Information
-
Patent Grant
-
6792915
-
Patent Number
6,792,915
-
Date Filed
Monday, August 13, 200123 years ago
-
Date Issued
Tuesday, September 21, 200420 years ago
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Inventors
-
Original Assignees
-
Examiners
Agents
-
CPC
-
US Classifications
Field of Search
US
- 123 446
- 123 447
- 123 514
- 123 516
- 123 456
- 123 17917
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International Classifications
-
Abstract
The fuel supply apparatus for supplying fuel to an internal combustion engine has a fuel tank (2), a first fuel pump (6) that supplies fuel from the fuel tank to a fuel line (10), a second fuel pump (12) that supplies fuel from the fuel line (10) via a pressurized line to at least one fuel valve (16) and a fuel return line (22) that connects the fuel line (10) to the fuel tank for return of excess fuel. A shut off valve (30), which is closed at high temperatures, and a pressure regulator valve (26) are arranged hydraulically in series in the fuel return line (22). A fuel scavenger line (60) is provided, by which fuel at high temperatures is returned to the fuel tank (2). The fuel scavenger line (60) conducts the fuel back to the fuel tank (2), at least partially through the second fuel pump (12) and through a hydraulic resistance. Gas bubble formation is prevented by a high fuel supply pressure and by transfer of heat from the second fuel pump (12).
Description
BACKGROUND OF THE INVENTION
1. Field of the Invention
The present invention relates to a fuel supply apparatus for an internal combustion engine and, more particularly, to a fuel supply apparatus for supplying fuel to an internal combustion engine, comprising a fuel tank, a first fuel pump that supplies fuel from the fuel tank to a fuel line, a second fuel pump that supplies fuel from the fuel line via a pressurized line to at least one fuel valve that supplies fuel to the internal combustion engine at least indirectly and a fuel return line including a pressure regulator valve that connects the fuel line to the fuel tank.
2. Description of the Related Art
A fuel supply apparatus that supplies fuel by means of a first fuel pump from a fuel tank over a fuel line to a second fuel pump is known. The second fuel pump, for its part, supplies the fuel over a pressurized line to at least one fuel valve. Usually the number of the fuel valves is the same as the number of the cylinders in the internal combustion engine. The fuel supply apparatus can be constructed so that the fuel valves inject the fuel directly into the combustion chambers of the internal combustion engine. In operation of this fuel supply apparatus a higher pressure is required in the pressurized line leading to the fuel valves. After turning off the internal combustion engine it is desirable to mostly or entirely relieve the pressure in the fuel line and in the pressurized line to the internal combustion apparatus for safety reasons and because the fuel valves do not close entirely tightly.
The German disclosure document, DE 195 39 885 A1, describes a fuel supply apparatus, in which a valve device is provided for starting the internal combustion engine, so that the first fuel pump supplies the fuel with a high supply pressure to the fuel valves during the starting process. In many cases this high supply pressure is sufficient to start the internal combustion engine in the shortest possible time. Gas bubbles can be largely compressed in many cases between the first fuel pump and the second fuel pump by the elevated supply pressure so that a reliable operation of the internal combustion engine is guaranteed. In spite of that during the operation of the internal combustion engine at high temperatures and especially when the internal combustion engine is shut off at high temperatures, problems in both starting again and operation of the internal combustion engine occur at high temperatures. As has currently been established and described therein the gas bubbles of course are largely compressed at high pressure, however they are not sufficiently removed from the fuel supply apparatus. Furthermore it has currently been established that problems can occur at higher operating temperatures of the internal combustion engine because of the insufficient heat transfer from the fuel supply apparatus.
SUMMARY OF THE INVENTION
It is an object of the present invention to provide a fuel supply apparatus of the above-described kind that does not suffer from the above-described disadvantage.
This object and others, which will be made more apparent hereinafter, are attained in a fuel supply apparatus for supplying fuel to an internal combustion engine, comprising a fuel tank, a first fuel pump that supplies fuel from the fuel tank to a fuel line, a second fuel pump that supplies fuel from the fuel line via a pressurized line to at least one fuel valve so that the fuel at least indirectly reaches the internal combustion engine and a fuel return line including a pressure regulator valve that conducts fuel back from the fuel line to the fuel tank.
According to the invention a shut off valve is provided in the fuel return line hydraulically in series with the pressure regulator valve and a fuel scavenger line is provided that conducts the fuel back to the fuel tank, at least partially through the second fuel pump and through a hydraulic resistance.
Especially when there is a high thermal load on the fuel in the fuel supply apparatus, particularly when the second fuel pump is hot, also when the fuel is hot, the fuel supply apparatus according to the invention provides sufficient heat transfer from the fuel line so that no gas bubbles are generated in it. Fuel can be fed back to the fuel tank because of the scavenger line, which facilitates the advantageous heat transfer. Because of the closable shut off valve, fuel is returned over the scavenger line at high pressure in the fuel line between both fuel pumps, so that effective scavenging is guaranteed. Furthermore it is guaranteed that no gas bubbles or vapor bubbles occur at the inlet to the second fuel pump. Because of that feature a power loss, especially in the second fuel pump, and particularly at higher temperatures is reliably prevented. Reliable starting of the internal combustion engine is also guaranteed, especially at the higher temperatures.
Advantageous further embodiments of the invention are described and claimed in the appended dependent claims.
