Patent Application
20130240304
This invention relates to brake systems used to control the motion of vehicles under severe conditions such as high speed operation and braking.
During high speed braking, a hydraulic piston contacts a brake pad under a high load generating considerable frictional heat which is transmitted through the brake pad into the underlying piston. Under severe conditions, such as in competition driving and heavy vehicle or aircraft braking, the frequency and duration of brake application increases to the point where the heat input into the piston exceeds the ability of the brake assembly to dissipate the heat and prevent the heat from being transmitted through the piston to the hydraulic system. In this situation, the fluid temperature approaches a point where the fluid begins to boil, creating a compressible gas wherein brake pressure is lost and braking is compromised. In extreme cases, the brake pedal can reach its displacement limit, braking control is lost, and a dangerous situation develops.
Efforts to minimize overheating in braking systems are ongoing. Material or engineering improvements to minimize the transmission of heat from the friction surface to the hydraulic fluid system would be beneficial.
A multilayer brake assembly includes a caliper, multilayer brake pads and a hydraulic cylinder assembly. The multilayer brake pads consist of a fiber reinforced ceramic matrix composite thermal insulating material positioned between a layer of friction material and a backing layer. A piston in the cylinder assembly acts to push the brake pads against a rotor in a braking event.
Another embodiment is a multilayer brake pad assembly that includes a layer of fiber reinforced ceramic matrix composite thermal insulating material between a layer of friction material and a layer of backing material to reduce the transfer of heat from the friction layer to the backing material.
Another embodiment is a piston in a brake assembly formed of a fiber reinforced ceramic matrix composite thermal insulating material.
The invention addresses the problem of brake overheating by installing a thermal insulator in the thermal circuit between the friction material and the steel backing plate of a disc brake pad, thereby decreasing the chances of hydraulic fluid overheating and boiling during high performance braking. A schematic of a prior art disc brake system for a vehicle is shown in
During a braking event, a pedal, not shown, applies pressure to a master cylinder that increases pressure in cylinder 34. Piston 32 responds by pressing brake pads 26 against rotor 24. The braking pressure, as indicated by arrows 36, creates friction energy that slows the rotational velocity of rotor 24 attached to a wheel of the vehicle, and thereby slows or stops the vehicle.
Disc brake system 10 may be taken as a representative friction brake system employed on vehicles in general. Examples include cars, trucks, trains, and aircraft.
A major design factor in all friction braking systems is the management of the heat generated during the braking process. Friction materials are designed to withstand high temperatures while maintaining an acceptable coefficient of friction and fracture strength. Brake systems are designed to dissipate the heat generated at the braking interfaces by channeling air flow over the pads, by introducing internal cooling passages and external fins into the rotor design and by employing high temperature and high strength materials in the rotors and brake pads. As an example, most rotors on high performance cars are cross-drilled to improve cooling air flow.
Friction material development in the art has focused on materials possessing high strength and friction coefficients at elevated temperatures. Friction materials may be polymer, metal, or ceramic matrix composites containing at least one hard friction material. The friction material may be a continuous fiber, a discrete fiber, or other particulate forms. Furthermore, the fibers may be in continuous or yarn form. Most, if not all, friction materials for brake discs and pads are commercially available proprietary formulations. Emphasis on high temperature performance has directed development to ceramic matrix materials containing friction producing elements such as fibers. An example of recent prior art braking friction materials is described in U.S. Pat. No. 5,806,636 to Atmur et al. and incorporated herein as reference. The brake materials described are a family of fiber reinforced ceramic matrix composite (FRCMC) materials with high fracture resistance and high temperature stability. The fibers provide the friction component. Several ceramic matrix compositions are polymer derived and commercially available such as silicon-carboxyl resin (sold as Allied Signal Blackglas) and alumina silicate resin (Applied Polymerics C02) combined with fiber systems such as Nextel 312, Nextel 550, silicon nitride, silicon carbide, graphite, carbon, and others.
