The present invention relates to a compact cooling device for an internal combustion engine and to a method for manufacturing such a cooling device.
A spray nozzle for cooling a piston of an internal combustion engine enables a cooling fluid such as oil to be projected on to an appropriate area of the piston.
Piston cooling spray nozzles are habitually formed by separate parts attached to the engine block are linked to a cooling fluid inlet aperture. The spray nozzle's position is determined accurately to produce a cooling fluid jet directed towards a precise area of the base of the piston, or towards an inlet of a piston oil channel. In motor vehicles of the recreational vehicle type and private passenger vehicle type the internal combustion engines are fitted with simple spray nozzles, each of which directs a fluid jet on to a piston.
However it is desirable, in order to increase the cooling efficiency, to have several cooling fluid jets with identical or different target areas.
In the field of heavy goods vehicles or site plant the engines are subject to particularly high stress and require a more powerful cooling system. Such a cooling system represented in
To make cooling system able to provide two jets per piston more compact bidirectional spray nozzles have been developed, where the spray nozzle comprises a single tube and two outlets to provide two jets pointing in different directions.
Such a spray nozzle is described in document EP 1 394 376. Indeed, this spray nozzle is compact, and suitable for a recreational motor vehicle and private motor vehicle; however it has a smaller flow rate compared to the cooling system with two separate tubes, and the accuracy of the jets may be less satisfactory than that of a cooling system with two separate tubes.
Document JP H07 317519 describes a device for lubricating and cooling an internal combustion engine comprising a main body on which an assembly with two pipes is assembled, where the pipes are in fluid communication with the main body. The two tubes are manufactured such that they are coupled securely to one another, and cannot be shaped separately.
One aim of the present invention is consequently to provide a cooling device allowing improved cooling, whilst being more compact and having jets with satisfactory target accuracy, and which provides a simplified method of manufacture of such a cooling device.
The aim mentioned above is attained by a cooling device comprising two superposed separate tubes; by this means the cooling device is made more compact. Each tube also forms with a feed body a subassembly which is manufactured separately from the other subassembly, the tubes being orientated before the two subassemblies are attached to one another. The tubes are then directly correctly orientated, and do not require an orientation step, for example by bending the tubes after assembly. By this means an additional step of bending the tubes is avoided, which would require equipment to be installed between the close tubes, which would pose problems of feasibility.
The cooling device according to the present invention is therefore relatively simple to produce, and compact, and has satisfactory accuracy in terms of the cooling jets, and a cooling flow rate comparable to the device of the state of the art, with two separate tubes.
It may be envisaged to use this cooling device with at least two cooling tubes, with one or two pistons.
The cooling device may comprise more than two separate tubes, where the cooling tubes are then added in a very simple manner, for example by superposing another subassembly consisting of a tube and a feed body.
The subject-matter of the present invention is then a cooling device for a motor vehicle engine comprising an end for connection to a cooling fluid feed system and at least one first end and one second end for evacuating cooling fluid towards one or more areas for cooling, where said cooling device comprises at least one first and one second superposed subassembly, where the first subassembly comprises a first feed body connected to the feed aperture, and a first tube connected to the first feed body the free end of which forms the first evacuation end, where the first tube extends laterally relative to the first feed body, and is shaped so as to have a desired orientation, where the second subassembly comprises a second feed body connected to the feed aperture, and a second tube connected to the second feed body the free end of which forms the second evacuation end, where the second tube extends laterally relative to the second feed body, and is shaped so as to have a desired orientation, and where the first and second feed bodies are securely attached to one another in sealed fashion.
The first and second subassemblies are, for example, securely attached by brazing. Alternatively, the first and second subassemblies are securely attached by means of a valved-bolt assembly.
The first feed body may comprise the feed aperture of the cooling device and the second subassembly may be intended to be supplied with cooling fluid through the first feed body.
In one example embodiment each first and second subassembly comprises two tubes.
According to an additional characteristic the device may comprise means to control the flow of the cooling fluid.
The cooling device preferably comprises means for attachment to an engine block. In one example embodiment the means of attachment to an engine block are formed by a securing plate attached to a first feed body which can be attached to the engine block. In another example embodiment the valved-bolt assembly also forms the means of attachment to the engine block.
The device may advantageously comprise means of orientation relative to the engine block. The orientation means are, for example, supported directly by the first feed body or by a plate which is securely attached to the first feed body. The orientation means may be formed by a pin intended to penetrate into an aperture formed in the engine block.
Another subject-matter of the present invention is an internal combustion engine comprising an engine block and pistons installed such that they can slide in said engine block, and at least one cooling device according to the invention, where at least one of the tubes of said cooling device is pointing towards a piston.
Another subject-matter of the present invention is a method for the manufacture of a cooling device according to the invention, comprising the following steps:
a) construction of a first subassembly comprising a first feed body fitted with a feed aperture intended to be connected to a cooling fluid feed system, and at least one first tube, where said first tube is connected to the first feed body,
b) construction of a second subassembly comprising a second feed body comprising a feed aperture intended to be connected to a cooling fluid feed system, and at least one second tube connected to the second feed body,
c) shaping of the first tube so as to give it a given orientation,
d) shaping of the second tube so as to give it a given orientation,
e) assembly and secure attachment of the two subassemblies.
In a preferred manner, the first tube and the second tube are shaped so as to give them a given orientation before the two subassemblies are assembled.
The shaping of the first tube and of the second tube is accomplished for example by bending.
The step of secure attachment of the first and second subassemblies may be accomplished by brazing between the feed bodies.