BRIEF DESCRIPTION OF THE DRAWING
The objects, features and advantages of the invention will now be illustrated in more detail with the aid of the following description of the preferred embodiments, with reference to the accompanying figures in which:
FIG. 1
is a schematic diagram of a first embodiment of a fuel supply apparatus according to the invention;
FIG. 2
is a schematic diagram of a second embodiment of a fuel supply apparatus according to the invention;
FIG. 3
is a schematic diagram of a third embodiment of a fuel supply apparatus according to the invention;
FIG. 4
is a cross-sectional view through a second fuel pump according to the invention;
FIG. 5
is a schematic diagram of a fourth embodiment of a fuel supply apparatus according to the invention;
FIG. 6
is a schematic diagram of a fifth embodiment of a fuel supply apparatus according to the invention;
FIG. 7
is a schematic diagram of a sixth embodiment of a fuel supply apparatus according to the invention;
FIG. 8
is a schematic diagram of a seventh embodiment of a fuel supply apparatus according to the invention;
FIG. 9
is a schematic diagram of an eighth embodiment of a fuel supply apparatus according to the invention;
FIG. 10
is a detailed schematic diagram of a portion of a fuel supply apparatus according to the invention;
FIG. 11
is a schematic diagram of a ninth embodiment of a fuel supply apparatus according to the invention; and
FIG. 12
is a schematic diagram of a tenth embodiment of a fuel supply apparatus according to the invention.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
The fuel supply apparatus according to the invention can be used for metering fuel to an internal combustion engine for various different types of internal combustion engines. It can be used with different methods of operation of an internal combustion engine. The internal combustion engine, for example, can be an Otto motor with fuel injection or with a carburetor and spark ignition. The engine can be provided with reciprocating pistons (reciprocating engine) or with a rotary piston (Wankel engine). The internal combustion engine can also be a hybrid motor. In this latter engine with stratified charge the fuel-air mixture is sufficiently enriched in the vicinity of the spark plug so that combustion occurs in an average mixture, but also in a strongly lean mixture, and reliable ignition is guaranteed.
Gas exchange to and from the combustion chambers or breathing of the internal combustion engine can occur, for example, according to a four-stroke or two-stroke method. Gas exchange valves (inlet valves and outlet valves) can be provided in a known manner to control the gas exchange or breathing of the internal combustion engine. The internal combustion engine can be constructed so that one or more fuel valves directly inject fuel into the combustion chamber or chambers of the internal combustion engine. The control of the power of the internal combustion engine preferably occurs by control of the rate of supply of fuel to the combustion chambers. The fuel valve or valves can also introduce the fuel to an inlet valve or valves of the combustion chamber. In this embodiment the air for combustion of the fuel is usually supplied to the combustion chamber via a throttle. The position of this throttle controls the power delivered by the engine.
The internal combustion engine, for example, has a cylinder with a piston, or it can be provided with several cylinders and with a corresponding number of pistons. A fuel injection valve is preferably provided for each cylinder.
So that the scope or extent of the disclosure is not unnecessarily wide, the following description of the preferred embodiments is limited to reciprocating engines with four cylinders, in which four fuel valves directly inject the fuel, usually gasoline, into the combustion chambers of the internal combustion engine. The fuel injection rate controls the power of the internal combustion engine. Charge stratification with fuel enrichment in the vicinity of the spark plug occurs during idle and lower loads. Outside of this range the mixture is very lean. During full load or higher loads uniform distribution between fuel and air in the combustion chambers is desired.
FIG. 1
shows a fuel tank
2
, a vacuum line
4
, a first fuel pump
6
, an overpressure valve
7
, an electric motor
8
, a fuel line
10
, a second fuel pump
12
, pressurized line
14
, four fuel valves
16
and a control unit
20
. The fuel valves
16
are often designated in professional circles as injector valves or injectors and are controlled by electrical control signals transmitted from the control unit
20
over electrical line e
2
.
The first fuel pump
6
has a pressurized side
6
h
and a drawing or vacuum side
6
n.
The second fuel pump
12
has a high pressure side
12
h
and a low pressure side
12
n.
The fuel line
10
leads from the pressurized side
6
h
of the first fuel pump
6
to the low pressure side
12
n
of the second fuel pump
12
. A return channel leads back to the fuel tank
2
from the high pressure side
6
h
of the first fuel pump
6
.
A fuel return line
22
branches from the fuel line
10
. Fuel from the fuel line
10
can be conducted back into the fuel tank
2
by means of the fuel return line
22
. A filter
24
is arranged in the fuel line
10
, between the first fuel pump
6
and the second fuel pump
12
.
A pressure regulator valve
26
and a shut off valve
30
are provided in the fuel return line
22
. The pressure regulator valve
26
and the shut off valve
30
are connected to act one after the other. That means that the pressure regulator valve
26
and the shut off valve
30
are connected in series with each other. The pressure regulator valve
26
and the valve device
30
can also be compactly embodied together in a common housing.
The shut off valve
30
has a first position
30
a
and a second position
30
b.
In the first position
30
a
fuel can flow from the fuel line
10
through the fuel return line
22
through the pressure regulator valve
26
into the fuel tank
2
. In this position the pressure regulator valve
26
directly determines the supply pressure of the fuel in the fuel line
10
. If the shut off valve
30
is in its second position
30
b,
fuel cannot flow directly from the fuel line
10
to the pressure regulator valve
26
.
The first fuel pump
6
is driven by an electric motor
8
. The first fuel pump
6
, overpressure valve
7
, electric motor
8
, filter
24
, pressure regulator valve
26
and shut off valve
30
are arranged in or near the fuel tank
2
. These parts are preferably arranged on the fuel tank
2
outside of it or within the fuel tank
2
.
The second fuel pump
12
is mechanically coupled with a drive shaft of symbolically indicated motor
32
by means of a mechanical transmitting means
12
m.
