U.S. patent number 3,921,604 [Application Number 05/257,548] was granted by the patent office on 1975-11-25 for fuel injection apparatus for internal combustion engines.
This patent grant is currently assigned to Robert Bosch G.m.b.H.. Invention is credited to Heinz Links.
United States Patent |
3,921,604 |
Links |
November 25, 1975 |
Fuel injection apparatus for internal combustion engines
Abstract
There is described a pump-and-nozzle assembly which forms part
of a fuel injection apparatus serving an internal combustion
engine. The assembly includes a reciprocating pump piston driven by
a servo piston which is intermittently exposed to fuel pressure to
cause said pump piston to execute its delivery strokes. Between two
delivery strokes the pump work chamber is charged with pressurized
fuel through a throttle while the pump piston executes its return
stroke. The said throttle causes the charging period to be
substantially longer than the injection period. The admission of
pressurized fuel to the servo piston is controlled by the switching
positions of a valve plunger. The latter, in turn, is exposed to
pressurized fuel for periods controlled by a solenoid valve. Said
charging periods take place during the variable de-energized
periods of the solenoid valve. In this manner the injected fuel
quantities are determined.
Inventors: |
Links; Heinz (Stuttgart,
DT) |
Assignee: |
Robert Bosch G.m.b.H.
(Stuttgart, DT)
|
Family
ID: |
5809278 |
Appl.
No.: |
05/257,548 |
Filed: |
May 30, 1972 |
Foreign Application Priority Data
|
|
|
|
|
May 28, 1971 [DT] |
|
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2126736 |
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Current U.S.
Class: |
123/499;
123/458 |
Current CPC
Class: |
F02M
59/105 (20130101); F02M 57/025 (20130101) |
Current International
Class: |
F02M
57/02 (20060101); F02M 57/00 (20060101); F02M
59/10 (20060101); F02M 59/00 (20060101); F02m
039/00 (); F02b 003/00 () |
Field of
Search: |
;123/139E,139.10,139AC,32AE,139R |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
Primary Examiner: Myhre; Charles J.
Assistant Examiner: Cox; Ronald B.
Attorney, Agent or Firm: Greigg; Edwin E.
Claims
What is claimed is:
1. A fuel injection pump-and-nozzle assembly forming part of a fuel
injection apparatus serving an internal combustion engine, said
assembly being of the type that has (a) a pump piston executing
alternating delivery strokes and return or charging strokes, (b) a
pump work chamber bounded by said pump piston, (c) a servo piston
connected to said pump piston to drive the latter, said servo
piston having a diameter greater than that of said pump piston, (d)
a pressure source externally of said assembly for delivering fuel
under pressure to said assembly, (e) first supply conduit means
extending from said pressure source to said pump work chamber, (f)
a supply valve disposed in said first supply conduit means, (g) a
servo pressure chamber bounded by said servo piston, (h) second
supply conduit means extending from said pressure source to said
servo pressure chamber, (i) discharge conduit means extending from
said servo pressure chamber, (j) a housing including a bore, and
(k) a valve plunger disposed within said bore for controlling said
second supply conduit means and said discharge conduit means, said
valve plunger being adapted to assume a first switching position
for admitting pressurized fuel from said pressure source to said
servo pressure chamber for effecting said delivery strokes and a
second switching position for establishing communication between
said servo pressure chamber and said discharge conduit means for
effecting said return strokes, the improvement comprising,
A. a control pressure chamber formed within said bore and bounded
by said valve plunger,
B. third supply conduit means extending from said pressure source
to said control pressure chamber,
C. a solenoid valve disposed in and forming part of said third
supply conduit means at a location immediately adjacent said valve
plunger for intermittent energization in phase with the operation
of the engine, so that pressurized fuel is admitted through said
third supply conduit to said control chamber to move said valve
plunger from one of its switching positions to the other, and
D. a throttle member for affecting the speed of said return
strokes, said throttle member being disposed in said first supply
conduit means between said supply valve and said pressure source,
said throttle member including means defining a permanently set
flow passage section so dimensioned as to substantially lengthen
said charging period with respect to the injection period during
which fuel is injected into the engine from said pump work
chamber.
2. An improvement as defined in claim 1, wherein the maximum
permissible fuel injection quantity is determined by the maximum
stroke of said pump piston.
