U.S. patent number 3,677,236 [Application Number 05/070,038] was granted by the patent office on 1972-07-18 for fuel-injection devices for mixture-aspiring internal-combustion engines.
This patent grant is currently assigned to The Plessey Company Limited. Invention is credited to Norman Moss.
United States Patent |
3,677,236 |
Moss |
July 18, 1972 |
FUEL-INJECTION DEVICES FOR MIXTURE-ASPIRING INTERNAL-COMBUSTION
ENGINES
Abstract
To control the rate of fuel injection into the induction pipe of
a combustion engine, a transistor switch is arranged to vary the
length of each energization of a periodically energized ultrasonic
transducer which produces fuel atomization by longitudinally
vibrating the open outlet end of a fuel nozzle which leads into the
induction pipe and in which the fuel pressure is kept in balance
with the air pressure in the induction pipe.
Inventors: |
Moss; Norman (Ilford,
EN) |
Assignee: |
The Plessey Company Limited
(Ilford, EN)
|
Family
ID: |
34227892 |
Appl.
No.: |
05/070,038 |
Filed: |
September 8, 1970 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
Issue Date |
|
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727976 |
May 9, 1968 |
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Current U.S.
Class: |
123/491; 123/493;
123/478; 261/DIG.48 |
Current CPC
Class: |
F02D
41/30 (20130101); F02M 27/08 (20130101); F02M
69/041 (20130101); F02D 2700/0266 (20130101); F02D
41/2096 (20130101); Y10S 261/48 (20130101) |
Current International
Class: |
F02M
27/08 (20060101); F02M 69/04 (20060101); F02D
41/30 (20060101); F02M 27/00 (20060101); F02D
41/20 (20060101); F02m 051/06 () |
Field of
Search: |
;123/32EA,32AE
;261/DIG.48 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Goodridge; Laurence M.
Assistant Examiner: Flint; Cort
Parent Case Text
This application is a continuation-in-part of application, Ser. No.
727,976 filed May 9, 1968, abandoned.
Claims
What I claim is:
1. A valveless device for injecting liquid fuel into an
air-induction line conveying a flow of combustion air to a
mixture-aspiring combustion engine, comprising a low-resistance
injection nozzle having an open-ended outlet portion leading into
the air-induction line, means for supplying liquid fuel to said
nozzle and for automatically maintaining the fuel pressure in the
open end of said outlet in balance with the pressure of the
adjacent air, an ultrasonic transducer which when energized
produces ultrasonic vibrations of the outlet portion of the nozzle
in its longitudinal direction to atomize and inject fuel from said
nozzle into the flow of combustion air in the air-induction line,
first control means for periodically initiating energization of
said transducer, further control means associated therewith, for
terminating each period of such energization, and automatic means
for variably controlling the length of each such period in
accordance with operating data of the engine.
2. A fuel-injection device as claimed in claim 1 for a
reciprocating-piston engine, wherein said first control means are
arranged to operate near the commencement of each induction stroke
of each cylinder, and wherein said further control means are
arranged to operate at a later point of said stroke whose cyclic
spacing from said first point is arranged to vary in proportion to
the product of engine speed and the amount of fuel required per
induction stroke.
3. A fuel-injection device as claimed in claim 2, wherein the means
for variably determining the period of energization of the
transducer comprise an engine-driven distributor-switch device in
which a rotary-contact wiper co-operates with a control contact
whose angular setting is arranged to vary in proportion to the
engine speed and to a function of induction-line pressure to
determine one of the terminal points of the transducer-energization
period, subsidiary means being provided which normally prevent the
length of the energization period from falling below a
predetermined minimum.
4. A device as claimed in claim 3, wherein an element arranged to
co-operate with the wiper to determine the other of said terminal
points, is adjustable from a normal position in a direction
opposite to the displacement of the control element from said
minimum position.
5. A device as claimed in claim 1, which includes an automatic
device preventing operation of the transducer until the engine
speed reaches a predetermined value.
6. A device as claimed in claim 1, which includes means operable to
increase the length of each energization period of the transducer
in order to facilitate the starting of the engine from a cold
condition.
Description
This invention relates to mixture-aspiring internal combustion
engines and has for an object to provide an improved fuel-injection
system for engines of the kind specified which lends itself readily
to variation, independently of the operation of any valves, of the
rate of fuel injection, and particularly in a reciprocating engine
to variation of the quantity of fuel injected during each induction
stroke of each cylinder, in combination with good atomization of
the injected fuel.
