Oil decantation system for an internal combustion engine

Abstract

The invention relates to an oil decantation system (1) comprising: (i) a separator device (6) designed to trap the oil droplets (107) that are present in a flow of a blow-by gas (110); and (ii) a jet pump (5) positioned upstream of the separator device (6) and designed to accelerate and draw the flow of the blow-by gas (110) before it enters said separator device (6).

Claims

1. An oil decantation system for an internal combustion engine comprising: a separator device configured to trap oil droplets that are present in a flow of a blow-by gas; and a jet pump positioned upstream of the separator device configured to accelerate the flow of the blow-by gas before it enters said separator device, wherein the jet pump comprises: a tubular body a first end of which comprises a fitting for connection to a source of propellant gas and a second end of which comprises a nozzle; and a conduit disposed opposite the separator device, the nozzle opening into the conduit.

2. The decantation system according to claim 1, wherein the decantation system further comprises a secondary passage closed by a movable flap, disposed in parallel with the jet pump allowing increasing a passage area of the flow of the blow-by gas.

3. The decantation system according to claim 1, wherein the jet pump comprises a check valve.

4. The decantation system according to claim 2, wherein the decantation system comprises an aperture sealed by a movable flap, the aperture delimiting the secondary passage towards the separator device.

5. The decantation system according to claim 1, wherein the decantation system comprises a wall, an upstream face of the wall physically receives the conduit and a downstream face of the wall physically receives the separator device, the conduit and the separator device being in communication by an opening formed in the wall.

6. The decantation system according to claim 5, wherein the conduit is integrally molded with the wall.

7. The decantation system according to claim 1, wherein the decantation system comprises a wall, an upstream face of the wall physically receives the conduit and a downstream face of the wall physically receives the separator device, the conduit and the separator device being in communication by an opening formed in the wall, and wherein the opening has a semi-circular upper area and a trapezoidal lower area, the semi-circular upper area facing the conduit whereas the trapezoidal lower area faces the opening.

8. The decantation system according to claim 4, wherein the decantation system comprises a wall, an upstream face of the wall physically receives the conduit and a downstream face of the wall physically receives the separator device, the conduit and the separator device being in communication by an opening formed in the wall, and wherein the decantation system comprises a wall of material which extends between an external face of the conduit and the wall in which is formed the aperture forming the secondary passage.

9. The decantation system according to claim 2, wherein the movable flap is held in a closed position by gravity.

10. The decantation system according to claim 1, wherein the separator device comprises a valve provided with decantation means separating the droplets and a clean gas.

11. An internal combustion engine comprising a decantation system according to claim 1.

12. The decantation system according to claim 2, wherein the jet pump comprises a check valve.

13. The decantation system according to claim 1, wherein the decantation system comprises an aperture sealed by a movable flap, the aperture delimiting a secondary passage towards the separator device.

14. The decantation system according to claim 3, wherein the decantation system comprises an aperture sealed by a movable flap, the aperture delimiting a secondary passage towards the separator device.

15. The decantation system according to claim 2, wherein the decantation system comprises an aperture sealed by a movable flap, the aperture delimiting the secondary passage towards the separator device.

16. The decantation system according to claim 12, wherein the decantation system comprises an aperture sealed by a movable flap, the aperture delimiting the secondary passage towards the separator device.

17. The decantation system according to claim 16, wherein the decantation system comprises a wall, an upstream face of the wall physically receives the conduit and a downstream face of the wall physically receives the separator device, the conduit and the separator device being in communication by an opening formed in the wall.

18. The decantation system according to claim 17, wherein the conduit is integrally molded with the wall.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) The invention will be better understood upon reading the following non-limiting description, with reference to the appended figures.

(2) FIGS. 1, 2, 4 and 5 show, in a longitudinal sectional view, a decantation system according to several operating regimes;

(3) FIG. 3 is an enlarged scale view illustrating the operation of an jet pump of the decantation system according to the invention;

(4) FIG. 6 represents a variant of the device shown in FIGS. 1, 2, 4 and 5;

(5) FIGS. 7 and 8 show a wall and the opening made in this wall which connects the jet pump and the decantation system;

(6) FIG. 9 is a graph showing the spectral efficiency at different flow rates of a decantation system according to the prior art and a decantation system according to the invention;

(7) FIG. 10 shows an engine equipped with a decantation system according to the invention.

DETAILED DESCRIPTION

(8) Schematically, an internal combustion engine 100 as represented in FIG. 10 comprises in particular a cylinder 101 within which a piston 102 moves, a crankcase 103 within which oil 106 splashes, and a suction duct 104. During the operation of the engine, burnt gases 105 infiltrate into the oil pan 103 passing between the cylinder 101 and the piston 102 throughout the piston's rings. Their evacuation causes a gas flow called blow-by gas 110 loaded with oil droplets collected during splashing in the oil 106.