3. An improvement as defined in claim 1, wherein said flow passage
section of said throttle member is so dimensioned that for the
maximum permissible engine rpm each charging period during which
fuel is supplied to said work chamber from said pressure source
extends to the entire period between the terminal moment of the
injection period of one work cycle and the starting moment of the
injection period of the successive work cycle.
4. An improvement as defined in claim 1, wherein said solenoid
valve is an electromagnetically operated, pressure-equalized
3/2-way valve having a sphere as its movable valve member.
5. An improvement as defined in claim 1, including means for
varying the pressure of fuel prevailing in said second conduit
means as a function of at least one engine parameter.
6. An improvement as defined in claim 6, wherein said engine
parameter is the engine rpm.
7. An improvement as defined in claim 5, wherein said engine
parameter is the engine load.
8. An improvement as defined in claim 1, wherein said first, second
and third supply conduit means intersect said bore.
9. An improvement as defined in claim 1, wherein said bore is
disposed substantially transverse to the direction of
injection.
10. A fuel injection pump-and-nozzle assembly forming part of a
fuel injection apparatus serving an internal combustion engine,
said assembly being of the type that has (a) a pump piston
executing alternating delivery strokes and return or charging
strokes, (b) a pump work chamber bounded by said pump piston, (c) a
servo piston connected to said pump piston to drive the latter,
said servo piston having a diameter greater than that of said pump
piston, (d) a pressure source externally of said assembly for
delivering fuel under pressure to said assembly, (e) first supply
conduit means extending from said pressure source to said pump work
chamber, (f) a supply valve disposed in said first supply conduit
means, (g) a servo pressure chamber bounded by said servo piston,
(h) second supply conduit means extending from said pressure source
to said servo pressure chamber, said second supply conduit means
having a bore forming a part thereof which opens into said servo
pressure chamber, said servo piston having an extension rigidly
affixed to said servo piston and projecting axially outwardly from
that face of said servo piston that bounds said servo pressure
chamber, said extension projecting into said bore and defining
therewith a variable flow passage section, the magnitude of which
is a function of the momentary axial position of said servo piston,
(i) discharge conduit means extending from said servo pressure
chamber, (j) a housing including a bore, and (k) a valve plunger
disposed within said bore for controlling said second supply
conduit means and said discharge conduit means, said valve plunger
being adapted to assume a first switching position for admitting
pressurized fuel from said pressure source to said servo pressure
chamber for effecting said delivery strokes and a second switching
position for establishing communication between said servo pressure
chamber and said discharge conduit means for effecting said return
strokes, the improvement comprising:
A. a control pressure chamber formed within said bore and bounded
by said valve plunger;
B. third supply conduit means extending from said pressure source
to said control pressure chamber;
C. a solenoid valve disposed in and forming part of said third
supply conduit means at a location immediately adjacent said valve
plunger for intermittent energization in phase with the operation
of the engine, so that pressurized fuel is admitted through said
third supply conduit to said control chamber to move said valve
plunger from one of its switching positions to the other; and
D. a throttle member for affecting the speed of said return
strokes, said throttle member being disposed in said first supply
conduit means between said supply valve and said pressure source,
said throttle member including means defining a permanently set
flow passage section so dimensioned as to substantially lengthen
said charging period with respect to the injection period during
which fuel is injected into the engine from said pump work chamber.
Description
BACKGROUND OF THE INVENTION
This invention relates to a fuel injection apparatus for internal
combustion engines, particularly diesel engines, and is of the type
which has a separate pump-and-nozzle assembly for each engine
cylinder. Each pump-and-nozzle assembly has a pump piston that is
driven by a servo piston having a diameter larger than that of the
pump piston. The pump-and-nozzle assembly is coupled to a pressure
source which supplies both the pump work chamber and the servo
pressure chamber with pressurized fuel. In the conduit between the
pressure source and the pump work chamber -- bounded by the pump
piston -- there is situated a supply valve. One radial face of the
servo piston bounds the servo pressure chamber. A valve plunger
which is driven by pressurized fuel delivered by the pressure
source and controlled in phase with the internal combustion engine
by means of a control device, has a first switching position in
which it permits the flow of the fuel to the servo pressure chamber
and a second switching position in which it allows the fuel to be
discharged from the servo pressure chamber through a return or
discharge conduit. In this manner the valve plunger controls the
return stroke of the servo piston and thus determines the beginning
of the filling or charging stroke of the pump piston. In the second
switching position the speed of the charging stroke is affected by
a throttle.