According to the present invention fuel is injected into the stream
of combustion air by means of an open-ended nozzle in which
normally fuel is maintained in pressure balance with the pressure
in the air stream, the injection of the fuel into the airstream and
its atomization being effected by producing, during a variable
portion of the induction period, ultrasonic vibrations of the open
end of the nozzle in its longitudinal direction, the quantity of
fuel injected during, for example, each induction stroke of each
cylinder, being controlled by varying the fraction of the period of
the stroke or the like in which electric current of appropriate
frequency is applied to a transducer to produce the ultrasonic
vibrations.
In order that the invention may be more readily understood, one
embodiment will now be described in more detail with reference to
the accompanying drawings, in which
FIG. 1 is a somewhat diagrammatic axial section of a nozzle unit
comprising an ultrasonic transducer and an open-ended
fuel-injection nozzle, and
FIG. 2 is a diagram of the layout and electric circuit for a
fuel-injection system.
Referring now first to FIG. 1, a suitable form of nozzle unit
comprises a piezo-electric transducer element 1, for example of
barium-titanate material, in the form of a cylindrical annulus
having metallized coatings 2 and 3 respectively applied to its
exterior and interior cylinder surfaces so that, when an
alternating voltage is applied across the two coatings, the element
will alternately contract and expand longitudinally. This
longitudinal vibration is transmitted, through aluminum bodies 4
and 5 respectively, to a nozzle body 6 at one end and to a second
body 7 at the other end of the device. These two bodies are clamped
to the two sides of the transducer element 1 by a stud 8 having
screw-threaded ends engaging screw-threaded bores of the nozzle
body 6 and of the second body 7 respectively. A bush 9 of
insulating material having at one end a flange 9a and a washer 10,
also of insulating material and placed against the other end of the
bush 9, are provided to center the element 1 relative to the
aluminum bodies 4 and 5 and prevent these bodies from electrically
short-circuiting the inner and outer coatings 2 and 3 of the
element 1. The nozzle 6 has an axial bore 11, which is open at its
outer end, and to which near its other end fuel is supplied from a
flexible connection 12 by a passage 13. It has been found that,
when, with the fuel pressure at the nozzle outlet balanced with the
pressure of the adjacent air, the nozzle 11 is vibrated
longitudinally by the application of a suitable
ultrasonic-frequency voltage to the coatings 2 and 3 of the element
1, fuel is emitted from the nozzle in the form of a spray at a rate
which, for a given frequency and amplitude of the voltage, is
substantially constant, so that the amount of fuel injected is
proportionate to the length of time during which the ultrasonic
voltage is applied.
Referring now to FIG. 2, which illustrates a convenient manner in
which the transducer and nozzle equipment may be arranged in the
induction pipe of an engine, the unit described with reference to
FIG. 1, bears as a whole unit the reference numeral 14 and is
arranged in an induction pipe 15 containing near it inlet end a
throttle 18. This induction pipe leads to the inlet manifold and
inlet valves 16 of a combustion engine 17, and the unit 14 is fed
with fuel from a float chamber 19, which is accommodated in the
induction pipe 15 and is fed under the control of a needle valve
19a operated by a float 19b accommodated in the float chamber 19,
from a feed line 20 supplied in the usual manner either under
static pressure from a fuel tank or by a suitable low-pressure fuel
pump, not shown. The float chamber 19 is vented, above its fuel
level, to the interior of the induction pipe 15, so that the
pressure acting in the induction pipe at the end of the nozzle 14
also acts on the fuel in the float chamber 19, and the level of
fuel in the float chamber is so arranged that the fuel pressure in
the nozzle 14 is insufficient to cause any significant amount of
fuel to escape from the opening of the nozzle 11 of the unit 14
except during operation of the transducer element 1.
In order to operate the transducer element, a voltage of ultrasonic
frequency is supplied to it by leads 21 and 22 from a vibrator
circuit 23 under the control of a transistor switch 24. The latter
is controlled by a differential distributor 25, in which an
engine-driven wiper arm 38 co-operates with a control-ring element
36 and an inner ring 41 to periodically energize an ON-line 26 to
close the transistor switch 24 and subsequently to energize an
OFF-line to open the transistor switch. In the case of a
four-stroke engine this closing of the transistor switch is
effected shortly after the beginning of each induction stroke, and
the OFF-line 27 is energized at a later time of the induction
stroke. Both times are variable by signals in a manner which will
now be discussed in more detail.