Before the fibers are consolidated, they are first coated with an interface material such as silicon nitride, silicon carbide, or boron nitride to allow partial separation between the matrix and fibers after firing to allow fiber pullout during fracture if the material is overloaded during use. The brake parts are produced by first mixing polymer resin with the coated fiber system. Alumina or mullite powder is then added for additional wear resistance. The resin mixture is then formed into a part and fired to about 1800° F. (982° C.) to convert the mixture into a FRCMC. Wear resistance in completed parts is improved by aligning fibers in the vicinity of the near surface region of the part during lay-up.
The above prior art material is an example of state of the art brake materials with high temperature resistance, good thermal conductivity, good braking friction due to the fiber content, and wear resistance due to the ceramic additions. Most large aircraft braking systems and braking systems in high performance race cars use carbon/carbon composite friction materials such as the ones described above.
Other braking materials in the art comprise organic and inorganic based matrix composites containing metal fibers, organic and inorganic fibers, and other abrasives, as well as modifiers such as glass, rubber, minerals, and lubricants, and mixtures thereof. All breaking materials need fracture toughness values sufficient to resist fracture under loads experienced in hard braking conditions.
As noted above, frictional heating is an important issue with braking systems in high performance applications. Heat may be transmitted through brake pads 26, backing plates 28, and piston 32 into cylinder 34 to heat hydraulic fluid. If the heating is excessive, braking efficiency may be degraded. The present invention is an improved brake pad assembly with a thermal barrier. The thermal barrier restricts thermal flow toward hydraulic cylinder 34 while allowing lateral heat flow to escape the system. The thermal barrier has bimodal thermal conductivity. The thermal conductivity in a longitudinal direction toward piston 32 and cylinder 34 is lower than the thermal conductivity in a lateral direction towards the sides of the brake pad assembly.
A schematic of inventive brake pad 26′ is shown in
Friction layer 40 comprises a friction material known to those in the art. An example of the material of friction layer 40 is the FRCMC material described above, comprising, for instance, carbon fiber reinforced, polymer precursor carbon matrix containing a ceramic addition to reduce wear. Backing plate 28 may be steel as described above.
Friction layer 40, thermal insulating layer 42 and backing plate 28 may be bonded to each other by mechanical means, by adhesive or chemical means, or by other attachment means known in the art. Providing proper lateral restraint exists such as, for example, a steel container supporting the lateral surface of inventive brake pad 26′, friction material 40 and thermal insulating layer 42, need not be bonded to each other.
Thermal insulating layer 42 may be a fiber reinforced ceramic matrix composite (FRCMC) material with a high fracture toughness and low thermal conductivity. In an embodiment, insulating layer 42 may have anisotropic thermal conductivity wherein the thermal conductivity in the short transverse direction, that is, the direction perpendicular to the surface of the layer, is lower than the thermal conductivity in a direction parallel to the top and bottom surfaces of thermal insulating layer 42.