In a known fuel injection apparatus of the aforeoutlined type (such
as disclosed, for example, in German Pat. No. 1,070,442), the
control device is constituted by a mechanically driven rotary
distributor which is common to all the pump-and-nozzle assemblies
and which controls the admission of the pressurized liquid to the
valve plunger with switching periods that are accurately and
permanently set by the structure of the distributor. Because of the
length of the fuel lines necessitated by the system itself (these
lengths, in addition, vary widely, particularly in large engines)
and because of the mechanical control of the switching periods, an
exact and rapid operation of the fuel injection apparatus required
for engines of recent design is very difficult to achieve. This
fuel injection apparatus furthermore operates in an rpm-dependent
manner since the switching periods of the distributor driven by the
engine change according to the engine rpm. Thus, the throttle
effect also changes in an rpm-dependent manner at the control
locations, so that a uniform injected fuel quantity in case of
rapidly changing rpm's can be ensured only with great difficulty,
if at all.
In another known fuel injection apparatus of similar structure
(such as disclosed, for example, in U.S. Pat. No. 2,598,528), the
valve plunger is mechanically connected with the armature of an
electromagnet and is driven thereby and controlled in phase with
the operation of the internal combustion engine. This fuel
injection apparatus has the disadvantage that the inertia of the
armature and the valve plunger make a sufficiently rapid and
accurate operation, particularly when used in fast-running diesel
engines, difficult if not impossible. Since the electromagnet, for
moving the valve plunger into both of its switching positions, has
to execute relatively large strokes, and because of the masses to
be moved has to be of relatively large volume, it is a further
disadvantage of this fuel injection apparatus that the
electromagnet has a relatively large delay of response and its
switching periods are too long.
OBJECT AND SUMMARY OF THE INVENTION
It is an object of the invention to provide an improved fuel
injection apparatus of the aforeoutlined type which is free from
the aforenoted disadvantages and which, particularly when used with
fast-running diesel engines, operates sufficiently rapidly and
accurately and in which the injected fuel quantity may be
maintained at exact values independently of the fast changing
engine rpm's.
Briefly stated, according to the invention, each pump-and-nozzle
assembly has, as a control device, a solenoid valve which is
disposed in the immediate vicinity of the valve plunger. By means
of varying those switching periods of the solenoid valve in which
the valve plunger, due to its position, causes the servo piston to
execute its return stroke, the length of the charging stroke and
thus the readied fuel injection quantity may be altered.
The invention will be better understood, as well as further objects
and advantages will become more apparent, from the ensuing detailed
specification of a preferred, although exemplary, embodiment taken
in conjunction with the drawing.
BRIEF DESCRIPTION OF THE DRAWING
FIG. 1 is a longitudinal sectional view of the pump-and-nozzle
assembly according to the preferred embodiment of the invention
showing the servo piston and the pump piston in their lower dead
center position;
FIG. 2 is a sectional view along line II--II of FIG. 1 showing the
servo piston and the pump piston in their upper dead center
position;
FIG. 3 is a schematic representation of the structure shown in
FIGS. 1 and 2 and including in addition, in symbolic
representation, associated components of the fuel injection
apparatus in a first switching position of the valve plunger at the
beginning of the delivery stroke; and
FIG. 4 is a diagram illustrating the injection quantity Q.sub.E as
a function of the injection, charging and control periods.
DESCRIPTION OF THE PREFERRED EMBODIMENT
Turning now to FIGS. 1 and 2, the pump-and-nozzle assembly 10 is
formed of three structural groups 11, 12 and 13 which are tightened
together to constitute a structural unit.
The first structural group 11 includes a housing 14 containing, in
a mounting bore 15 that extends normal to a transversal bore 16, an
electromagnetically operated 3/2-way valve 17 which serves as a
control device and which hereinafter will be referred to as the
solenoid valve 17. In the transversal bore 16 there is guided a
valve plunger 18, one end of which is exposed to the force of a
spring 19, while its other end is exposed to a hydraulic pressure
which prevails in a control pressure chamber 21 and which is
controlled by the solenoid valve 17.
The second structural group is a hydraulically-operated pump 12
which is controlled by the valve plunger 18 through a control bore
22 and which has a housing 23, a servo piston 24, a pump piston 25,
a throttle member 26 (FIG. 2) and a supply valve 27. The servo
piston 24, with one of its radial faces 28, bounds the lower
portion of a servo pressure chamber 29 while the upper portion of
the latter is bounded by a sleeve 31 containing the control bore
22.
The third structural group is formed of an injection nozzle 13
which is in axial alignment with the pump 12 and which has a spring
housing 32, an intermediate block member 33 and a nozzle body 34.
In the latter there is guided a nozzle needle 35, on which there is
inserted within the spring chamber 36 of the spring housing 32, a
spring seat disc 37 supporting a closing spring 38. The closing
spring 38 seeks to maintain the nozzle needle 35 in its closed
position and engages with its other end an insert 39, the
dimensions of which, together with the spring bias, determine in a
known manner the magnitude of the stroke of the nozzle needle 35. A
tightening nut 40 surrounds all components of the fuel injection
nozzle 13 and is threadedly in engagement with the housing 23 of
the pump 12.
The housing 14 of the first structural group 11 has, normal to the
longitudinal axis of the pump-and-nozzle assembly 10, a supply bore
41 (FIG. 2) to which there is coupled a supply conduit 43 carrying
fuel under a servo pressure p.sub.S from a pressure source which is
schematically shown in FIG. 3 and which will be discussed in more
detail hereinafter. The fuel is admitted from the fuel supply bore
41 to an annular chamber 46 in the wall of the transversal bore 16
and therefrom through a control conduit portion 47 to the solenoid
valve 17 and through a charging bore 48 and the throttle member 26
to the supply valve 27. When the latter is open which is the case
during the charging stroke of the pump, fuel may flow from a spring
chamber 49 of the supply valve 27 through a port 51 to the pump
work chamber 52. By means of serially arranged further conduits 53,
53a and 53b the pump work chamber 52 and the spring chamber 49 are
in a continuous communication with an annular chamber 54 in the
vicinity of the nozzle opening 55.
From a second annular chamber 56 provided in the wall of the
transversal bore 16, there extends a return bore 57 outwardly to
the upper face 58 of the housing 14. To the return bore 57 there is
coupled a return conduit 59 which leads to a fuel tank.
The flow passage section of the throttle member 26 threadedly
engaged in the charging bore 48 affects the supply speed of the
fuel to the supply valve 27 and thus to the pump work chamber 52.
Stated differently, the said flow passage section determines the
charging period t.sub.F of the pump-and-nozzle assembly 10. The
charging period t.sub.F is, by virtue of the throttle member 26,
substantially lengthened (for example, 18 fold) with respect to the
injection period t.sub.E and, accordingly, a correspondingly
greater accuracy in the metering of the injected fuel quantity Q is
achieved. By virtue of the lengthened charging period t.sub.F, even
very small injection quantities (smaller than 3 mm.sup.3 per
stroke) may be accurately controlled.
The solenoid valve 17 which is disposed in the bore 15 of the
housing 14 immediately adjacent the valve plunger 18 and which in
FIG. 1 is shown in section and in a simplified manner, is a known,
pressure-equalized 3/2-way valve actuated by an electromagnet 61
and having a valve housing 62 and, as its movable valve member, a
sphere 63. The latter engages, in its shown closed position, a
valve seat 64 and thus blocks fuel admission from the control
conduit portion 47 to a control conduit 65 leading to the control
pressure chamber 21. Simultaneously, the control conduit 65 and
thus the control pressure chamber 21 are, by means of an open
second valve seat 66 in communication with the return or discharge
conduit 59 through a bore 67 and a return bore 57 in the housing
14.