As a variant, the step of secure attachment of the first and second subassemblies is accomplished by means of a valved-bolt assembly.
The manufacturing method may comprise an additional step of shaping of the free end of at least one of the first and second tubes after step e).
The present invention will be better understood using the description which follows and the appended illustrations, in which:
In
The cooling device comprises a first subassembly E1 and a second subassembly E2 which are securely attached to one another.
First subassembly E1 comprises first tube 2 and a feed body 6. First tube 2 comprises a first end 2.1 by which it is attached to feed body 6, and a second free end 2.2 intended for the outlet of the cooling fluid jet and for its orientation in the direction of the piston.
Feed body 6 is hollow and comprises a first longitudinal end 6.1 intended to be connected to a cooling fluid feed circuit of the internal combustion engine, a second longitudinal end 6.2 configured to feed second subassembly E2 with cooling fluid, and a lateral aperture 8 for connection to first end 2.1 of first tube 2. Body 6 thus causes the cooling fluid to flow from first longitudinal end 6.1 to end 2.2 of first tube 2 via lateral aperture 8 and towards second longitudinal end 6.2.
The second subassembly comprises second tube 4 and a second feed body 10.
Second feed body 10 comprises a longitudinal end 10.1 connected to second longitudinal end 6.1 of first feed body 6. Second feed body 10 also comprises a lateral aperture 11, to which second tube 4 is connected by a first end 4.1. Second tube 4 also comprises a second end 4.2 through which the cooling fluid jet is evacuated and directed towards a piston.
Feed body 10 is separate from feed body 6 and is securely attached to it. In the represented example feed body 10 comprises a connecting sleeve projecting from first longitudinal end 10.1 of the second feed body fitted into second longitudinal end 6.2 of first feed body 6. In the represented example first feed body 6 has the shape of a cylinder of axis X1, and second feed body 10 has the shape of a cylinder of axis X2. Feed bodies 6, 10 are superposed on one another, and longitudinal axes X1, X2 are coaxial.
In the example of
In
For example, tubes 2 and 4 are attached to feed bodies 6, 10 respectively, for example by brazing.
The method of manufacture of the cooling device according to the invention will now be described.
In a first step, each subassembly E1, E2 is manufactured separately, the first tube is attached securely to first feed body 6 by its longitudinal end 2.1, for example by brazing, and second tube 4 is securely attached to second feed body 10 by its longitudinal end 4.1, for example by brazing. At the end of this step the tubes are generally straight.
In a subsequent step the tubes are deformed to give them a desired orientation relative to their feed body. In the represented example only a portion of the length of the tube located at the free end of the tube is deformed, for example by bending, to orientate it in a given direction, which will be the direction of the jet. In this example it is not the entire length of the tube which is deformed.
As a variant, it could be envisaged to deform the tube from its end connected to the feed body, as represented in
Tubes 2 and 4 are deformed before assembly and secure attachment of the two subassemblies E1, E2. The step of orientation of the tubes is thus simplified, since the equipment can be positioned freely without being hindered by the presence of another tube.
In a subsequent step, when first 2 and second 4 tubes have the desired orientation, the two feed bodies 6, 10 are securely attached to one another in sealed fashion. For example, the two bodies are securely attached by brazing.
As a variant, assembly by insertion fitting and brazing could be envisaged, for example second feed body 10 is fitted into first feed body 6, and this is then followed by brazing. As a variant, insertion fitting only may be sufficient. Indeed, for a minimal 15 Bar feed pressure, assembly by insertion fitting may be accomplished such that a seal is preserved.
Orientation means may preferentially be comprised between the two subassemblies E1, E2, such as an orientation key form, or an orientation pin.
After the two subassemblies are securely attached there may be an additional step of bending of the free ends of the tubes, to adjust their orientation. It will however be understood that most of the deformation of the tubes to determine their orientation is accomplished before the two subassemblies are assembled.
In
As can be seen in
In
In
Orientation means may advantageously be comprised between the two feed bodies 106, 110, such as those described in relation with
It will be understood that every other means of attachment of the cooling device to the engine block may be used.
In
This device is produced in a similar manner to the one described above for the example embodiments of the devices of
In
In
It could also be envisaged not to have the tubes of both subassemblies contained roughly in the same vertical plane, but to have them contained in two separate planes.
In
The cooling device can also comprise means to inhibit the flow of the cooling fluid until the pressure of the cooling fluid exceeds a determined threshold value. These means are formed for example by ball valves or piston valves. Such means are installed, for example, in the first feed body, and by this means control the feed of both tubes 2, 4 simultaneously.
Using the present invention cooling devices can be inserted in small spaces of the motor vehicle engines, whilst proximity with the rotating elements is ensured. Indeed, in very compact cooling devices they can be positioned as close as possible to the rotating elements which it is desired to cool. In addition, due to its manufacturing method, great flexibility can be obtained in terms of the targeting angles of each of the jets, and the jets can also be made very accurate.
The tubes of a cooling system may be convergent, divergent or intersecting. They may also be used to cool one piston, or several pistons. It may also be envisaged for the cooling device to have more than two tubes, for example three, where these all point towards the same piston.
The cooling device may also comprise more than two subassemblies, for example three or more. If there are three subassemblies the second feed body then roughly has the shape of the first feed body, and the third feed body has that of the second feed body of the device of
Number | Date | Country | Kind |
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13 53293 | Apr 2013 | FR | national |
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Number | Date | Country | |
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20140305392 A1 | Oct 2014 | US |