The camshaft of the internal combustion engine
32
functions as the drive shaft. Since the second fuel pump
12
is mechanically coupled to the drive shaft of the internal combustion engine, the second fuel pump operates according to the rotation speed of the drive shaft of the internal combustion engine
32
. Because the second fuel pump
12
is flanged closely to the housing of the internal combustion engine
32
, considerable heat is transferred from the internal combustion engine
32
to the second fuel pump
12
, which causes a comparatively great heat load on the fuel in the fuel tank
2
.
The pressurized line
14
leading from the second fuel pump
12
to the fuel valves
16
can for simplicity be divided into an entrance section
42
, a reservoir
44
and a plurality of distributor lines
46
. The respective fuel valves
16
are connected to the reservoir
44
by corresponding distributor lines
46
. The pressure sensor
48
is connected to the reservoir
44
and senses the pressure of the fuel in the pressurized line
14
. The pressure sensor
48
transmits an electrical sensor signal dependent on the magnitude of this pressure to the control unit
20
over electrical conductor e
1
.
A control valve
50
, which is controlled electrically by the control unit
20
via electrical line e
2
, is connected to the reservoir
44
of the pressurized line
14
. Fuel is conducted from the pressurized line
14
to the low pressure side
12
n
of the second fuel pump
12
by means of circulator line
52
. A hydraulic resistance element is arranged between the control valve
50
and the low pressure side
12
n.
The resistance element is a check valve
53
, which opens only in the direction to the fuel line
10
under a very low pressure difference.
The first fuel pump
6
, for example, can be a positive-displacement fuel pump driven by an electric motor
8
, which feeds a predetermined amount of fuel for each revolution. The pressure of the fuel on the high pressure side
6
h
of the first fuel pump
6
is subsequently designated as the supply pressure. The supply pressure in the fuel line
10
is determined by the pressure regulator valve
26
when the shut off valve is opened. The pressure regulator valve
26
is set, for example, at a pressure difference of 3 bar. Also the supply pressure in the fuel line
10
amounts to three bar (3 bar) when the shut off valve
30
is open.
A scavenger line
60
leads from the second fuel pump
12
to the fuel tank
2
. The scavenger line
60
is connected with the low pressure side
12
n
of the second fuel pump
12
within the pump housing
12
g,
as shown in FIG.
4
. The hydraulic resistance is formed by a first overflow valve
61
and a second overflow valve
62
. Branch point
63
is located in the circulator line
52
. The scavenger line
60
branches from the branch point
63
. In the advantageous embodiment shown in
FIG. 1
the scavenger line
60
opens into an opening
64
between the shut off valve
30
and the pressure regulator valve
26
in the fuel return line
22
. The first overflow valve
61
is adjusted to a comparatively low pressure difference, preferably 1 bar. Also the second overflow valve
62
is adjusted to a comparatively low pressure difference, preferably at 1 bar. Because the pressure differences of both overflow valves
61
,
62
can be adjusted to comparatively low values, a comparatively simple structure can be selected for the overflow valves, without large leakage resulting at the set pressure difference.
The first fuel pump
6
generally supplies somewhat more fuel to the fuel line
10
than is taken from the fuel line
10
by the second fuel pump
12
. In normal operation the excess fuel flows through the normally open shut off valve
30
and through the pressure regulator valve
26
, so that the supply pressure in the fuel line
10
adjusts itself based on the pressure difference in the pressure regulator valve
26
.
When temperature sensor
65
establishes that an especially high temperature has been reached, an appropriate signal is supplied to the control unit
20
over conductor e
4
. The control unit
20
then switches the shut off valve
30
to its second position
30
b
via electrical line e
5
, so that the direct connection of the fuel line
10
to the pressure regulator valve
26
is interrupted. With the shut off valve
30
closed, the excess fuel not taken from the fuel line
10
by the second fuel pump
12
flows through the pump housing
12
g
of the second fuel pump
12
, by the first fuel overflow valve
61
, through the second overflow valve
62
and through the pressure regulator valve
26
back into the fuel tank
2
. Because of that a supply pressure, which corresponds to the sum of the pressure differences of the valves
61
,
62
and
26
, results. The overpressure valve
7
, for example, is adjusted to a pressure, which is higher than the sum of the pressure differences at the valves
61
,
62
and
26
in the selected embodiment.
Because the scavenger line
60
leads through the pump housing
12
g
of the second fuel pump
12
, heat energy from the second fuel pump
12
can be conducted away by the fuel flowing through the scavenger line
60
, whereby an excessive temperature of the fuel in the region of the fuel line
10
and in the region of the second fuel pump
12
is avoided. Because of that feature it is guaranteed that the supply pressure in the fuel line
10
with the shut off valve
30
closed is higher than the supply pressure during normal operating conditions of the internal combustion engine
32
, so that a non-standard high temperature does not lead to gas bubbles in the fuel line
10
, whereby no decrease in efficiency of the second fuel pump
12
need be feared even at higher heat load. Because the increased supply pressure is set only at comparatively high temperature, also usually only for a comparatively short time interval, no noteworthy shortening of the service life of the comparatively economically manufactured first fuel pump
6
results.
Because the excess fuel quantity supplied by the second fuel pump
12
in the pressurized line
14
, which is not injected by the fuel valves
16
, passes through the control valve
50
from the reservoir
44
, over the circulator line
52
through the check valve
53
directly to the low pressure side
12
n
of the second fuel pump
12
, unnecessary routes for the circulation of the fuel are avoided and no heated fuel is guided back to the fuel tank
2
from the pressurized line
14
in normal operating conditions of the internal combustion engine, so that unnecessary heating of the fuel in the fuel tank
2
is avoided during normal operating conditions of the engine.