The electromagnet 61 has an armature 69 which is guided in the
valve housing 62 and which, urged by the force of a spring 71,
presses the sphere 63 against the valve seat 64 when the
electromagnet 61 is in a deenergized condition. To permit the use
of a spring 71 of moderate force, the solenoid valve 17 is
pressure-equalized by providing a channel 72 through which the
servo pressure p.sub.S prevailing in the control conduit portion 47
is communicated to a chamber 73 which is located behind the
armature 69 and which accommodates the spring 71. The faces on the
sphere 63 and the armature 69 which are exposed to the pressure of
the fuel are at least approximately of the same magnitude so that
the forces exerted on the sphere 63 in the opening and closing
directions are also at least approximately identical. For this
reason the spring 71 merely has to be strong enough to maintain the
sphere 63 at the valve seat 64.
The second, non-illustrated, open position of the solenoid valve 17
is achieved when the electromagnet 61 is energized, for example, by
means of an electronic control apparatus (shown only symbolically
in FIG. 3). In this manner the force of the spring 71 is overcome
by the electromagnet forces and the armature 69 is displaced. The
fuel then flows through the first valve seat 64 and presses the
sphere 63 against the second valve seat 66 so that the fuel may
then flow from the control conduit portion 47 through the first
valve seat 64 into the control chamber 21 where it drives the valve
plunger 18 against the force of the spring 19 to the right and
brings an annular groove 74 provided on the valve plunger 18 into
such a position that the annular chamber 46 which is under the
servo pressure p.sub.S will be connected with the control bore 22.
As a result, the fuel flows through the control bore 22 into the
servo pressure chamber 29. The servo piston 24 and the pump piston
25 are, for example, in case of the largest possible fuel injection
quantity, moved by the servo pressure from their position shown in
FIG. 2 (upper dead center) into their lower dead center position
illustrated in FIG. 1. During this displacement of the pistons 24,
25, fuel is delivered from the pump work chamber 52 through the
channel 51 (FIG. 2) and the conduits 53, 53a and 53b to the annular
chamber 54 and to the nozzle opening 55 of the fuel injection
nozzle 13 and thus fuel injection takes place.
The sections of the valve housing 62 which are exposed to different
large pressures are isolated from one another in the stepped
mounting bore 15 by means of sealing rings 76, 76a and 76b.
The use of an abovedescribed solenoid valve is particularly
advantageous, since the small mass of the moving components permits
an almost delay-free switching operation which is a desideratum for
a rapid and accurate operation of the solenoid valve.
The fuel which leaks through the nozzle needle 35 of the fuel
injection nozzle 13 and which accumulates in the spring chamber 36
of the spring housing 32 may, as indicated in FIG. 2, flow through
a conduit 77 and an adjoining conduit 78 to the return conduit 59,
since the conduit 78 merges into that portion of the bore 15 which
is upwardly and downwardly isolated by sealing rings 76 and 76a and
from which, as shown in FIG. 1, there extends the bore 67 to the
return bore 57.
The fuel leaking through the pistons 24 and 25 is collected in a
chamber bounded by an annular groove 79 (FIG. 2). Said chamber is
located in the zone of contact between the servo piston 24 and the
pump piston 25 and is in communication with the conduit 78. A check
valve 81 provided in the conduit 78 prevents the fuel from being
drawn back from the return conduit 59 and the conduit 78 during the
suction stroke of the servo piston 24 since in this manner the
downward motion of the servo piston 24 during the injection stroke
would be hindered.
In order to affect the course of the stroke speed of the pump
piston 25 (FIG. 1) during the delivery stroke and thus affect the
course of the fuel injection, the servo piston 24 driving the pump
piston 25 has a conical extension 82 protruding from its radial
face 28. The extension 82 projects into the control bore 22 and
defines there a flow passage section 83 which is variable in cross
section and which is dependent upon the stroke position H of the
servo piston 24. In this manner the stroke speed of the pump piston
25 and thus the course of the fuel injection may be varied. It is
also feasible to provide the pump piston 25 with a cylindrical
extension, in which case the control bore has a correspondingly
matching configuration.
In the lower dead center position of the pump piston 25 illustrated
in FIG. 1, for the depressurization of the fuel injection nozzle
13, the pump work chamber 52 is connected through a channel 85 in
the pump piston 25 with the annular chamber 86 which, in turn, is
coupled through a connecting bore 87 (FIG. 2) to the conduit 77. In
this manner a depressurization down to the pressure prevailing in
the return chamber 59 (practically 0 kg/cm.sup.2) may be achieved.