(9) The engine 100 is equipped with an oil separator device 1 according to the invention.

(10) The blow-by gases 110 are routed at the inlet of the oil separator device 1 according to the invention, the latter allowing freeing the flow of the blow-by gas 110 from the oil droplets contained therein. The captured oil droplets 107 are collected and routed towards the oil pan 103 for recycling. The gaseous flow 111 freed from the oil droplets is evacuated into the air suction duct 104 of the engine.

(11) Referring to FIG. 1, the oil separator system 1 according to the invention comprises a tubular body 2 having an inlet duct 3 for a blow-by gas 110 which is connected to a crankcase of an engine, an outlet duct 4 which is connected to the intake of this engine, an jet pump 5 intended to accelerate the speed of the blow-by gas 110 and an oil separator device 6 in which the blow-by gas 110 is freed from its oil droplets 107. The tubular body 2 comprises a wall 7 oriented perpendicularly to the direction of the flow. The wall 7 separates, upstream, the jet pump 5 and, downstream, the oil separator device 6. The wall 7 has an opening 14 that communicates the jet pump 5 and the separator device 6.

(12) As shown in the figures, the separator system 1 comprises a jet pump 5 adapted to increase the speed of the blow-by gas 110 before its introduction into the separator device 6.

(13) The objective is, to increase the oil decantation effect, by increasing the speed of the gas and, thus, the efficiency of the separator device 6.

(14) Referring to FIG. 2, the jet pump 5 operates by means of a propellant gas 113 which, in practice, comes from a branch-up made on the supercharging circuit (not represented) of the engine and which causes a gas to accelerate, namely the blow-by gas 110 which comes from the crankcase.

(15) The jet pump 5 comprises a tubular body 8 provided with a nozzle 9 at its end. The nozzle 9 opens into a conduit 10; the conduit 10 has a conical geometry and opens itself onto the oil separator device 6.

(16) In the example represented in the figures, the conduit 10 is integrally molded with the wall 7.

(17) Thus, the jet pump 5 comprises a conduit 10 adapted to receive the blow-by gas 110 coming from a crankcase through the inlet duct 3 and a nozzle 9 fed with a propellant gas 113 whose end opens into the conduit 10.

(18) One can notice the relatively simple structure of the jet pump 5 that, particularly, comprises only fixed components that can be easily inserted into the decantation system and this, without any significant extra cost.

(19) The nozzle 9 is, herein, connected to the supercharging circuit of the engine (not represented in the figures). The propellant gas 113, which may be branched on the supercharging circuit at a pressure in the range of 0 to 2 bars, conveys the blow-by gas 110 that circulates in the inlet duct 3. The blow-by gas 110 thus accelerated comes out of the conduit 10 with an increased speed. The acceleration effect created by the jet pump 5 is more specifically represented in FIG. 3.

(20) The system 1 may further comprise an aperture 12 closed by a movable flap 13. The aperture 12 is disposed between the inlet duct 3 and the separator device 6 and is placed in parallel with the conduit 10. In practice, there is provided a wall made of a plastic material which extends between the external surface of the conduit 10 and the wall 7 in which the aperture 12 is formed; thus, this forms a secondary passage parallel to the main passage formed by the conduit 10.

(21) The flap 13 may be a blade made of a plastic material which seals the aperture 12 by gravity.

(22) The aperture 12 is branched off the conduit 10. Thus, when the flap 13 is open, the blow-by gas 110 arriving through the inlet duct 3 benefits from a secondary passage towards the separator device 6; in this manner, the blow-by gas 110 is not forced to pass exclusively through the nozzle 10.

(23) In the embodiment of FIGS. 1 to 5, the body 8 of the jet pump 5 is provided with a check valve 15; the latter is formed by a shutter 16 pushed by a spring 17. It should be noted that the shutter 16 may have a geometry with a changing diameter so as to set the flow rate passing throughout the check valve 15 depending on the stroke of the shutter 16.

(24) The function of the separator device 6 is to purify the blow-by gas 110 which is therefore loaded with oil droplets to convert it into a purified gas 110 adapted to be reintroduced at the intake of the engine.

(25) The separator device 6 may have various shapes; in the illustrated embodiment of the invention, the separator device 6 is of a cylindrical type and acts by coalescence.

(26) Thus it comprises, in particular, a body 20 bearing on the wall 7 which is disposed opposite the conduit 10 and opposite the aperture 12 so that the separator device 6 can be fed with a flow coming from the conduit 10 or coming from the conduit 10 and the aperture 12 in a combined manner.