The fuel pump
12
has a pump housing
12
g
shown in the drawing with dashed lines. The overflow valves
61
,
62
, check valve
53
, branch point
63
and the sensor
65
are preferably contained within the pump housing
12
g.
The sensor
65
is, for example, a temperature gauge and it can, for example, be arranged directly in the pump housing
12
g
or in the vicinity of the pressurized line
14
. Instead of the sensor
65
, for example, also the water temperature of the cooling water of the internal combustion engine
32
can be ascertained to measure the temperature.
FIG. 2
shows an additional preferred embodiment of the fuel supply apparatus according to the invention.
In all figures for the following described embodiments the same, or similarly acting, parts are designated with the same reference characters. In so far as nothing to the contrary is mentioned and/or shown in the figures in regard to features shown and described in one of the figures, the same goes for the other embodiments shown in the other figures. In so far as nothing is said regarding a change in the description, the individual features of the separate embodiments are combinable with each other.
The scavenger line
60
in the embodiment shown in
FIG. 2
differs from the corresponding scavenger line
60
in the embodiment of FIG.
1
. The scavenger line
60
in the embodiment of
FIG. 2
leads directly from the second overflow valve
62
to the fuel tank
2
. In order to obtain a uniformly high feed pressure with shut-off valve
30
closed, as explained with the aid of
FIG. 1
, the pressure difference of the second overflow valve
62
is not set at 1 bar as in the first embodiment, but instead is set for example at 5 bar.
An intervening section of the scavenger line
60
between the first overflow valve
61
and the second overflow valve
62
is combined with an intervening section of the circulator line
52
between the control valve
50
and the check valve
53
in the embodiments shown in
FIGS. 1 and 2
. Because of this feature of this embodiment an effective scavenging of both the fuel line
10
and the housing
12
g
of the second fuel valve
12
takes place. The circulator line
52
thus provides both scavenging and heat transfer.
FIG. 3
shows an additional particularly advantageous preferred embodiment of the fuel supply apparatus according to the invention.
The fuel from the low pressure side
12
n
of the second fuel supply pump
12
reaches the fuel tank
2
through the scavenger line
60
and the pressure regulator valve
26
via an overflow valve
66
in the embodiment shown in FIG.
3
. The overflow valve
66
provides hydraulic resistance in the scavenger line
60
.
In contrast to the embodiment shown in
FIGS. 1 and 2
the scavenger line
60
downstream of the overflow valve
66
is not combined with or connected to the circulator line
52
. The advantage that fewer valves are required is attained because of that feature. In spite of that at last one indirect evacuation of the circulator line
52
is possible by means of the check valve
53
, the low pressure side
12
n
of the second fuel pump
12
and the scavenger line
60
with the overflow valve
66
in the embodiment shown in FIG.
3
.
In order to obtain the same pressure conditions in the embodiment shown in
FIG. 3
as in the embodiments shown in
FIGS. 1 and 2
, the pressure difference of the overflow valve
66
, for example, is set to 2 bar.
In principle the overflow valve
7
can be eliminated in the embodiments shown in
FIGS. 1
to
3
. However the overflow valve
7
is recommended in these embodiments as a protection against the eventual clogging of the filter
24
.
FIG. 4
is a cross-sectional view of the second fuel pump
12
.
The fuel pump
12
has at least one pump plunger
12
p.
Preferably the fuel pump
12
has three pump plungers, but only one is shown for simplicity in FIG.
4
. Fuel reaches the interior of the pump housing
12
g
via the fuel line
10
. The low pressure
12
n
and the at least one pump plunger
12
p
are located within the pump housing
12
g.
The pump plunger
12
p
is surrounded by fuel, which has the same supply pressure as in the fuel line
10
. The scavenger line
60
branches from the highest point of the interior of the housing
12
g
of the fuel pump
12
. The air collecting at the highest point in the pump housing
12
g
is conducted through the scavenger line
60
to the fuel tank
2
because of the location of the connection of the scavenger line to the housing
12
g.
FIG. 5
shows an additional particularly advantageous preferred embodiment of the fuel supply apparatus according to the invention.
A channel leading to the fuel tank
2
branches from the high pressure side
6
h
of the fuel pump
6
immediately downstream behind the first fuel pump
6
. The overflow valve
7
is arranged in this channel. The overflow valve
7
is, for example, set to 8 bar. The overflow valve
7
is still however located before the filter
24
in the flow direction, in order to guarantee that clogging of the filter
24
does not lead to an excessive pressure in the first fuel pump
6
.
The branch point
63
, from which the scavenger line
60
branches from the circulator line
53
, is located between the control valve
50
and the check valve
53
. Hydraulic resistance is provided in the scavenger line
60
. A throttle
70
provides the hydraulic resistance.
The check valve
53
has a compressed spring. The spring pressure of the check valve
53
is tuned to the flow resistance of the throttle
70
. The spring pressure is determined so that, when the shut off valve
30
is in its open position, a desired fuel flow rate from the circulator line
52
through the scavenger line
60
and the pressure regulator valve
26
to the fuel tank
2
is continuously provided.
When the shut off valve
30
is in its closed position
30
b,
excess fuel supplied by the first fuel pump
6
, but not delivered by the injector valves
16
, flows through the overpressure valve
7
into the fuel tank
2
. Also a part of the excess fuel flows through a throttle
70
and through the pressure regulator valve
26
to the fuel tank
2
. The pressure at the overpressure valve
7
is thus set so that it is higher than the pressure difference at the pressure regulator valve
26
and the fuel flowing through the scavenger line
60
also accumulates at the throttle
70
. Then with the shut off valve in its closed position the supply pressure in the fuel line
10
is clearly higher than the supply pressure occurring in normal operation with the shut off valve
30
in its open position. Gas bubbles occurring in the second fuel pump
12
and/or in the fuel line
10
are thus reliably compressed. A portion of the fuel is returned from the circulator line
52
to the fuel tank
2
. An additional transfer of undesirable heat energy generated in the fuel supply apparatus is obtained because of that feature. The relative portions of fuel flowing directly from the circulator line
52
to the low pressure side
12
n
of the second fuel pump
12
and flowing through the scavenger line
60
back to the fuel tank
12
can be controlled or adjusted by controlling the compression pressure of the spring in the check valve
53
.
