(19) |
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(11) |
EP 1 046 805 A2 |
(12) |
EUROPEAN PATENT APPLICATION |
(43) |
Date of publication: |
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25.10.2000 Bulletin 2000/43 |
(22) |
Date of filing: 19.04.2000 |
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(84) |
Designated Contracting States: |
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AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE |
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Designated Extension States: |
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AL LT LV MK RO SI |
(30) |
Priority: |
23.04.1999 GB 9909284
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(71) |
Applicant: Howie, Robin Middlemass |
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Edinburgh, EH1O 4DB (GB) |
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(72) |
Inventor: |
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- Howie, Robin Middlemass
Edinburgh, EH1O 4DB (GB)
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(54) |
Internal combustion engine |
(57) A means of improving the performance of internal combustion engines by coating the
surfaces of combustion chambers, such as cylinder heads, inlet and outlet valves,
and piston crowns, and inlet and exhaust valve ports with a layer of low thermal mass
formed from a suitable combination of thermally conducting and thermally insulating
materials.
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[0001] This invention relates to internal combustion engines.
[0002] In conventional internal combustion engines, a proportion of the heat generated by
combustion of the fuel-air charge is lost to the surfaces of the combustion chamber,
therefore reducing the temperature of the combustion products, power output and fuel
efficiency. In addition, heat lost to the surfaces of the combustion chamber, ie.
the walls of the combustion chamber, the crown of the piston and any inlet and outlet
valves fined, can heat the incoming fuel-air charge so effectively reducing the mass
of fuel-air charge available for combustion and reducing the available power output
in an engine of a given size. In general terms the weight of charge admitted to naturally
aspirated engines decreases by about 1% per 3 - 4 C° increase in fuel-air charge temperature
prior to compression. That is, heat lost to the surfaces of the combustion chamber
reduces the power output by both reducing the temperature of the fuel-air charge following
combustion and by reducing the mass of fuel-air charge available for combustion. Heat
lost to the surfaces of the combustion chamber increases the heat rejection load imposed
on the engine cooling system.
[0003] A number of techniques have been applied to reducing heat loss to the surface of
the combustion chamber. One effective technique is to coat such surfaces with a suitable
heat insulating ceramic material. However, such treatment has limited operational
lifetimes, typically of the order of 1,000 hours. While adequate for race engines
which are regularly stripped following each race, such limited lifetime would be unsuitable
for vehicles or other equipment used for normal industrial, commercial or domestic
purposes.
[0004] The effect of coating engine surfaces with thermally insulating materials effectively
coats the surfaces with a material with low thermal mass.
[0005] A mechanically robust coating of low thermal mass can be obtained by covering the
surfaces of interest with a thin layer of thermally resistant metal backed by a layer
of thermal insulation between the thin metal layer and the surface being coated so
that the metal layer is supported by the insulation and the insulation is protected
against damage by the metal surface. The metal layer can consist of thermally resistant
metals such as nickel or chromium. The insulation layer can consist of the ceramic
material currently sprayed onto combustion chamber surfaces or of suitable minerals
such as mica or pearlite powder. The thickness of the metal layer is minimised to
reduce its thermal mass. The metal layer is suitably bonded to the surface being coated
to provide a robust protection to the thermal insulation below, the thickness of the
metal is made small compared to the distance to any point of bonding to the underlying
surface so that heat conduction along the metal coating is small compared with heat
transfer between the metal surface and the underlying surface through the insulation
layer.
[0006] A specific embodiment of the invention will now be described by way of example only
with reference to Figure 1 which shows application of the invention to a piston crown.
[0007] Modified Piston Crown 10 is formed on Piston 11 in the form of a 0.5 mm thick layer
of Mineral Insulation 12 covered by Cup 13 of a 0.2 mm thickness of a nickel/chromium
high temperature alloy. Cup 13 is welded at Circumference 14 to a suitable alloy Ring
15 located in a slot in Piston 11 such as provided for Piston Rings 16 and 17. The
outside diameter of welded Circumference 14 is slightly smaller than the outside diameter
of Piston Rings 16 and 17 so that there is no contact between Cup 13 and the walls
of the cylinder.
[0008] The thickness of the metal of Cup 13 is selected such that the Cup has sufficient
physical strength when supported by Mineral Insulation 12 to withstand the detonation
of the fuel-air charge in the cylinder and such that the overall thermal conduction
from the upper surface of the Cup to Piston 11 is small compared with thermal conduction
through Mineral Insulation 12. That is, overall heat transfer to Piston 11 is controlled
by Mineral Insulation layer 12.
[0009] The reduced heat load on Piston 11 potentially enables the overall mass of the piston
to be reduced thus improving engine fuel efficiency.
1. A means of improving the performance of internal combustion engines by coating the
surfaces of combustion chambers, such as cylinder heads, inlet and outlet valves,
and piston crowns, and inlet and exhaust valve ports with a layer of low thermal mass
formed from a suitable combination of thermally conducting and thermally insulating
materials.
2. A means of improving the performance of internal combustion engines as described in
Claim 1) in which the layer of low thermal mass consists of an outer layer of thermally
conducting robust materials resistant to high temperatures physically supported by
a layer of mechanically robust thermally insulating materials.
3. A means of improving the performance of internal combustion engines as described in
Claims 1 and 2) in which the layer of low thermal mass consists of a layer of thermally
conducting robust materials resistant to high temperatures physically supported by
a layer of mechanically robust thermally insulating materials and in which the thickness
of the thermally conducting layer is selected such that thermal conduction along the
thermally conducting layer is small compared to thermal conduction through the thickness
of the thermally insulating layer.