If it is desired to maintain a higher residual pressure in the pump
work chamber 52, the annular chamber 86, instead of being connected
with the conduit 77, may be connected with the charging bore 48, so
that in the pump work chamber 52 and in the fuel injection nozzle
13 there will remain a residual pressure which will equal the servo
pressure p.sub.S of the pressure source.
In the upper dead center position shown in FIG. 2, the servo piston
24, at the end of the charging stroke and at the beginning of the
delivery stroke, engages with its radial face 28 an abutment 88
which is formed by the radial face of a cylindrical extension 89 of
the sleeve 31 and which bounds from above the servo pressure
chamber 29. The length of the cylindrical extension 89 determines
the maximum stroke H.sub.max of the servo piston 24 and pump piston
25 and thus determines the maximum injection quantity Q.sub.max. By
proper setting of the stroke H.sub.max one may limit the greatest
injection quantity Q.sub.max to the maximum permissible full load
injection quantity, so that even in case of a defective control of
the fuel injection apparatus, a fuel quantity larger than the full
load quantity can never be injected. This feature ensures that the
maximum permissible injected fuel quantity cannot be exceeded. This
is particularly advantageous in diesel engines, in case the maximum
permissible injected fuel quantity is identical to the full load
fuel quantity. In this manner an emission, during excess fuel
injection, of uncombusted pollutants prohibited with ever
increasing severity by the clean air laws, is effectively
prevented.
In FIG. 3 the pump-and-nozzle assembly 10 is shown with the
associated and known components of the fuel injection apparatus in
a simplified manner. The pistons 24, 25 are in their upper dead
center position as shown in FIG. 2, whereas the solenoid valve 17
which is shown only symbolically, is in its open position in which
it connects the supply conduit 43 through the control conduit 65
(shown here in broken lines) with the control pressure chamber 21.
Consequently, the valve plunger 18 is moved against the force of
the spring 19 towards the right and its annular groove 74 connects
the supply conduit 43, 41 through the annular chamber 46 and the
control bore 22 with the servo pressure chamber 29. In this
switching position the pressure or injection stroke is initiated
which takes place until the pump piston 25 engages its lower
abutment 90 (FIG. 1). The supply conduit 43 is coupled to a
pressure source 91.
The pressure source 91 may be formed, as indicated in this example,
of a gear pump 93 which is driven by the internal combustion engine
92 and the output pressure of which may be maintained by means of a
pressure regulating valve 94 at the desired servo pressure, for
example, p.sub.S = 50 kg/cm.sup.2.
The servo pressure p.sub.S, by virtue of appropriate design of the
pressure regulating valve 94, may be regulated in an rpm and/or
load-dependent manner. The load-dependency may be achieved, for
example, in a known and not illustrated manner by changing the
spring bias as a function of the position of the accelerator pedal
or by turning the movable valve member which forms part of the
regulator valve 94 and which is provided with an oblique overflow
control edge.
In order to compensate for pressure fluctuations, the pressure
source 91 is provided with a pressure accumulator 95. The gear pump
93 draws fuel through a suction conduit 96 and a filter 97 from a
fuel tank 98 into which the fuel may flow back from the
pump-and-nozzle assembly 10 through the return conduit 59.
In case the fuel injection apparatus is used with a multicylinder
internal combustion engine, a plurality of pump-and-nozzle
assemblies are used which are coupled to the supply conduit 43 by
means of branches 43a, 43b and 43c and to the return or discharge
conduit 59 by means of branches 59a, 59b and 59c.
The control of the solenoid valve 17 is effected by means of a
known and only symbolically shown control apparatus 99 which
transmits the switching signals of variable length to the
electromagnet 61 of the solenoid valve 17.