In the embodiment shown in
FIG. 5
the throttle
70
provides that a certain portion of fuel, which can be selected according to the pre-compression of the spring in the check valve
53
, is also fed back from the circulator line
52
to the fuel tank
2
under normal operating conditions.
FIG. 6
shows an additional particularly advantageous preferred embodiment of the fuel supply apparatus according to the invention.
Deviating from the embodiment of
FIG. 5
the hydraulic resistance in the scavenger line
60
is provided by an overflow valve
72
arranged in the scavenger line
60
. The overflow valve
72
is set so that it opens when the pressure difference of 2 bar is reached. The check valve
53
is set so that it opens at a very low pressure difference. Because of these features in normal operation of the fuel supply unit, which means, when the shut off valve
30
is in its open position
30
a,
the supply pressure in the fuel line
10
is determined by the pressure regulator valve
26
. Then the fuel supplied by the second fuel pump
12
and not delivered by the fuel valves
16
flows a short way from the high pressure side
12
via the control valve
50
, through the circulator line
52
and through the check valve
53
to the low pressure side
12
n
of the second fuel pump
12
. The pre-tensioned overflow valve
72
provides that no fuel flows back from the circulator line
52
to the fuel tank
2
. Because of these features in normal operation of the fuel supply apparatus the temperature of the fuel in the fuel tank
2
is kept as low as possible.
In order to return fuel the shut off valve
30
is set in its closed position
30
b.
The supply pressure in the fuel line
10
then climbs until it exceeds the pressure at the overflow valve
7
and the predetermined pressure limit of the overflow valve
72
so that fuel flows from the circulator valve
52
, through the overflow valve
72
and through the pressure regulator
26
and into the fuel tank
2
.
FIG. 7
shows an additional particularly advantageous preferred embodiment of the fuel supply apparatus according to the invention.
An additional hydraulic resistance element is provided in the circulator line
52
in the embodiment symbolically represented in
FIG. 7
, which is not present in the embodiment shown in FIG.
6
. The additional hydraulic resistance element is a throttle
74
. The throttle
74
is arranged hydraulically in series with the check valve
53
. The throttle
74
can be considered as being either downstream or upstream of the check valve
53
. The throttle
74
and the check valve
53
are located downstream of the branch point
63
to the scavenger line
60
.
When a comparatively large amount of fuel is pumped into the circulator line
52
at higher rotation speeds of the internal combustion engine
32
, a back up pressure develops before the throttle
74
and, when this backup pressure is large enough to overcome the pre-tensioned overflow valve
72
, at least one portion of the fuel pumped by the second fuel pump
12
flows back into the fuel tank
2
. This is one purpose of the throttle
74
.
The embodiment shown in
FIG. 7
can be adjusted so that a portion of the fuel from the circulator line
52
flows back into the fuel tank
2
at high rotation speed of the internal combustion engine
32
. Otherwise a higher supply pressure must be provided in the fuel line
10
by switching the shut off valve
30
into its closed position
30
b.
This has the advantage that at higher rotation speeds of the engine
32
, which inevitably and frequently occur during travel, the first fuel pump
6
need not be operated against high feed pressure, which increases the service life. In the embodiment according to
FIG. 7
the shut off valve
30
must be shut off for only a short time interval, for example for return of fuel during the starting process of the internal combustion engine
32
. This means that the fuel pump
6
operates only rarely against a high supply pressure, which substantially extends the service life of the fuel pump
6
.
FIG. 8
shows an additional particularly advantageous preferred embodiment of the fuel supply apparatus according to the invention.
The throttle
74
and the check valve
53
are located hydraulically downstream of the branch point
63
in the circulator line
52
, from which the scavenger line
60
branches in the embodiment shown in FIG.
8
. The throttle
74
and the non-return valve
53
are hydraulically connected in parallel to each other. The check valve
53
is biased with a closing spring. The check valve
53
opens when a sufficiently large pressure difference is present at the throttle
74
for opening of the check valve. The check valve
53
also limits the pressure drop across the throttle
74
.
An additional hydraulic resistance is provided in the scavenger line
60
hydraulically downstream of the branch point
63
. The additional hydraulic resistance is provided by a throttle
76
provided in the scavenger line
60
. The throttle
76
is hydraulically in series with the overflow valve
72
either upstream or downstream of it.
The proportion of fuel flowing through the scavenger line
60
to the fuel tank
2
and flowing through the circulator line
52
to the low pressure side
12
n
of the fuel pump
12
can be adjusted by tuning or adjustment of the throttles
74
and
76
and the pre-tension in the check valve
53
and the overflow valve
72
. The rotation speed value at which a part of the fuel flowing through the circulator line
52
flows back to the fuel tank
2
via the scavenger line
60
can also be preset.
FIG. 9
shows an additional particularly advantageous preferred embodiment of the fuel supply apparatus according to the invention.
FIG. 10
is a detailed view of part of the embodiments of the fuel supply apparatus shown in
FIGS. 9
,
11
and
12
.
