TECHNICAL FIELD
[0001] The present invention relates generally to a fuel injector and a protection mean
preventing soot deposit on its nozzle.
BACKGROUND OF THE INVENTION
[0002] A direct injection engine has adopted a configuration in which a fuel multi-port
injector is mounted into a mounting port in a cylinder head, and fuel is injected
directly into a cylinder from a nozzle at the tip of this fuel injector. After the
injection, the nozzle closes as a pintle inside the body of the injector axially translates
and abuts against the inner face of the nozzle. A minor quantity of liquid fuel remains
captured in the continuous volume defined by the injection ports connected to the
volume, known as the sac volume, which is inside the injector under the extremity
of the pintle. In the chamber motions of gas occurs in the chamber resulting from
pressure differences between various zones of the chamber. The nozzle is then laterally
hit by some gas. Pictorially, one could say the nozzle has a luv side, hit by the
burned gas, and an opposite lee side. Consequently the liquid fuel present in the
ports opening on the luv side is pushed back in toward the sac volume and, consequently,
some unburned liquid fuel exits from the ports opening on the lee side, said fuel
settling on the nozzle. This fuel oxidises in an oxygen-poor environment leaving some
amounts of soot clinging to the nozzle. With the multitude of such events the soot
then accumulates and forms a deposit layer on the nozzle which, in turn allows more
fuel to be deposited in there. This accumulation of soot goes against an optimum operation
mode of the engine.
SUMMARY OF THE INVENTION
[0003] The present invention aims at solving the above mentioned problem. For this purpose,
it is proposed a protection mean for the nozzle of a multi-port fuel injector axially
arranged in the mounting bore of the cylinder head of a direct injection combustion
engine. The bore opens in a combustion chamber, the tip point of the injector being
its nozzle set to deliver pressurized fuel in the combustion chamber. The protection
mean axially extends beyond the nozzle to prevent said nozzle from being in direct
contact with lateral gas motions created by pressure differences occurring inside
the combustion chamber.
[0004] Particularly, the protection mean is a shielding wall extending inside the combustion
chamber and providing a protection to the nozzle of the injector. The shielding wall
is a cylindrical tube arranged around the nozzle. The cylindrical tube may have a
circular section.
[0005] The protection mean can be a standalone component arranged and fixed to the cylinder
head for instance in the mounting bore, or fixed to the injector.
[0006] Also, the protection mean can be integral with the injector body and can extend beyond
the nozzle in order to surround it and protect it.
[0007] Furthermore, the protection mean may be integral with the cylinder head extending
inside the combustion chamber so that when the injector is arranged in the mounting
bore, the protection mean surrounds and protects its nozzle.
[0008] The protection axially extends beyond the tip point of the injector by a distance
0.1 to 5 mm. I a preferred embodiment the extension is limited to 2 to 3 mm.
[0009] Alternatively, the injector can be entirely arranged inside the mounting bore, the
protection mean being the final section of the bore which axially extends beyond the
nozzle into the combustion chamber.
[0010] The invention is also related to a fuel injector for a direct injection combustion
engine, the injector comprising a protection mean for its nozzle from being in direct
contact with lateral gas motions created by pressure differences occurring inside
the combustion chamber. The protection mean is as previously described.
[0011] The invention is further related to an internal combustion engine provided with a
fuel injector which nozzle is protected by a protection mean as previously described.
BRIEF DESCRIPTION OF THE DRAWINGS
[0012] The present invention is now described by way of example with reference to the accompanying
drawings in which:
- Figure 1 is a partial cross-section view showing schematically the arrangement of
an injector in a cylinder head according to the invention;
- Figure 2 is an alternative arrangement as figure 1.
- Figure 3 is a magnified detail of the nozzle of the injector of Figures 1 or 2.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
[0013] As per the figures, an in-cylinder type gasoline engine 10 is provided with an in-cylinder
multi-port fuel injector 12 according to a preferred embodiment of the present invention.
[0014] An internal combustion engine (gasoline engine) 10 is mainly composed of a cylinder
block (not shown) and a cylinder head 14. The cylinder head 14 has a mounting bore
16 which extends into a combustion chamber 18 along a main axis X.
[0015] In the following description, the main axis X will be orientated vertically from
the bottom to the top, which corresponds to the orientation of the figures, without
limiting purpose.
[0016] It has to be noted that the figures show only the lower half portion of the injector
12.
[0017] The fuel injector body 20 is axially inserted in the mounting bore 16, the tip portion
22 of the fuel injector 12, which comprises a nozzle 24, extending toward the combustion
chamber 18. Inside its body 20, the fuel injector 12 comprises a pintle 26 which is
axially reciprocally movable in order to control opening and closing of the nozzle
24.
[0018] According to the embodiment shown, the tip portion 22 of the injector has a tubular
shape closed at its lower end by a transversal wall 28 that axially deflects toward
the chamber 18 in a conical shape 30. The deflection 30 is provided with a plurality
of ports 32 enabling the pressurized fuel to be expelled from the inside of the injector
body 20 to the combustion chamber 18.