In FIG. 4 in the lower portion of the diagram there is shown the
course of the stroke H of the pump piston 25 and thus, there is
illustrated the fuel injection quantity Q as a function of the
charging, injection and control periods t.sub.F, t.sub.E, and
t.sub.S, respectively. The greatest possible fuel injection
quantity Q.sub.max (the highest point on the curve A) is achieved
with a stroke H.sub.max. At an engine rpm of, for example, 4500,
the charging period t.sub.F for obtaining Q.sub.max is 25.2
milliseconds (ms). The associated injection period t.sub.E then
amounts to 1.5 ms. In case of an operation according to curve A,
these two periods add up to a cam angle of 360.degree., thus, to
one revolution of the cam shaft. In case of a four-cycle engine,
one cam shaft rotation corresponds to two crankshaft rotations,
that is, to a crank angle of 720.degree.. Then, the injection and
charging periods (t.sub.E + t.sub.F) add up to 26.7 ms which
corresponds to the cycle period T of one work cycle of the engine
in case of an engine rpm of 4500, since T = 2.60/4500 =
2.360/6.4500 = 26.7 .times. 10.sup..sup.-3 sec = 26.7 ms. The
equality T = t.sub.F + t.sub.E holds true only if moment t.sub.2 is
simultaneously the terminal moment of the injection period and the
beginning moment of the charging period.
The smaller injection quantity Q.sub.1 (partial load injection
quantity) is achieved with a stroke H.sub.1 and with an injection
course according to the curve B shown in broken line. The
associated charging period is t.sub.F1 and the corresponding
injection period is t.sub.E1. To the injection quantity Q.sub.1
there belongs a pump piston stroke H.sub.1. In FIG. 4 it is assumed
that for Q.sub.1 too the engine rpm is 4500, since a smaller engine
rpm would result in a correspondingly larger cycle period T (not
shown). Between the terminal moment of t.sub.E1 and the beginning
of t.sub.F1 there is a dwelling period t.sub.R1, during which the
pump piston 25 is in contact with its lower abutment, that is, it
is in its lower dead center position. In this case the cycle period
T is composed of periods t.sub.E1 + t.sub.R1 + t.sub.F1. The
switching periods of the electromagnet 61 of the solenoid valve 17
are illustrated by the solid line curve C for the largest possible
fuel injection quantity Q.sub.max and by the broken line curve D
for the partial load fuel quantity Q.sub.1. At C.sub.1 and D.sub.1
the solenoid valve 17 is in its closed position, whereas at C.sub.2
and D.sub.2 it is in its open position. The beginning and the end
of the energizing periods t.sub.S and t.sub.S1 determine the
beginning moment t.sub.1 of the injection period and the beginning
moment t.sub.2 and, respectively, t.sub.4 of the charging period.
The period between two energizing periods t.sub.S or t.sub.S1 in
which the electromagnet 61 is in a de-energized condition and thus,
the solenoid valve 17 is in its closed position C.sub.1 or D.sub.1,
is designated as de-energized period and identified at t.sub.A or
t.sub.A1. The moment of the termination of the injection period is
indicated at t.sub.2 and t.sub.3 ; it is affected basically only by
the prepared fuel injection quantity Q.sub.max or Q.sub.1, because
the other influencing magnitudes, such as the servo pressure
p.sub.S and the characteristic magnitudes of the injection nozzle
13 remain constant. If desired, the fuel servo pressure p.sub.S may
be varied, for example, in an rpm-dependent manner, for altering
the injection periods within limits.
OPERATION OF THE PREFERRED EMBODIMENT
In the description that follows, there will be set forth the mode
of operation of the pump-and-nozzle assembly 10 during one work
cycle T of the engine with reference to FIGS. 1-4.
Prior to the start of the injection of the full load quantity
Q.sub.max (FIGS. 2, 3 and curves A, C in FIG. 4) the servo piston
24 is, upon completion of a preceding charging stroke, in its upper
dead center position at H.sub.max where its radial face 28 engages
the upper abutment 88. At moment t.sub.1 the solenoid valve 17
switches from the closed position C.sub.1 into the open position
C.sub.2. The sphere 63 (FIG. 2) rapidly moves from the first valve
seat 64 to the second valve seat 66 and the fuel, which is
pressurized to the servo pressure p.sub.S by the pressure source
91, is admitted to the control pressure chamber 21 which causes the
valve plunger 18 to shift so that pressurized fuel is admitted to
the servo pressure chamber 29 (FIG. 3). At this time the fuel
exerts a pressure on the radial face 28 of the servo piston 24 and
drives the same, together with the pump piston 25, downwardly until
the latter, at moment t.sub.2, arrives in its lower dead center
position as shown in FIG. 1. During the course of the aforenoted
downward motion of the pump piston, it travels its maximum stroke
H.sub.max (FIG. 2) and delivers the fuel prevailing in the pump
work chamber 52 through the port 51 and conduits 53, 53a and 53b to
the nozzle opening 55 of the fuel injection nozzle 13. During this
step, in the pump work chamber 52 there is generated an injection
pressure p.sub.E of, for example, 300 kg/cm.sup.2, which
correspondingly to the transformation ratio between the servo
piston 24 and the pump piston 25, is greater than the servo
pressure p.sub.S of, for example, 50 kg/cm.sup.2. The closing
spring 38 of the fuel injection nozzle 13 is, in this example,
biased at 150 kg/cm.sup.2 of nozzle opening pressure. Thus, the
pressure p.sub.E of the fuel in the nozzle chamber 54 exerts a
pressure on the nozzle needle 35 overcoming the opening pressure of
the spring 38 and lifting the nozzle needle off its seat. In this
manner a fuel injection quantity Q.sub.max is injected in a known
manner by the pump piston 25.