In the embodiments shown in
FIGS. 9 and 10
the second fuel pump
12
has a pump plunger
12
p,
an inlet side check valve
12
a,
an outlet-side check valve
12
b,
a compression chamber
12
k
and a control valve
50
′.
A pressure damper
78
is connected to the fuel line
10
. The pressure damper
78
is preferably located inside the pump housing
12
g.
A hydraulic resistance element is arranged in the circulator line
52
′. The resistance element is a check valve
80
, which opens in the direction of the fuel line
10
. The circulator line
52
′ opens into the fuel line
10
at an opening
82
. The circulator line
52
′ runs from the compression chamber
12
k,
through the control valve
50
′, by the branch point
63
′, through the check valve
80
and through the opening
82
into the fuel line
10
. The circulator line
52
′ extends a short way directly inside the pump housing
12
g.
The control valve
50
′ has an open switch position
50
′
a
and a closed position
50
′
b.
The scavenger line
60
branches off at the branch point
63
′ between the control valve
50
′ and the check valve
80
. The scavenger line
60
has a hydraulic resistance downstream of the branch point
63
′. The hydraulic resistance is a throttle
84
.
A connection line
86
leads from the fuel line
10
to the region of the compression chamber
12
k
in which the plunger
12
p
travels. The pressure transmitted over the connection line
86
provides a reduction of the friction in the region of the chamber
12
k
in which the plunger
12
p
travels.
A leakage or bleeder line
88
is connected to the region of the compression chamber
12
k
remote from the end of the pump plunger
12
p.
A second shut off valve
90
is arranged in the fuel return line
22
downstream of the pressure regulator valve
26
. The second shut off valve
90
has an open position
90
a
and a closed position
90
b.
The leakage line
88
opens into the return line
22
between the pressure regulator valve
26
and the second shut off valve
90
at opening
92
.
During a suction stroke, which means, during the downward travel of the pump plunger
12
p
so that the compression chamber
12
k
increases in size, the fuel flows from the fuel line
10
through the inlet side check valve
12
a
into the compression chamber
12
k.
During a compression stroke, which means, during the upward travel of the pump plunger
12
p
so that the compression chamber
12
k
decreases in size, the pump piston
12
p
forces the fuel from the compression chamber
12
k
through the outlet side check valve
12
b
into the reservoir
44
of the pressurized line
14
, in so far as control valve
50
′ is in its closed position
50
′
b.
It is possible to control the control valve
50
′ so that it is in the open position
50
′
a
during a part of the compression stroke of the pump plunger
12
p.
While the control valve
50
′ stands in its open position
50
′
a
during a portion of the compression stroke, the fuel is fed through the open control valve
50
′, through the circulator line
52
′ and through the check valve
80
into the fuel line
10
, because of the normally high pressure in the fuel line
10
. The throttle
84
and the pre-tensioned check valve
80
can be adjusted with respect to each other, so that, when the control valve
50
′ is open during the compression stroke, a part of the fuel flowing through the circulator line
52
′ flows back through the scavenger line
60
and through the pressure regulator valve
26
into the fuel tank
2
.
The fuel flow rate into the pressurized line
14
from the second fuel pump
12
can be controlled by suitable switching of the control valve
50
′ according to the stroke of the pump plunger
12
p.
The fuel flow rate from the second fuel pump
12
into the pressurized line
14
can be controlled by controlling the control valve
50
′ so that the desired high pressure exists in the pressurized line
14
, which can be sensed by the pressure sensor
48
. The control valve
50
′ is controlled according to the pressure determined by the pressure sensor
48
.
An additional return line
94
connects to the fuel line
10
from the pressurized line
14
with the reservoir
44
. A pressure-limiting valve
96
is provided in the return line
94
. The pressure-limiting valve
96
is provided so that, even if an error occurs, for example due to an error in the control valve
50
′, no dangerous excess pressure can exist in the fuel line
14
. The pressure-limiting valve
96
can be controlled electrically, and indeed so that the pressure in the reservoir
44
can be quickly reduced according to the operating conditions.
When the shut off valve
30
is in its open position
30
a,
only a very reduced portion of the fuel flowing through the circulator line
52
′ flows through the scavenger line
60
into the fuel tank
2
as the throttle
84
and the pressure difference of the check valve
80
are adjusted to each other. The usually greater fuel flow flows through the check valve
80
in the fuel line
10
, where the pressure damper
78
is provided, in order to provide a buffer reservoir for in-flowing pulsating fuel.
When the shut off valve
30
is put in its closed position
30
b,
the overpressure valve
7
determines the supply pressure in the fuel line
10
. Because the overpressure valve
7
is set at a higher pressure than the pressure regulator valve
26
, the supply pressure with the shut off valve
30
closed is higher than with it open. With the shut off valve
30
in its closed position the fuel flow flowing from the compression chamber
12
k
through the control valve
50
′ largely flows through the throttle
84
, through the scavenger line
60
into the fuel line
22
and from there into the fuel tank
2
.
When the internal combustion engine
32
is operating the second shut off valve
90
is in its open position
90
a.
If the internal combustion engine
32
is turned off, the second shut off valve
90
is switched into its closed position, in order to avoid a temporary pressure drop in the low pressure system by way of the gap between the pump plunger
12
p
and the pump housing
12
g.
FIG. 11
shows an additional particularly advantageous preferred embodiment of the fuel supply apparatus according to the invention.
In the embodiment shown in
FIG. 11
the leakage or bleeder line
88
leads to the fuel tank
2
without co-use of the return line
22
, which differs from the embodiment shown in FIG.
9
. The shut off valve
90
is provided in the leakage line
88
. Because only a very reduced fuel flow rate through the leakage line
88
occurs, which is many times less than that through the return line
22
, so that a very small and very light valve is suitable for use as the shut off valve
90
.
