U.S. patent number 3,693,889 [Application Number 05/169,030] was granted by the patent office on 1972-09-26 for fuel injection nozzle.
This patent grant is currently assigned to Robert Bosch GmbH. Invention is credited to Gregor Schuster.
United States Patent |
3,693,889 |
Schuster |
September 26, 1972 |
FUEL INJECTION NOZZLE
Abstract
In a fuel injection nozzle, for varying the fuel quantities
injected thereby, there is provided a movable throttle member which
determines the flow passage section of a bypass or return channel
provided in the fuel injection nozzle. The position and thus the
throttling effect of the throttle member is determined by the axial
distance between two threadedly interengaging components of the
fuel injection nozzle.
Inventors: |
Schuster; Gregor (Stuttgart,
DT) |
Assignee: |
Robert Bosch GmbH (Stuttgart,
DT)
|
Family
ID: |
5778813 |
Appl.
No.: |
05/169,030 |
Filed: |
August 4, 1971 |
Foreign Application Priority Data
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|
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Aug 4, 1970 [DT] |
|
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P 20 38 643.0 |
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Current U.S.
Class: |
239/533.6;
239/124; 239/582.1; 239/579 |
Current CPC
Class: |
F02M
61/02 (20130101) |
Current International
Class: |
F02M
61/02 (20060101); F02M 61/00 (20060101); B05b
001/30 () |
Field of
Search: |
;239/124,125,126,127,533,579,581,582 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Wood, Jr.; M. Henson
Assistant Examiner: Thieme; Reinhold W.
Claims
What is claimed is:
1. In a fuel injection nozzle of the type that includes (a) means
receiving fuel under pressure from outside said nozzle, (b) an
injection opening through which a first part of said fuel leaves
said nozzle and (c) a bypass channel through which a second, or
remaining part of said fuel is returned uninjected, the improvement
comprising,
A. a first part containing a portion of said bypass channel,
B. a throttle member movably disposed in said portion of said
bypass channel,
C. a flow passage section defined jointly by said throttle member
and said portion of said bypass channel; the magnitude of said flow
passage section being determined by the position of said throttle
member in said portion of said bypass channel,
D. a second part secured to said first part in axial alignment
therewith,
E. means for varying the axial position of said first and second
parts with respect to one another and
F. an abutment integral with said second part and moving with
respect to said portion of said bypass channel upon variation of
said axial position; said abutment being disposed in the path of
motion of said throttle member for variably limiting its extent of
motion.
2. An improvement as defined in claim 1, wherein said throttle
member has a conical configuration.
3. An improvement as defined in claim 1, wherein said first and
second parts are threadedly secured to one another; said axial
position of said parts with respect to one another is variable by
rotating said parts relative to one another; said portion of said
bypass channel is formed as a cylindrical bore; said throttle
member is axially reciprocably held in said cylindrical bore; said
improvement further includes a tubular stub forming another portion
of said bypass channel and forming an integral component of said
second part; said tubular stub telescopically extends into said
cylindrical bore and has a terminal edge face constituting said
abutment.
4. An improvement as defined in claim 3, including
A. a closing member integral with said throttle member and disposed
adjacent said injection opening to cooperate therewith and
B. a spring urging said throttle member away from said abutment and
urging said closing member into a position where it obturates said
injection opening; said spring has a force which is smaller than an
oppositely directed force derived from said fuel under pressure to
permit said throttle member to move into engagement with said
abutment and said closing member to open said injection opening in
response to said fuel under pressure.
5. In a fuel injection nozzle of the type that includes (a) means
receiving fuel under pressure from outside said nozzle, (b) an
injection opening through which a first part of said fuel leaves
said nozzle and (c) a bypass channel through which a second, or
remaining part of said fuel is returned uninjected, the improvement
comprising,
A. a first part containing a portion of said bypass channel,
B. a throttle member movably disposed in said portion of said
bypass channel,
C. a flow passage section defined jointly by said throttle member
and said portion of said bypass channel; the magnitude of said flow
passage section being determined by the position of said throttle
member in said portion of said bypass channel,
D. a second part secured to said first part in axial alignment
therewith,
E. means for varying the axial position of said first and second
parts with respect to one another and
F. means integral with said second part and cooperating with said
throttle member to vary said position thereof upon variation of
said axial position of said first and second parts.
Description
This invention relates to a fuel injection nozzle wherein the
quantities of the injected fuel may be altered by changing the flow
passage section of a return or bypass channel by means of a
throttle member which is disposed in said channel and which is
associated with a movable abutment to change its stroke.
In a known fuel injection nozzle of the aforenoted type (such as
disclosed, for example, in German Published patent application DOS
No. 1,551,645), for the purpose of altering the quantities of the
returning (bypassed) fuel, and thus changing the quantities of
injected fuel, either the nozzle has to be entirely removed from
the fuel injection system or an adjustable throttle member has to
be provided at an accessible location of the bypass channel. The
first solution has the disadvantage that every time a nozzle is
removed, the oil conduits are drained and further, until the
desired adjustment is obtained, the nozzle has to be screwed in and
out several times. The second solution has the disadvantage that in
the nozzle structure between the throttle member and the injection
opening there prevails a relatively large oil volume which,
dependent upon the elasticity of the oil and the differing
viscosity, leads to changes in the injected fuel quantities and
particularly to additional or after-injection.
It is an object of the invention to provide an improved fuel
injection nozzle of the aforenoted type wherein the quantities of
the returned fuel may be altered without removal of the nozzle.
Briefly stated, according to the invention there is provided a fuel
injection nozzle which comprises two parts, the relative position
of which is variable in an axial direction. Between the two parts
there is movably disposed the aforementioned throttle member. One
of said parts accommodates the pressure chamber and the injection
openings, as well as that part of the return conduit, the flow
passage section of which is varied by the throttle member. The
other part of the fuel injection nozzle carries an abutment which
determines the stroke of the throttle member.
The invention will be better understood, as well as further objects
and advantages will become more apparent, from the ensuing detailed
specification of two exemplary embodiments taken in conjunction
with the drawing, wherein:
FIG. 1 is an axial sectional view of a first embodiment of the
invention and
FIG. 2 is an axial sectional view of a second embodiment of the
invention.
Turning now to FIG. 1, there is shown a hollow nozzle body 1 into
which there is clamped, by means of a sleeve 2 having an externally
threaded integral collar, an insert 3 provided with an injection
opening 3'. The sleeve 2 has a relatively small-diameter,
downwardly open axial bore 6 and an adjoining, relatively
large-diameter, upwardly open axial bore 7. Between the sleeve 2
and the insert 3 there is provided a vortex chamber 4 which is
formed of a cylindrical and an adjoining conical cavity. The latter
continues in the injection opening 3'. The cylindrical portion of
the vortex chamber 4 communicates with the bore 6 of the sleeve 2.
Into the vortex chamber 4 there merge tangential supply channels 8
(only one shown).
The bore 7 telescopically receives a tubular stub 9 of a nozzle
holder 10 shown only in part. The nozzle holder 10 threadedly holds
the nozzle body 1, so that depending upon the angular position of
the stub 9, the latter projects into the bore 7 to a greater or
lesser extent. In order to prevent an accidental rotation of the
nozzle body 1 with respect to the nozzle holder 10, these two
components are tightened to one another by means of a counternut
11. In the bore 7 there is axially displaceably disposed a throttle
member 12 provided with guiding wings 12'. The conical
needle-shaped extension 13 of the throttle member 12 projects into
the bore 6 to affect the flow passage section thereof. Dependent
upon how far the tubular stub 9 extends into the bore 7 after
threading the nozzle body 1 into the nozzle holder 10, the needle
13, during operation, projects into the bore 6 to a greater or
lesser extent thus throttling the bore 6 in a variable manner.
The fuel admitted to the fuel injector nozzle in the direction of
arrows A through conduits not shown, flows through a schematically
shown filter 14 into an annular space between the nozzle body 1 and
the sleeve 2 then through openings 2' and supply channels 8 into
the vortex chamber 4. From the vortex chamber 4 one part of the
fuel is injected into a combustion chamber of the combustion engine
through the nozzle opening 3', while the other part of the fuel
flows through the bores 6 and 7 into the tubular stub 9 and then,
through the return tube 15 in the direction of arrow B back, for
example, to a fuel tank (not shown).
It is seen that the more the nozzle body 1 is screwed into the
nozzle holder 10, the smaller is the flow passage section of the
annular chamber formed between the needle 13 and the bore 6 and the
greater is the fuel quantity injected into the associated
combustion chamber of the internal combustion engine. As the fuel
under pressure flows upwardly in the bore 6, the throttle member 12
is displaced upwardly and is stopped by an abutment constituted by
the lower terminal edge face 9a of the tubular stub 9. FIG. 1 shows
the throttle member 12 in this operative position.
Turning now to FIG. 2, in the second embodiment shown therein, a
throttle member 16 -- functioning in the same manner as the
throttle member 12 of the first embodiment -- has an integral,
axially aligned pin 17 which serves as a closing member for the
injection opening 3'. For this purpose the throttle member 16 is
biased by a spring 18. At the conical portion of the throttle
member 16 there are disposed wings 20 to ensure a uniform central
guidance of the throttle member in the bore 6.
During the inoperative periods of the fuel injection nozzle, the
throttle member 16 assumes a position as shown in FIG. 2. In this
position the pin 17 entirely obturates the nozzle opening 3'. As
soon as fuel under pressure is admitted to the vortex chamber 4,
the throttle member 16 is, under simultaneous compression of the
spring 18, shifted into its operative position where it contacts an
abutment pin 19 held in the tubular stub 9. The flow passage
section of the bore 6 is determined by the axial height position of
the abutment pin 19. The second embodiment is particularly
advantageous in that it comprises a nozzle closing means (i.e., the
pin 17) which effectively prevents an after-injection (or the
emptying of the fuel conduits) subsequent to the cut-off of fuel to
the fuel injection nozzle.
* * * * *