[0019] The pintle 26 has a spherical extremity 34 that closes the nozzle 24 by abutting
against the inner face of the deflection 30 along a circular closed line 36 set above
the ports 32. As detailed on Figure 3, when the nozzle 24 is closed, a volume defined
by the ports 32 and a sac volume 38 keeps captured a small quantity of liquid fuel.
The sac volume 38 is defined as the small volume which is below the spherical extremity
34 and the inner tip of the deflection 30. Alternative geometries of the pintle and
deflection exist and can benefit from the present invention.
[0020] In a preferred embodiment sketched in Figure 1, the injector body 20 axially extends
beyond the nozzle 24 in a tubular cylinder 40 that surrounds the nozzle 24. It is
known that the combustion chamber 18 has zones of different pressures and, the pressure
differences generate lateral gas motion in the chamber 18 symbolized on the Figures
1 and 2 by the arrow A. The cylinder 40 provides a protection mean for the nozzle
24 so that it is not in direct contact with said lateral gas motion A. The nozzle
40 is substantially flush with the inner face of the combustion chamber 18. The protection
mean 40 extends inside de combustion chamber 18 on a distance D that can be up to
5 mm. In a preferred embodiment the distance D is from 2 to 3 mm. According to the
preferred embodiment just described, the protection mean 40 is integral to the injector
body 20.
[0021] In an alternative embodiment, the protection mean 40 is a standalone component fixed
in the wall of the chamber 18, for instance partially inserted in the mounting bore
and partially extending out in the chamber. In another alternative embodiment, the
mean is integral to the cylinder head and arranged so that when the injector is set,
the protection mean protects the nozzle.
[0022] Whatever preceding choice is made, the protection mean 40 previously described as
a cylinder tube can be given other shapes according to the in-cylinder design and
to the resulting gas motions. For instance the portion extending in the combustion
chamber 18 may be a portion of cylinder or a simple flat wall protecting just one
side of the injector. This may be sufficient to protect the nozzle 24 from being in
direct contact with said lateral gas motion F.
[0023] Another protection mean 40 for the nozzle 40 may be provided by the mounting bore
16 itself. In this alternative, the fuel injector 12 is arranged back inside the bore
16 leaving free a final section 42 of the bore, section extending from the tip of
the injector 22 to the opening of the bore 16 in the combustion chamber 18.
1. Protection mean (40) for the nozzle (24) of a multi-port fuel injector (12) axially
(X) arranged in the mounting bore (16) of the cylinder head of a direct injection
combustion engine (10), the bore (16) opening in a combustion chamber (18), the tip
point (22) of the injector (12) being its nozzle (24) set to deliver pressurized fuel
in the combustion chamber (18) wherein the protection mean (40) axially extends beyond
the nozzle (24) to prevent said nozzle (24) from being in direct contact with lateral
gas motions (A) created by pressure differences occurring inside the combustion chamber
(16).
2. Protection mean (40) as set in the preceding claim wherein the mean (40) is a shielding
wall (40) extending inside the combustion chamber (18) and providing a protection
to the nozzle (24) of the injector (12).
3. Protection mean (40) as set in claim 2 wherein the shielding wall (40) is a cylindrical
tube arranged around the nozzle (24).
4. Protection mean (40) as set in claim 3 wherein the cylindrical tube has a circular
section.
5. Protection mean (40) as set in any of the preceding claim wherein the mean (40) is
a standalone component arranged and fixed to the cylinder head for instance in the
mounting bore (16), or fixed to the injector (12).
6. Protection mean (40) as set in any of the claim 1 to 4 wherein the mean is integral
with the injector body (20) and extends beyond the nozzle (24) in order to surround
it and protect it.
7. Protection mean (40) as set in any of the claim 1 to 4 wherein the mean is integral
with the cylinder head extending inside the combustion chamber (18) so that when the
injector (12) is arranged in the mounting bore (16), the protection mean (40) surrounds
and protects its nozzle (24).
8. Protection mean (40) as set in any of the preceding claim wherein the mean axially
extends beyond the tip point (22) of the injector (12) by a distance (D) of 0.1 to
5 mm.
9. Protection mean (40) as set in claim 1 wherein the injector (12) is entirely arranged
inside the mounting bore (16), said mean being the final section (42) of the bore
(16) which axially extends beyond the nozzle (24) into the combustion chamber (18).
10. Fuel injector (12) for a direct injection combustion engine (10) comprising a protection
mean (40) for its nozzle (24) from being in direct contact with lateral gas motions
(A) created by pressure differences occurring inside the combustion chamber (16),
the protection mean (40) being as set in any of the preceding claim.
11. Internal combustion engine (10) provided with a fuel injector (12) which nozzle (24)
is protected by a protection mean (40) as set in any of the claims 1 to 9.