[0001] The invention relates to a fuel supply system for a combustion engine. Furthermore,
the invention relates to a method for delivering fuel to a fuel injector of a combustion
engine.
[0002] Conventional fuel supply systems in vehicles comprise a high-pressure fuel pump that
is connected to a high-pressure rail. The fuel rail is hydraulically connected a multitude
of fuel injectors. The high-pressure fuel pump conventionally is driven by the camshaft
of the combustion engine of the vehicle. Accordingly, the fuel pressure is only generated
when the combustion engine is running, which is critical in particular during engine
cranking. Conventionally, the fuel pressure is also a function of the revolutions
per minute of the combustion engine because of the coupling of the high-pressure fuel
pump with the camshaft of the combustion engine. Furthermore, the fuel injectors are
all hydraulically coupled to one common high-pressure rail. Therefore, pressure waves
are transmitted between the fuel injectors.
[0003] A further aspect of the conventional system is that the components such as the fuel
pumps or the common fuel rail are relatively expensive components because they must
handle high-pressure fuel and be properly sealed.
[0004] Additional engine management requirements like stop/start are look for a quick pressure
build inside the injector to allow a quick injection to restart the engine. Also,
engine cranking at low temperature requires high-pressure operating conditions to
reduce engine emissions.
[0005] It is desirable to create a fuel supply system for a combustion engine that supplies
the fuel reliably. Furthermore, it is desirable to create a method for delivering
fuel to a fuel injector that works reliably. It is furthermore desirable that the
system is cost-efficient.
[0006] According to one embodiment of the invention, the fuel supply system for a combustion
engine comprises a multitude of fuel injectors for providing fuel to the combustion
engine. The fuel supply system further comprises a multitude of fuel pumps. Each fuel
pump of the multitude of fuel pumps is hydraulically coupled with one fuel injector
for providing fuel to the respective fuel injector. The respective fuel pumps each
comprise an electromagnetic or piezoelectric actuator for driving the respective fuel
pump.
[0007] Each fuel pump delivers fuel to one single injector. Since each fuel pump provides
fuel to only one fuel injector, the fuel injectors are hydraulically independent from
each other downstream the fuel pumps. Therefore, no pressure waves are generated that
impact other fuel injectors. Furthermore, since the fuel pumps each comprise an electromagnetic
or piezoelectric actuator, they are cost-effective. Each fuel pump is arranged to
provide the fuel with a pressure of about 50 to 200 bar. Furthermore, due to the coupling
of one fuel pump to one single fuel injector, there is no need for a common high-pressure
rail that is coupled to a multitude of fuel injectors.
[0008] According to two further aspects, the fuel pumps each are hydraulically directly
coupled to the respective fuel injector. Thereby, high-pressure sealings are avoided
and the system is reliable.
[0009] According to further aspects, each fuel pump is electrically coupled with an engine
control unit for controlling the system. Each fuel pump is controllable by the engine
control unit independent of the combustion engine. Furthermore, each fuel pump is
controllable by the engine control unit independent of the other fuel pumps. Therefore,
pressured fuel is provided by the fuel pumps for the fuel injectors reliably especially
during engine cranking. Quick pressure build inside the fuel injector is realized
and accordingly quick operation conditions to reduce engine emissions, especially
in engine management requirements like stop/start. The fuel pressure is available
and independent from the engine revolutions per minute. The fuel pressure is fitted
to the actual demand. No higher pressure than actually demanded is needed to correctly
operate the combustion engine such as in conventional systems. Stop/start operating
mode and low temperature cranking do not require engine rotating to build up the fuel
pressure.
[0010] According to one embodiment of the invention, a method for delivering fuel to a fuel
injector of a combustion engine comprises a controlling of a pump to suck in fuel
into a pump chamber when a fuel injector that is hydraulically coupled to the pump
is in a closed state. The method further comprises a controlling of the fuel injector
in an open state as to inject the fuel of the fuel chamber into a combustion chamber
of the combustion engine. The fuel out of the pump chamber is injected out of the
pump chamber only when the fuel is injected into a combustion chamber via the fuel
injector.
[0011] Fuel is efficiently provided to the combustion chamber via the fuel injector. The
pressurized fuel is only provided when needed. There is no need for redundant pressure
as in conventional systems.
[0012] According to further aspects, one sucking in and one injecting is performed by one
injection into the combustion chamber.
[0013] Reference will now be made in detail to the preferred embodiments, examples of which
are illustrated in the accompanying drawings. Elements of the same design and function
that appear in different drawings are identified by the same reference signs.
- Figure 1
- schematically shows a fuel supply system according to an embodiment,
- Figure 2
- schematically shows a fuel supply system according to a further embodiment.
