side and an inboard end and an outboard end and includes a first layer defining a first surface of the heat shield assembly and having a first tab member disposed proximate the inboard end at the first circumferential side and a second tab member disposed proximate the outboard end at the first circumferential side; and a second layer defining a second surface of the heat shield assembly and having one or more first crimped portions extending along the first circumferential side and configured to engage the first tab member and the second tab member.

A magnetic brake for a motor uses the magnetic force on the surface of a flux concentrating rotor to pull a flexible brake spring or friction sheet into friction contact with the rotor. An electromagnetic stator pulls the flexible brake spring or friction sheet away from the rotor when it is energized. The brake spring may be a variable thickness around the circumference in a radial flux motor or radially in an axial flux motor and is thicker near where it is fixed to the housing. The brake spring may be split so it can clamp down on the rotor symmetrically. The OD of the brake spring may be closer to the surrounding stator near the fixed section of the brake spring so the air gap to the brake stator is smaller and the gap to the rotor and the ID of the brake spring is larger to allow the brake stator to pull on this area with greater force initially when it is energized to disengage the brake.

A multiple disc brake system comprises an annular disc stack that includes interleaved sets of rotor discs and stator discs; an axially extending torque tube; and an actuator that axially moves the rotor discs into engagement with an axially adjacent stator disc. Each of the stator discs includes a plurality of circumferential arranged stator lugs that secure the stator discs to the torque tube, where each of the plurality of circumferential stator lugs comprises tapered side walls that taper inwardly transverse to the axially extending torque tube.

An electromagnetically operable brake arrangement for decelerating a rotationally mounted shaft, includes a magnet, a coil, a spring element, an armature disk, a brake pad support, a damping plate and a friction disk, the damping plate being situated between the armature disk and the magnet; the damping plate having projections; each of the projections extending further in a radial direction than in a circumferential direction; in particular, the projections each jutting out axially; in particular, at least a subset of the projections being evenly spaced apart from each other in the circumferential direction.

The invention relates to a method for attenuating vibrations of an aircraft wheel/brake assembly arising during braking, the brake comprising rotor discs (2b) rotationally driven with the wheel by means of bars (5) secured to the wheel and engaging in notches (3b) of the rotor discs, and stator discs (2a) which are kept rotationally immobile by means of tenons (5) secured to a torque tube (1) of the brake and engaged in notches (3a) of the stator discs, the notches having flanks that are protected by brackets (7). The method involves selecting bracket/tenon pair and/or bracket/bar pairs with a coefficient of friction less than or equal to 0.6.

A piston assembly for a multi-disk system may comprise an adjustor sleeve and a piston configured to telescope relative to the adjustor sleeve. A puck may be located at an end of the piston. The piston assembly may include a multi-layer insulator. The multi-layer insulator may comprise a first insulator layer contacting the puck or the piston, and a second insulator layer contacting the first insulator layer. The first and second insulator layers may each comprise a solid disk.

A torque tube for a brake assembly may include a tube portion having a first centerline axis, a conical back-leg portion extending from the tube portion in a radially outward angled orientation relative to the first centerline axis, and a lip portion disposed at a radially outward end of the conical back-leg portion. The lip portion may have added structural material to improve the structural properties of the torque tube to prevent or mitigate damage that would otherwise be caused by friction-induced vibrations.