FIG. 12
shows a further particularly advantageous preferred embodiment of the fuel supply apparatus according to the invention.
In the embodiment shown in
FIG. 12
the shut off valve
30
is downstream of the pressure regulator valve
26
, in contrast to other embodiments. The scavenger line
60
branches from the fuel line
10
at the branch point
63
″. The leakage or bleeder line
88
open to the scavenger line
60
downstream of the throttle
84
. The opening
64
, at which the scavenger line
60
opens into the return line
21
, is between the pressure regulator valve
26
and the shut off valve
30
.
The control valve
50
′ is connected with the fuel line
10
by means of the circulator line
52
′ and the opening
82
. During the suction stroke of the fuel pump
10
the fuel can flow not only through inlet side check valve
12
a
with the control valve
50
′ open, but also through the control valve
50
′ into the compression chamber
12
k.
During the compression stroke of the fuel pump
12
the control valve
50
′ is kept in the closed position
50
′
b
until the desired pressure is reached in the pressurized line
14
.
Two dashed lines
98
r
and
98
f
are shown in FIG.
12
. Usually parts found to the left of the dashed line
98
r
are found in the rear of the motor vehicle. Parts found to the right of the dashed line
98
f
are generally found in the front region of the motor vehicle.
Usually in order to connect the parts arranged in the front region of the vehicle with those in the rear region, comparatively long fuel lines are installed. For that reason the number of lines connecting the parts in the front with those in the rear are kept as small as possible. As can be seen from
FIG. 12
, the fuel line
10
and the scavenger line
60
are sufficient for connection of the parts in the front region with those in the rear region in this preferred embodiment.
In order to make restarting the internal combustion engine
32
easier, when the internal combustion engine
32
is shut off at comparatively high temperature, the following procedure is suggested: When the internal combustion engine
32
is shut off, keep the first fuel pump
6
in operation with the shut off valve
30
still open for a predetermined time interval, which can depend on the temperature. Heat energy collected from the region of the second fuel pump
12
and from the region of the fuel line
10
and the pressure damper
78
is transferred over the scavenger line
60
to the fuel tank
2
. This avoids the danger of undesirable gas bubble formation in the fuel tank
2
. Furthermore it can be provided that, after the rinsing or scavenging of the fuel line
10
, shortly prior to shutting off the electrically operated fuel pump
6
, the shut off valve
30
is switched into its closed position
30
b.
For that reason the pressure in the fuel line
10
and in the pressure damper
78
climbs to the supply pressure determined by the overflow valve
7
, which is higher than the supply pressure determined by the pressure regulator valve
26
with the shut off valve
30
open. Because of that a higher pressure exists in the pressure damper
78
with the internal combustion engine shut off, which makes subsequent starting of the engine
32
easier, even at higher temperatures.
The embodiments shown in
FIGS. 1
to
8
are especially used, when the second fuel pump
12
has several pump plungers
12
p,
usually three pump plungers
12
p.
The embodiments illustrated in
FIGS. 9
to
12
are especially used when the second fuel pump
12
has a single pump plunger
12
p.
The disclosure in German Patent Application 100 39 773.8 of Aug. 16, 2000 is incorporated here by reference. This German Patent Application describes the invention described hereinabove and claimed in the claims appended hereinbelow and provides the basis for a claim of priority for the instant invention under 35 U.S.C. 119.
While the invention has been illustrated and described as embodied in a fuel supply apparatus for an internal combustion engine, it is not intended to be limited to the details shown, since various modifications and changes may be made without departing in any way from the spirit of the present invention.
Without further analysis, the foregoing will so fully reveal the gist of the present invention that others can, by applying current knowledge, readily adapt it for various applications without omitting features that, from the standpoint of prior art, fairly constitute essential characteristics of the generic or specific aspects of this invention.
What is claimed is new and is set forth in the following appended claims.
Claims
- 1. A fuel supply apparatus for supplying fuel to an internal combustion engine, said fuel supply apparatus comprisingat least one fuel valve (16) for introducing the fuel into the internal combustion engine; a fuel tank (2); a fuel line (10); a first fuel pump (6) for supplying the fuel from the fuel tank (2) to the fuel line (10); a second fuel pump (12) for supplying the fuel from the fuel line (10) via a pressurized line (14,42,44) to said at least one fuel valve (16) so that the fuel is introduced into the internal combustion engine at least indirectly; a fuel return line (22) connecting the fuel line (10) to the fuel tank (2) for fuel return; a pressure regulator valve (26) arranged in the fuel return line (22); a shut off valve (30) arranged in the fuel return line (22) so as to be hydraulically in series with the pressure regulator valve (28); and a fuel scavenger line (60) for conducting the fuel back to the fuel tank (2) at least partially through the second fuel pump (12) and through a hydraulic resistance means; wherein the fuel scavenger line (60) opens into the fuel return line (22) hydraulically between the shut off valve (30) and the pressure regulator valve (26).
- 2. The fuel supply apparatus as defined in claim 1, further comprising means for controlling the shut off valve (30) according to a temperature.
- 3. The fuel supply apparatus as defined in claim 1, wherein the second fuel pump (12) has a pump housing (12g) and the fuel scavenger line (60) extends through said pump housing (12g).
- 4. The fuel supply apparatus as defined in claim 3, wherein the second fuel pump (12) has a low pressure side (12n) and the fuel scavenger line (60) branches from the pump housing (12g) at a highest position thereof on said low pressure side (12n) of the second fuel pump.
- 5. The fuel supply apparatus as defined in claim 1, further comprising an overpressure valve (7) connected in parallel hydraulically to the pressure regulator valve (26).