A schematic showing the structural details of FRCMC thermal insulating layer 42 of the invention with anisotropic thermal conductivity is shown in
The thermal insulating layers of the invention comprise, in general, fiber reinforced ceramic matrix composites. The matrix thermal conductivity of thermal insulating layer 42 is suggested to be less than conventional ceramic materials such as oxide, nitride, and carbide ceramics. As a benchmark, the thermal conductivities of polycrystalline aluminum oxide, silicon carbide, silicon nitride, and boron nitride are about 0.30 W/cmK, 0.14 W/cmK, 0.24 W/cmK, and 0.25 W/cmK respectively. According to the invention, the thermal conductivity of the ceramic matrix may be from about 0.01 W/cmK to 0.05 W/cmK. Ceramic materials with thermal conductivities in this range are mainly confined to the families of glasses and glass-ceramics. For example, the thermal conductivities of fused silica, sodalime glass, and pyrex glass, are 0.015 W/cmK, 0.015 W/cmK, and 0.010 W/cmK, respectively an order of magnitude lower than those of ceramic materials quoted above. The thermal conductivities of silicate based glass-ceramics are about the same as the glasses. In an embodiment, thermal insulating layer 42 is a fiber reinforced glass or glass-ceramic matrix composite wherein the matrix may be a silicate glass or glass-ceramic with a thermal conductivity from about 0.01 W/cmK to 0.05 W/cmK. The fibers may be ceramic fibers with thermal conductivities exceeding that of the matrix. As a result, the anisotropic thermal conductivity of thermal insulating layer 42 may be controlled, if necessary, by the geometrical distribution of the fiber load in the matrix in thermal insulating layer 42. For example, if the thermal conductivity in the plane of layer 42 is designed to be greater than that in the short transverse direction perpendicular to the plane, it is advantageous that the fibers have a length that is a significant fraction of the thickness of layer 42 and that the majority of the fibers are oriented parallel to the plane of layer 42. In a FRCMC material with the above mentioned internal structure, part of the heat flux in the layer from friction layer 40 under extreme braking conditions will be directed toward the outside edges of the layer away from the backing plate and components beneath it as suggested by
Procedures to produce FRCMC thermal insulating layers with predesigned geometric fiber loading to produce materials with anisotropic thermal conductivities such as the example described above, are known in the art and can be applied to produce the insulating material of the present invention.
The thermal conductivities of fibers in the FRCMC friction material of this invention are advantageously greater than the glass and glass-ceramic matrices of the invention. As an example, the thermal conductivities of silicon carbide fibers and graphite fibers known in the art exceed 0.4 W/cmK and 1.0 W/cmK respectively.
In the 1980s and 1990s, a series of fiber reinforced ceramic matrix composites (FRCMC) were developed by United Technologies Corporation are that. A number of these materials can be used to advantage in the present invention. The Compglas® composites comprised glass or glass-ceramic matrices containing carbon or silicon carbide fibers. Mechanical properties and thermal resistance were exceptional. Exemplary matrix materials included borosilicate glass, high silicon content glass, aluminosilicate glass, and lithium aluminosilicate glass-ceramic. Thermal stability to temperatures greater than 1800° F. (982° C.) and flexural strengths to values greater than 300 MPa were achieved. In an embodiment, Compglas® and similar materials with anisotropic fiber orientation are candidates for application as thermal insulating layer 42.
While the invention has been described with reference to an exemplary embodiment(s), it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from the essential scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiment(s) disclosed, but that the invention will include all embodiments falling within the scope of the appended claims.
The following are non-exclusive descriptions of possible embodiments of the present invention.
A brake assembly can be attached to a vehicle frame to engage a rotor attached to a vehicle wheel during a braking event. The brake assembly can include a caliper, multilayer brake pads supported by the caliper and a backing layer. The brake pads are comprised of a thermal insulating layer of fiber reinforced ceramic matrix composite thermal insulating material in contact with and positioned behind a layer of friction material. A hydraulic cylinder assembly is supported by the caliper and comprises a piston movable within a hydraulic cylinder to forcibly push the brake pads against the rotor to frictionally engage the rotor during a braking event.
The assembly of the preceding paragraph can optionally include, additionally and/or alternatively any one or more of the following features, configurations, and/or additional components:
A multilayer brake pad assembly may comprise a friction layer of friction material, a backing layer, and a thermal insulating layer of a fiber reinforced ceramic matrix composite material positioned between the friction layer and the backing layer of the assembly.
The assembly of the preceding paragraph can optionally include, additionally and/or alternatively any one or more of the following features, configurations, and/or additional components:
A brake pad assembly may comprise a piston and a brake pad moveable by the piston wherein at least one of the brake pad and the piston comprise a fiber reinforced ceramic matrix composite thermal insulating material.
The assembly of the preceding paragraph can optionally include, additionally and/or alternatively any one or more of the following features, configurations, and/or additional components:
