AU2002334092A1 - Rotor disc for a disc brake - Google Patents
Rotor disc for a disc brakeInfo
- Publication number
- AU2002334092A1 AU2002334092A1 AU2002334092A AU2002334092A AU2002334092A1 AU 2002334092 A1 AU2002334092 A1 AU 2002334092A1 AU 2002334092 A AU2002334092 A AU 2002334092A AU 2002334092 A AU2002334092 A AU 2002334092A AU 2002334092 A1 AU2002334092 A1 AU 2002334092A1
- Authority
- AU
- Australia
- Prior art keywords
- rotor disc
- disc
- substrate
- coating layer
- composite
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
Description
ROTOR DISC FOR A DISC BRAKE
The present invention relates to a rotor disc, particularly, but not
exclusively for a disc brake and the like.
Traditionally, brake discs have been made of cast iron. Cast iron
exhibits the necessary thermal and strength characteristics for this purpose.
A disadvantage, however, is its weight. In an average motor vehicle with
disc brakes on all four wheels the rotor discs of the brakes may add 40 kg
to the weight of the vehicle. This weight is carried permanently around
with the vehicle, although the brakes may be used relatively infrequently,
thus adding to fuel consumption and emissions. Making discs of other
lighter materials has been proposed but so far a satisfactory solution has not
yet been found. For example, aluminium has been suggested but although
its thermal properties are good they are not as good as those of cast iron.
These poorer thermal characteristics adversely affect the performance of the
material as a rotor disc.
According to the present invention there is provided a composite rotor
disc comprising a substrate made of a thermally conductive material, a first
coating layer on at least one circular face of the disc, the first coating layer
being made of a thermally insulating material and a second coating layer
superposed on the first coating layer, the second coating layer being made
of a wear resistant, thermally conductive material whereby the substrate is
protected from heat generated at the circular surface of the disc.
In a preferred embodiment of the invention, the substrate is
advantageously aluminium or other suitable metal or metallic alloy. The first
coating layer may advantageously be Zirconia or other ceramic. The second
coating layer may advantageously be a carbon-silicon carbide composite or
other metallic alloy. The thicknesses of the layers and substrate
advantageously lie in the following ranges. Layers 0.01 to 2.00mm
substrate 5-40mm
In order that the invention may be more clearly understood
embodiments thereof will now be described, by way of example, with
reference to the accompanying drawings, in which:-
Figure 1 shows a cross section through a part of a rotor disc according
. to the invention.
Figure 2 shows a front elevational view of the rotor disc of figure 1 ,
Figure 3 shows a cross-section of a modification of the rotor disc of
figures 1 and 2, and
Figure 4 shows a cross-section of a further modification of the rotor
disc of figures 1 and 2.
Referring to Figures 1 and 2 the rotor disc is indicated generally by
the reference numeral 1 and ~~ .nprises a circular substrate 2 and two
superposed coating layers 3 and 4 disposed on both outer circular faces of
the substrate. The substrate is vented at 5 so that air may circulate through
the substrate to cool the substrate. The substrate 2 is made from a low
density but high thermal conductivity material such as aluminium or other
suitable metal or metallic alloy. The outer coating layer 3 is made from a
high thermal conductivity and high wear resistant material such as a carbon-
silicon carbide composite or metallic-type material. The inner coating layer
4 is made from a thermally insulating material such as zirconia or other
ceramic material.
In operation under braking conditions heat is generated on both
surfaces of the disc due to friction between the brake pad shown
diagrammatically at 6 and the rotor disc 1 as the disc 1 rotates causing the
temperature of the disc 1 to rise. Heat is lost from the disc 1 by conduction
convection and radiation. Heat lost by conduction is to the surrounding air
and through the material of-the outer layer 3. to. inner layer 4„an. Jhro.ugh
that layer to the substrate 2 beneath. Heat lost by convection is to the
surrounding air as the air moves relative to all surface of the disc including
those opening to the vent 5. Heat lost by radiation is lost from all hot
surfaces. An exemplary temperature profile through the rotor disc 1 is
shown at 7. The temperature is at its maximum on both outer surfaces of
the disc 1 where the heat is generated through the friction between the disc
brake pad 6 and those surfaces. Heat is conducted relatively easily through
the outer layers 3, which are made of a highly thermally conductive and
wear resistant material, to the inner layers 4, and the fall in temperature
through those layers is correspondingly small. Heat conduction through the
inner layers 4, which is made of a thermally insulating material, is restricted
and, as compared with the outer layer there is a greater fall in temperature.
The inner layers 4 therefore operate to protect the substrate from the heat
and high temperatures generated at the outer surfaces of the disc 1 . The
temperature at the interface between the substrate 2 and the inner layers 4
is much less than that between the outer and inner layers 3 and 4 and it
continues to fall across the material of the substrate heat flowing through
the substrate being removed at the surfaces adjoining the vent 5 by
conduction, convection and radiation.
The thickness of the layers 3 and 4 is advantageously in the range
0.05 to 5.00 millimetres, preferably in the range 0.01 to 2.00 millimetres
and in. this-example outer layers 3 are 1 .0 millimetres thick and inner layers ..