- 6. The fuel supply apparatus as defined in claim 1, wherein the hydraulic resistance means comprises a throttle (70, 76, 84) having a flow-through resistance depending on the fluid flow flowing therethrough.
- 7. The fuel supply apparatus as defined in claim 1, wherein the hydraulic resistance means comprises a valve (61, 62, 68, 72) that opens depending on a pressure.
- 8. A fuel supply apparatus for supplying fuel to an internal combustion engine, said fuel supply apparatus comprisingat least one fuel valve (16) for introducing the fuel into the internal combustion engine; a fuel tank (2); a fuel line (10); a first fuel pump (6) for supplying the fuel from the fuel tank (2) to the fuel line (10); a second fuel pump (12) for supplying the fuel from the fuel line (10) via a pressurized line (14,42,44) to said at least one fuel valve (16) so that the fuel is introduced into the internal combustion engine at least indirectly; a fuel return line (22) connecting the fuel line (10) to the fuel tank (2) for fuel return; a pressure regulator valve (26) arranged in the fuel return line (22); a shut off Valve (30) arranged in the fuel return line (22) so as to be hydraulically in series with the pressure regulator valve (26); a fuel scavenger line (60) for conducting the fuel back to the fuel tank (2) at least partially through the second fuel pump (12) and through a hydraulic resistance means; and a circulator line (52,52′) connecting the pressurized line (14, 42, 44) to the fuel line (10) via a control valve (50,50′), said scavenger line (60) branching from the circulator line (52,52′).
- 9. The fuel supply apparatus as defined in claim 8, further comprising means for controlling the shut off valve (30) according to a temperature.
- 10. The fuel supply apparatus as defined in claim 8, the second fuel pump (12) has a pump housing (12g) and the fuel scavenger line (60) extends through said pump housing (12g).
- 11. The fuel supply apparatus as defined in claim 10, wherein the second fuel pump (12) has a low pressure side (12n) and the fuel scavenger line (60) branches from the pump housing (12g) at a highest position thereof on said low pressure aide (12n) of the second fuel pump.
- 12. The fuel supply apparatus as defined in claim 8, wherein the hydraulic resistance means comprises a throttle (70, 76, 84) having a flow-through resistance depending on the fluid flow flowing therethrough.
- 13. The fuel supply apparatus as defined in claim 8, wherein the hydraulic resistance means comprises a valve (61, 62, 66, 72) that opens depending on a pressure.
- 14. The fuel supply apparatus as defined in claim 8, further comprising an overpressure valve (7) connected in parallel hydraulically to the pressure regulator valve (26).
- 15. The fuel supply apparatus as defined in claim 8, wherein the circulator line (52,52′) is connected to the fuel line (10) by means of a hydraulic resistance element (53,74,80).
- 16. The fuel supply apparatus as defined in claim 8, wherein the circulator line (52,52′) is connected to the fuel line (10) by means of a check valve (53,80).
- 17. The fuel supply apparatus as defined in claim 16, further comprising a throttle (74) connected in parallel hydraulically to the check valve.
- 18. The fuel supply apparatus as defined in claim 8, wherein the second fuel pump (12) has a compression chamber (12k) and the circulator line (52′) extends from the compression chamber (12k).
- 19. A fuel supply apparatus for supplying fuel to an internal combustion engine, said fuel supply apparatus comprisingat least one fuel valve (16) for introducing the fuel into the internal combustion engine; a fuel tank (2); a fuel line (10); a first fuel pump (6) for supplying the fuel from the fuel tank (2) to the fuel line (10); a second fuel pump (12) for supplying the fuel from the fuel line (10) via a pressurized line (14,42,44) to said at least one fuel valve (16) so that the fuel is introduced into the internal combustion engine at least indirectly; a fuel return line (22) connecting the fuel line (10) to the fuel tank (2) for fuel return; a pressure regulator valve (26) arranged in the fuel return line (22); a shut off valve (30) arranged in the fuel return line (22) so as to be hydraulically in series with the pressure regulator valve (26); a fuel scavenger line (60) for conducting the fuel back to the fuel tank (2) at least partially through the second fuel pump (12) and through a hydraulic resistance means; and a leakage line (88) connecting the second fuel pump (12) to the fuel tank (2).
- 20. The fuel supply apparatus as define in claim 19, wherein the leakage line (88) opens into the return line (22) upstream of the shut off valve (30).
- 21. The fuel supply apparatus as defined in claim 19, further comprising means for controlling the shut off valve (30) according to a temperature.
- 22. The fuel supply apparatus as defined in claim 19, wherein the second fuel pump (12) has a pump housing (12g) and the fuel scavenger line (60) extends through said pump housing (12g).
- 23. The fuel supply apparatus as defined in claim 22, wherein the second fuel pump (12) has a low pressure side (12n) and the fuel scavenger line (60) branches from the pump housing (12g) at a highest position thereof on said low pressure side (12n) of the second fuel pump.
- 24. The fuel supply apparatus as defined in claim 19, further comprising an overpressure valve (7) connected in parallel hydraulically to the pressure regulator valve (26).
- 25. The fuel supply apparatus as defined in claim 19, wherein the hydraulic resistance means comprises a throttle (70, 76, 84) having a flow-through resistance depending on the fluid flow flowing therethrough.
Priority Claims (1)
Number |
Date |
Country |
Kind |
100 39 773 |
Aug 2000 |
DE |
|
US Referenced Citations (8)
Foreign Referenced Citations (3)
Number |
Date |
Country |
195 39 885 |
Nov 1996 |
DE |
198 18 421 |
Oct 1999 |
DE |
0 837 239 |
Feb 2002 |
EP |