One of the signals employed for this purpose is arranged to be
produced by an alternating-current generator 28 of the
permanent-magnet type. This generator is driven by the engine and
produces a voltage proportional to the engine speed. Another signal
is produced by a manifold-pressure transducer 29, which alters the
transmission ratio or multiplication factor of a variable
transformer 30 by varying the number of operative turns in the
secondary transformer winding 33. The primary winding 31 of the
transducer 30 is supplied with the voltage output of the
engine-driven generator 28 via a resistor 32 whose resistivity
varies substantially with its temperature, and which is arranged in
the induction pipe 15. The output of the transformer secondary 33
is, after rectification in a rectifier bridge 34, applied to a
torque motor 35 which is so arranged that it will take up an angle
of deflection proportionate to its input voltage, and which
determines the angle setting of the ring element 36 of the
differential distributor 25 in such manner as to increase the
length of the injection period relative to the total period of each
input stroke with rising engine speed and with rising pressure in
the induction line. An adjustable idling-setting stop 37 has been
additionally provided to prevent the length of the fraction of the
input stroke utilized for injection from falling below a
predetermined minimum.
The triggering of the ON-line 26 and the OFF-line 27 is effected by
co-operation of the engine-driven wiper arm 38, which, in the case
of a four-stroke engine, rotates at half the engine speed, with an
ON-line contact 39 arranged on the adjustable control-ring element
36, while an OFF-line contact 40 is arranged on the normally fixed
inner ring 41. Since in practice the inlet-pressure transducer 29
measures the excess pressure in the induction pipe over ambient
pressure rather than the absolute pressure, a correction of the
signal in accordance with the ambient pressure is required, more
particularly in order to compensate for varying altitude, and for
this purpose an altitude-control resistor 45 is included in the
energizing circuit of the torque motor 35. This resistor may be
operated by an aneroid capsule 44, although, since this control is
not particularly critical, manual altitude control might be
substituted. In order to facilitate starting in cold weather, the
inner ring 41 is adapted to be manually turned by a choke lever 42
by a certain angle in the direction of the arrow X from its normal
position determined by a stop 43.
With the arrangement as so far described a minimum amount of fuel
corresponding to idling at the actual speed of the engine will be
supplied even when the throttle is closed at high engine speed,
whereas in such conditions, for example when coasting down a hill,
it is really desirable that fuel should not be supplied at all or
at least its supply to be cut to a minimum. For this reason a stop
50, which normally limits the movement of the pressure-transducer
29 at low induction-line pressure, is allowed to yield when the
suction exceeds a predetermined value. This is achieved by the
provision of a trapped pre-loaded spring 46, so that when the
suction exceeds that predetermined value, the pressure transducer
will move below the normal minimum position, thus causing the ring
36 to move beyond the normal minimum position for the actual speed
of the engine to the position defined by the stop 37. If desire,
compression of the pre-loaded spring 46 may alternatively be
employed to switch off the vibrator circuit altogether, for example
by a switch contact 47 in a line 48 leading to an auxiliary
transistor switch 49 in the output of the vibrator circuit 23.
It will be readily appreciated that while a magnetostrictive
transducer has been described and illustrated, the system of the
invention is not limited to the use of this kind of transducer,
which may for example be replaced by an electromagnetic
transducer.
A further auxiliary switch, controlled for example by the output
voltage of alternator 28, is preferably included in the output of
the vibrator circuit to prevent the injection of fuel until the
engine speed reaches a predetermined value lower than the idling
speed.
Furthermore while in the illustrated embodiment the nozzle 14 and
float chamber 19 are shown in the induction pipe 15 at a point
beyond the throttle 18, this arrangement may be modified by
arranging the float chamber 19 outside the induction pipe so long
as its vent aperture 19c is arranged to communicate with the
appropriate part of the induction pipe 15, and if desired the
injection nozzle 14 may be arranged in the entry portion of the
induction pipe 15 preceding the position of the throttle 18, i.e.
at a point where pressure variations from the outside atmosphere
are relatively small.
* * * * *