At the terminal moment t.sub.2 of the injection period, the
solenoid valve 17, after an energizing period of t.sub.S, switches
back from its open position C.sub.2 into its closed position
C.sub.1. The sphere 63 now blocks the fuel supply to the control
pressure chamber 21 and depressurizes the same through the control
conduit 65, the presently open second valve seat 66, the bore 68
and the return conduit 59 which leads to the fuel tank 98. The
spring 19 moves the valve plunger 18 into its initial position
shown in FIG. 1, whereby the annular groove 74 establishes
communication between the servo pressure chamber 29 and the return
conduit 59. As a result, the pressure in the servo pressure chamber
29 and the pump work chamber 52 drops suddenly, the supply valve 27
opens, and the fuel at servo pressure p.sub.S moves the pump piston
25 and the servo piston 24 away from its lower dead center position
during a charging period t.sub.F, braked by the throttle member 26.
This charging step occurs between moments t.sub.2 and t.sub.1 in
the charging period t.sub.F until, at moment t.sub.1, the solenoid
valve 17 again switches into its already described switching
position C.sub.1, so that the successive work cycle T may begin. In
the above-described case, the charging period t.sub.F is identical
to the de-energized period t.sub.A of the solenoid valve 17.
The flow passage section of the throttle member 26 threadedly
engaged in the charging bore 48 affects the fuel supply speed of
the fuel to the pump work chamber 52 and thus determines the
charging period t.sub.F of the pump-and-nozzle assembly 10. By
virtue of the throttle member 26 the charging period t.sub.F is
substantially (for example, 18 fold) lengthened with respect to the
injection period t.sub.E and thus there is achieved a
correspondingly greater accuracy in the metering of the fuel
quantity Q. By virtue of the lengthened charging period t.sub.F
even very small (smaller than 3 mm.sup.3 /stroke) injection
quantities may be very accurately controlled.
An automatic safety control is achieved if the throttle bore of the
throttle member 26 is so designed that the charging period t.sub.F
at the maximum permissible rpm (n.sub.max) is extended to the
entire period between the terminal moment t.sub.2 of the injection
period of one work cycle T and the beginning moment t.sub.1 of the
injection period of the successive work cycle T, as it is the case
in an operation according to curve A. When the maximum rpm
n.sub.max is exceeded, an automatic reduction of the injection
quantity is effected because in case of an increasing rpm, the
charging period which is rpm-independent, is no longer sufficient
for a complete charging of the pump work chamber 52.
In case of delivery of the partial load injection quantity Q.sub.1
according to the curves B and D in FIG. 4, during a charging period
t.sub.F1 between moments t.sub.4 and t.sub.1, there is readied only
an injection quantity Q.sub.1 for a charging stroke H.sub.1. At
moment t.sub.1 when the solenoid valve is switched from D.sub.1 to
D.sub.2, the injection stroke begins and terminates at moment
t.sub.3. Until the end of the energizing period t.sub.S1 at
t.sub.4, the pump piston 25 remains in its lower dead center
position during a dwelling period t.sub.R1. As the solenoid valve
17 is switched from its open position D.sub.2 into its closed
position D.sub.1 at moment t.sub.4, the charging stroke starts
which lasts for the charging period t.sub.F1 until the moment
t.sub.1. At t.sub.1 the next injection begins and the
abovedescribed operation is repeated.
* * * * *