[0014] Figure 1 schematically shows a fuel supply system 100. The fuel supply system 100
comprises a combustion engine 101. The combustion engine 101 is an internal combustion
engine of a vehicle, in particular a diesel gasoline combustion engine.
[0015] The system 100 further comprises a fuel reservoir 118 in which fuel 120 is stored.
In particular, the fuel is diesel gasoline. The fuel reservoir 118 is hydraulically
coupled via a pipe 117 to a multitude of fuel pumps 110, 111, 112, and 113. The fuel
pumps are electrically driven by an electronic actuator. The electronic actuator is
arranged to move a piston of the fuel pump in response to an electrical signal received
by the fuel pump. The movement of the piston of the fuel pump forced by the electric
actuator delivers fuel out of the reservoir 118 to the respective fuel injector. In
particular the electronic actuator is an electromagnetic actuator. The electromagnetic
actuator comprises a solenoid that interacts with the piston of the fuel pump. According
to further embodiments, the electronic actuator is a piezoelectric actuator.
[0016] The fuel pumps each are hydraulically connected to one single fuel injector 106,
107, 108, and 109. The fuel injectors are arranged to inject fuel into combustion
chambers 102, 103, 104, and 105 of the combustion engine 101.
[0017] The system 100 further comprises a low pressure pump 114 that is hydraulically arranged
upstream the fuel pumps 110 to 113 and that provides fuel out of the fuel reservoir
118 to the fuel pumps 110 to 113. Furthermore, an on/off valve 119 is arranged at
the pipe 117. An inlet valve 116 is arranged upstream of each fuel pump 110 to 113.
[0018] The system 100 further comprises an engine control unit 115 for controlling the system.
The engine controlling unit 115 is electrically coupled to each of the fuel pumps
110 to 113 and to each of the fuel injectors 106 to 109. The engine control unit is
further coupled to the on/off valve 119.
[0019] The engine control unit 115 is arranged to control the fuel pumps 110 to 113 to deliver
fuel out of the fuel reservoir 118 to the fuel injectors 106 to 109. The engine control
unit 115 is further arranged to control the fuel injectors between a closed state
and an open state. In the closed state, the fuel injectors prevent fuel from being
injected into the combustion chambers 102 to 105 of the combustion engine 101. In
the open state, fuel provided by the fuel pumps 110 to 113 is injected into the combustion
chambers via the fuel injectors 106 to 109.
[0020] The system 100 comprises as much fuel injectors as combustion chambers, for example
four combustions chambers and four fuel injectors. The system 100 comprises as much
fuel pumps as fuel injectors, for example four fuel pumps and four fuel injectors.
According to further embodiments, the system 100 comprises more than four fuel injectors,
combustion chambers and fuel pumps respectively, such as six fuel injectors, combustion
chambers and fuel pumps respectively. According to further embodiments, the system
100 comprises less than four fuel injectors, combustion chambers and fuel pumps respectively,
such as two fuel injectors, combustion chambers and fuel pumps respectively.
[0021] One fuel pump 110 delivers fuel to exactly one fuel injector. Downstream the fuel
pumps, the fuel injectors 106 to 109 are hydraulically independent from each other.
Upstream of each fuel pump, the inlet valve 116 is arranged. There are as many inlet
valves 116 as fuel pumps 110 to 113. The inlet valve 116 is a one-way valve and prevents
fuel from returning in the direction to the fuel reservoir 118.
[0022] During operation, the engine control unit 115 controls the valve 119 to open. Fuel
is delivered out of the fuel reservoir 118 to the fuel pumps 110 to 113 by the low
pressure pump 114 via the valve 119, the pipe 117, and the respective valves 116.
[0023] The engine control unit 115 controls the fuel pump 110 to suck in fuel only when
the respective fuel injector 106 is in its closed state. After sucking in fuel into
a pump chamber of the fuel pump 110, the fuel is provided under pressure in the pump
chamber for being injected into the combustion chamber 102. The pump 110 does not
eject the fuel out of the pump chamber as long as the fuel injector 106 is in its
closed state.
[0024] When the engine control unit 115 controls the fuel injector 106 to open, the fuel
is ejected under pressure out of the pump chamber and injected into the combustion
chamber 102 via the fuel injector 106. Afterwards, the engine control unit 115 sets
the fuel injector 106 again in its closed state and controls the pump 110 to suck
in fuel.
[0025] There is only one sucking in and only one ejecting of fuel out of the pump 110 per
one injection of fuel into the combustion chamber 102 via the fuel injector 106. Per
one opening of the fuel injector 106 there is one ejecting of the fuel out of the
pump chamber of the pump 110.
[0026] The functionality of the combination of the fuel pump 110, the fuel injector 106
and the combustion chamber 102 is transferable to the further combinations of the
respective fuel pumps with the respective fuel injectors and combustion chambers,
for example the combination of fuel pump 111, the fuel injector 107 and the combustion
chamber 103.