(27) FIGS. 7 and 8 show the opening 14 of the wall 7. The opening 14 has a semi-circular upper area 14a and a trapezoidal lower area 14b.

(28) The upper area 14a is located opposite the conduit 10 whereas the lower area 14b is located opposite the opening 12.

(29) The operating principle of the separator device 6 is to force the gas to take a radial path.

(30) In the embodiment illustrated in the figures, the separator device 6 has a valve 21 that is pushed by a spring 22; this configuration is represented in FIG. 7.

(31) When a blow-by gas is brought to exert a pressure on the valve 21, this one clears away, as shown in FIG. 8, and forces the gas to take a substantially radial trajectory. The shape of the outlet duct then changes the path of the gas according to the longitudinal axis. This results in a double inflection of the gas path, around the profile of the valve 21. Between these two inflections, the oil droplets, having a greater inertia than the gas alone, follow a more centrifugal path and hit a longitudinal wall of the separator device 2 which stops them, whereas the clean gas 111 continues its course in the outlet duct 4.

(32) The oil droplets 107 separated from the gas are collected to join the crankcase through a duct 24.

(33) In other embodiments, the decantation device 6 may implement baffles to de-oil the blow-by gas.

(34) The separator system 1 according to the invention may have several operating regimes which ensure a maximum efficiency.

(35) FIG. 1 illustrates the decantation system 1 at rest, that is to say a regime in which the separator device 2 is not requested, the valve 21 therefore bears against the wall 7.

(36) FIG. 2 shows the decantation system 1 in an operating regime in which the supercharging circuit supplies a propellant gas 113 which conveys the blow-by gas 110 and increases its speed. The propellant gas 113 pushes the valve 15 and comes into the body 8 and escapes through the nozzle 9. The valve 15 opens proportionally to the flow rate of the propellant gas 113 arriving from the supercharging circuit; thus, the propellant gas 113 is injected at the center of the conduit 10 and has a driving and acceleration effect on the blow-by gas 110 as shown more specifically in FIG. 3.

(37) However, there may occur depending on the engine operating conditions, a regime in which the supercharging gas is not available; this can be, for example, the case of an engine operating at high output for which the entire supercharging is requested to supply the cylinders which prevents from devoting a fraction of the supercharging gas to other functions. In this case, which is illustrated in FIG. 4, the valve 15 seals the jet pump 5 and the blow-by gas 110 can, depending on the amount and the pressure at which it comes into the decantation system 1, access the separator device 6 either by passing through the conduit 10 or by passing through the conduit 10 and the aperture 12 as represented in FIG. 4. The secondary passage that is formed by the aperture 12 adjacent to the conduit 10 allows limiting the pressure drop that is created by the jet pump 5 when the latter is not in action due to the unavailability of propellant gas.

(38) FIG. 5 shows an operating regime in which the jet pump 5 is in action and produces an acceleration of the incoming flow of the blow-by gas 110 and in which the flow of the blow-by gas 110 also passes throughout the secondary passage formed for the aperture 12.

(39) A variant of the invention may be considered in which, as illustrated in FIG. 6, the jet pump 5 is devoid of any valve. In this embodiment, the control of the propellant gas 113 may be carried out upstream of the jet pump 5 outside the strict perimeter of the decantation system 1. It is also possible to confer to the nozzle a particular geometry allowing managing the introduction of the propellant gas.

(40) The curves of FIG. 9 clearly illustrate the improvement of the spectral efficiency of oil separation. These curves show the efficiency as a function of the diameter of the oil droplets at different flow rates. The lowest efficiency (90% for droplets with a size larger than 1.5 μm) thus observed, is measured at a flow rate of 30 L/min whereas the highest efficiency (90% for droplets with a size larger than 0.6 μm) is measured for a flow rate of 90 L/min with a propellant gas pressure from 113 to 800 mbar.

(41) At a constant flow rate, for example 60 L/min, it is observed that the supply of propellant gas from 113 to 600 mbar allows considerably improving de-oiling for droplets of small diameters.

(42) These curves clearly demonstrate the effect produced by the acceleration of the blow-by gas 110 generated by the jet pump 5 on the quality of de-oiling. The arrow that appears overprinted on FIG. 9 shows the efficiency curves that approach 100% and droplets of smaller diameters as a function of the increase in the pressure of the propellant gas passing through the jet pump 5.

(43) The invention also provides a decantation device that creates a suction produced by the jet pump 5 allowing levelling or adding to the engine suction present in the duct 104. Thus, this allows creating a negative pressure in the inlet duct 3, this pressure not being negative without the use of the invention described above.

(44) Of course, the invention is not limited to the embodiments described above as non-limiting examples.