4 are 0.5 millimetres thick. The thickness of the substrate lies in the range
5 to 40 millimetres. By appropriately choosing the dimensions of the layers
and substrate and the material from which the layers and substrate are
made the thermal behaviour of the rotor disc may effectively be 'tuned' for
optimum operational performance.
In a modification, a protective layer may be disposed over the outer
cylindrical surface and adjacent the vent of the substrate as shown in figure
3 to protect the substrate against oxidation in all regions not coated by
layers 3 and 4. In this modification parts equivalent to the parts of the
embodiment of figures 1 and 2 bear the same reference numerals.
With the above described arrangements heat maybe conducted around the
outer layer(s)3 and lost by convention from the surface thereof. Heat from
the outer layer(s) may also be dissipated by controlled conduction through
the inner layer 4 and through the substrate 3 and lost by convention from
the surfaces adjacent the vent 5 in the substrate.
Although the disc has been described with a vent, the vent may be
dispensed with. Such an arrangement is illustrated in Figure 4. In this
figure parts equivalent to parts in figures 1 to 3 bear the same reference
numerals.
It will be appreciated that the above embodiment has been described
by way of example only and that many variations are possible without
departing from the scope of the invention.
Claims (15)
1 . A composite rotor disc a composite rotor disc comprising a substrate
made of a thermally conductive material, a first coating layer on at
least one circular face of the disc, the first coating layer being made
of a thermally insulating material and a second coating layer
superposed on the first coating layer, the second coating layer being
made of a wear resistant, thermally conductive material whereby the
substrate is protected from heat generated at the circular surface of
the disc.
2. A composite rotor disc as claimed in claim 1 , in which the substrate
is metal.
3.. A composite, rotor disc as claimed in claim 1 , in which the_m.etal in.
aluminium.
4. A composite rotor disc as claimed in claim 1 , in which the substrate
is a metallic alloy.
5. A composite rotor disc as claimed in any preceding claim, in which
the full coating layer is a ceramic.
6. A composite rotor disc as claimed in claim 5, in which the ceramic is
zirconia.
7. A composite rotor disc as claimed in any preceding claims, in which
the second coating layer is a metallic alloy.
8. A composite rotor disc as claimed in claim 7, in which the metallic alloy is a carbon-silicon carbide composite.
9. A composite rotor disc as claimed in any preceding claim, in which
the thickness of the substrate lies in the range 5 to 40 millimetres.
10. A composite rotor disc as claimed in any preceding claim, in which
the thickness of the layers lies in the range 0.05 to 5.00 millimetres.
1 1 . A composite rotor disc as claimed in any of claims 1 to 9, in which
the thickness of the layers lies in the range 0.01 to 2.00 millimetres.
1 2. A composite rotor disc as claimed in any preceding claims, in which
the first coating layer is 0.5 millimetres thick.
1 3. A composite rotor disc as claimed in any preceding claims, in which
the second coating layer is 1 .00 millimetres thick.
14. A composite- rotor- disc as claimed in any preceding claims, in which
the substrate is vented.
1 5. A composite rotor disc as claimed in any preceding claims, in which a
protective coating is disposed over the outer cylindrical surface.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0123618.1 | 2001-10-02 |
Publications (1)
Publication Number | Publication Date |
---|---|
AU2002334092A1 true AU2002334092A1 (en) | 2003-04-14 |
Family
ID=
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP3679444B2 (en) | Composite disc for high energy braking | |
US11396207B2 (en) | Wheel hub unit with thermally insulating coating for reducing the thermal load on a wheel bearing | |
US5377792A (en) | Friction pad of a disc brake for a vehicle | |
EP3403849B1 (en) | Insulator for heat generated by high friction | |
US20040094375A1 (en) | Piston having a cap and a brake caliper for use therewith | |
JP6863551B2 (en) | Heat shield structure for wheels | |
WO2013043634A1 (en) | Composite rotor | |
WO1992005292A1 (en) | Metal matrix composite component | |
KR20220147111A (en) | Brake disc and its manufacturing method | |
AU2002334092A1 (en) | Rotor disc for a disc brake | |
WO2003029683A1 (en) | Rotor disc for a disc brake | |
US5435420A (en) | Thermal insulating wheel spacer | |
US20050236240A1 (en) | Pad for calipers of disk brakes | |
KR20200054302A (en) | Disc brake | |
US5521015A (en) | Metal matrix composite component | |
CA2065686C (en) | Lightweight and high thermal conductivity brake rotor | |
JP3484275B2 (en) | Friction material | |
GB2388560A (en) | Carbon-carbon brake disc with protective outer layer on friction surface | |
JPH0130015B2 (en) | ||
McClure | A study of transfer films formed on the surface of automotive friction couples | |
AU2001100239A4 (en) | An improved method of cooling disc-brakes | |
JPH0571812B2 (en) | ||
JP2003120734A (en) | Vehicular brake rotary body | |
JPH08226478A (en) | Disk brake | |
KR20170132993A (en) | Different materials disc brake |