[0027] Since each fuel pump 110 to 113 provides fuel to only one fuel injector 106 to 109
respectively, the fuel injectors 106 to 109 are hydraulically independent from each
other downstream the fuel pumps 110 to 113. Therefore, no pressure waves are generated
that impact other fuel injectors. Furthermore, since the fuel pumps each comprise
an electromagnetic or piezoelectric actuator, they are cost-effective. Each fuel pump
110 to 113 is arranged to provide the fuel with a pressure of about 50 to 200 bar.
Furthermore, due to the coupling of one fuel pump to one single fuel injector, there
is no need for a common high-pressure rail that is coupled to a multitude of fuel
injectors.
[0028] Figure 2 schematically shows the system 100 of Figure 1 according to a further embodiment.
In contrast to the embodiment of Figure 1, according to the embodiment of Figure 2,
the pumps 110 to 113 are hydraulically coupled to the respective fuel injectors 106
to 109 via respective fuel pipes 121.
[0029] The system 100 according to the exemplary embodiments of Figure 1 and Figure 2 allows
having the fuel pressure on demand and not only when the combustion engine 101 is
running. Therefore, engine cranking is reliable because fuel pressure is readily available
to allow proper storing conditions without turning the engine. This operation condition
also supports a reliable stop/start function of the engine. The common high-pressure
fuel rail is no longer required and the system 100 has a reduced number of components
compared to conventional fuel supply systems. No fuel return line from the fuel pump
to the fuel reservoir 118 is required. Since each fuel pump is responsible to supply
high-pressure fuel to exactly one fuel injector, there are no or less pressure pulsations
transmitted between the fuel pumps 110 to 113 and the fuel injectors 106 to 109. There
is no influence from one fuel injector to the other fuel injectors. No pressure waves
are transmitted between the fuel injectors due to any injection event.
[0030] The system 100 is reliable especially when there are multiple injections of fuel
into one combustion chamber during one engine cycle. Since the fuel pumps 110 to 113
each are electrically driven, there is no longer a need for providing an overpressure
of 30% of additional injector P-Max performance as in conventional systems with a
common fuel high-pressure rail. By the fuel pumps according to the system 100, there
is the fuel provided at the pressure needed without a redundant additional pressure
for balancing pressure pulsations. If the system 100 includes the ballistic operating
condition function, the complete flow range could be obtained with one pressure value
only.
1. Fuel supply system for a combustion engine (101), comprising:
- a multitude of fuel injectors (106, 107, 108, 109) for providing fuel to the combustion
engine (101),
- a multitude of fuel pumps (110, 111, 112, 113), each fuel pump of the multitude
of fuel pumps (110, 111, 112, 113) being hydraulically coupled with one fuel injector
(106, 107, 108, 109) for providing fuel to the respective fuel injector (106, 107,
108, 109), wherein the respective fuel pumps (110, 111, 112, 113) each comprise an
electromagnetic or piezoelectric actuator for driving the respective fuel pump (110,
111, 112, 113).
2. System according to claim 1, wherein the fuel pumps (110, 111, 112, 113) each are
hydraulically directly coupled to the respective fuel injector (110, 111, 112, 113).
3. System according to claim 1, wherein the fuel pumps (110, 111, 112, 113) each are
hydraulically coupled to the respective fuel injector (110, 111, 112, 113) via a fuel
pipe (121).
4. System according to one of claims 1 to 3, comprising a low pressure pump (114) for
delivering fuel out of a fuel reservoir (118) to the multitude of fuel pumps (110,
111, 112, 113) being arranged upstream of the multitude of fuel pumps (110, 111, 112,
113).
5. System according to one of claims 1 to 4, wherein each of the fuel pumps (110, 111,
112, 113) is electrically coupled with an engine control unit (115) for controlling
the system and is controllable by the engine control unit (115) independent of the
combustion engine (101).
6. System according to one of claims 1 to 5, with each fuel injector of the multitude
of fuel injectors (106, 107, 108, 109) being attached to one combustion chamber of
a multitude of combustion chambers (102, 103, 104, 105) of the combustion engine (101).
7. Method for delivering fuel to a fuel injector (106, 107, 108, 109) of a combustion
engine (101), comprising:
- controlling a pump (110) to suck in fuel into a pump chamber only when the fuel
injector (106) that is hydraulically coupled to the pump (110) is in a closed state;
- controlling the fuel injector (106) to move to an open state as to inject the fuel
of the pump chamber into a combustion chamber (102) of the combustion engine (101),
wherein the fuel out of the pump chamber is ejected out of the pump chamber only when
the fuel is injected into a combustion chamber (102) via the fuel injector (106).
8. Method according to claim 7, wherein one sucking in and one ejecting is performed
per one injection into the combustion chamber (102, 103, 104, 105).