GB2248274A - I.c. engine fuel supply manifold - Google Patents

I.c. engine fuel supply manifold Download PDF

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Publication number
GB2248274A
GB2248274A GB9120374A GB9120374A GB2248274A GB 2248274 A GB2248274 A GB 2248274A GB 9120374 A GB9120374 A GB 9120374A GB 9120374 A GB9120374 A GB 9120374A GB 2248274 A GB2248274 A GB 2248274A
Authority
GB
United Kingdom
Prior art keywords
fuel
tubular body
duct
manifold
pressure regulator
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
GB9120374A
Other versions
GB9120374D0 (en
GB2248274B (en
Inventor
Alfredo Terzi
Flavio Giovannini
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Weber SRL
Original Assignee
Weber SRL
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Weber SRL filed Critical Weber SRL
Publication of GB9120374D0 publication Critical patent/GB9120374D0/en
Publication of GB2248274A publication Critical patent/GB2248274A/en
Application granted granted Critical
Publication of GB2248274B publication Critical patent/GB2248274B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M69/00Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel
    • F02M69/46Details, component parts or accessories not provided for in, or of interest apart from, the apparatus covered by groups F02M69/02 - F02M69/44
    • F02M69/54Arrangement of fuel pressure regulators
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M69/00Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel
    • F02M69/46Details, component parts or accessories not provided for in, or of interest apart from, the apparatus covered by groups F02M69/02 - F02M69/44
    • F02M69/462Arrangement of fuel conduits, e.g. with valves for maintaining pressure in the pipes after the engine being shut-down
    • F02M69/465Arrangement of fuel conduits, e.g. with valves for maintaining pressure in the pipes after the engine being shut-down of fuel rails

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)

Abstract

The manifold is formed of a tube 1 with injector connectors 2 and an inner tube 3 defining a supply duct 8 therebetween and has a fuel pressure regulator 7 and a diaphragm 14 for damping fuel pressure fluctuations in the supply duct. The location of the regulator 7 and the diaphragm 14 and the orientation of the manifold fuel supply and discharge connectors 22, 23 may vary (Figs. 2 to 4). <IMAGE>

Description

1 c 1 TUEL SUPPLY MANIFOLD FOR A SUPPLY LINE FOR AN INTERNAL COMBUSTION
ENGINE, OF THE TYPE HAVING ELECTROMAGNETICALLY-OPERATED FUEL METERING AND ATOMISING VALVES" The present invention relates to a fuel supply manifold for a supply line for an internal combustion engine which is arranged to supply fuel under pressure to a plurality of electromagnetically-operated fuel metering and atomising valves.
Manifolds of this type normally include a first tubular body which has a plurality of connectors f or the said valves and a second tubular body, normally disposed within the first and defining therewith a duct for supplying the fuel to the connectors, the duct being bounded by the inner and outer surfaces of the first and second tubular bodies respectively.
Such manifolds also include a pressure regulator which is arranged to keep the fuel pressure in the supply duct at a predetermined value; the regulators comprise essentially an inlet port and an outlet port for the fuel which communicate with the fuel supply duct def ined above and with a discharge duct for the fuel respectively, and an obturator member arranged to allow the fuel to flow 2 from the inlet port to the outlet port when the pressure in the supply duct exceeds a predetermined value. The pressure regulator is normally disposed in a seat in the manifold.
Manifolds of the type described above have the disadvantage that they do not provide a correct supply of fuel to the metering and atomising valves, particularly when the manifolds are used in supply lines in which the opening phases of the fuel metering and atomising valves occur simultaneously in all cylinders of the engine. Indeed, in any case of this type of operation, since the pump which supplies the fuel causes sharp, rapid pressure oscillations in the supply duct to the manifold, is vibrations, that is pressure waves, may be triggered in the fuel within the manifold itself and, not being damped by the pressure regulator, impede its operation and consequently have a harmful effect on the supply of fuel to the metering and atomising valves.
The object of the present invention is to provide a manifold of the type just indicated which eliminates the disadvantage described above.
Another object of the invention is to provide a manifold of the type indicated which is very compact, of small bulk and is consequently quick and simple to install in 3 an engine of a motor vehicle.
These objects are achieved by means of a fuel supply manifold for a fuel supply line for an internal combustion engine which is arranged to supply fuel under pressure to a plurality of electromagnetically-operated fuel metering and atomising valves, comprising essentially; a f irst tubular body having a plurality of connectors for the valves; a second tubular body disposed within the first and defining therewith a duct for supplying fuel to connectors, the duct being bounded by the inner and outer surfaces of the first and second tubular bodies respectively; a pressure regulator for maintaining the fuel pressure in the supply duct at a predetermined value, the pressure regulator comprising essentially an inlet port and an outlet port for the fuel communicating respectively with the fuel supply duct and with a fuel discharge duct and an obturator member for allowing the fuel to flow from the inlet port to the outlet port when the pressure in the supply duct exceeds a predetermined value, the pressure regulator being disposed in a seat in the manifold; characterised in that it includes:
a vibration damping unit for damping the pressure 4 waves in the fuel in the supply duct, the unit comprising essentially a deformable diaphragm acted upon by a spring, the diaphragm forming one wall of the fuel supply duct so that vibrations in the fuel within the duct are damped by the deformation of the diaphragm.
In order to provide a better understanding of the structure of the supply manifold of the invention, a more detailed description of the manifold itself will now be given, by way of example, with reference to the appended drawings in which:
Figures 1 to 4 show longitudinal sections of various embodiments of the supply manifold of the invention.
With reference first of all to Figure 1, the manifold of the invention comprises essentially a first tubular body 1 having a plurality of connectors 2 each of which is arranged to enable the connection of an electromagnetically-operated fuel metering and atomising valve of known type. The manifold also includes a second tubular body 3, within the first and substantially coaxial therewith, which, together with the first tube, defines a duct 4 for supplying fuel to the connectors 2; the said duct is bounded by the inner surface 5 and the outer surface 6 respectively of the tubular bodies 1 and 3.
A pressure regulator generally indicated 7, of known type, forms part of the manifold of the invention and is arranged to keep the f uel pressure in the duct 4 at a predetermined value; the regulator comprises essentially a casing 8 formed with an inlet port 7i and an outlet port 7u for the fuel which communicate respectively with the supply duct 4 and with a fuel discharge duct 9 which, in the embodiment of Figure 1, is formed within the second tubular body 3. The pressure regulator 7 also includes an obturator member (not shown) housed within the casing 8 and arranged to allow fuel to flow from the inlet port 7i to the outlet port 7u when the pressure in the supply duct 4 exceeds a predetermined value.
In the embodiment of Figure 1, the pressure regulator is housed in a seat 10 in the tubular body 1 and is f ixed therein by means of a suitable collar 11.
In accordance with the invention, the manifold includes a vibrationdamping unit generally indicated 13 which is arranged to damp vibrations in the fuel within the duct 4; this unit comprises essentially a deformable diaphragm 14 acted upon by a spring 15; these two members are located within a cup-shaped body 16 which, in the embodiment of Figure 1, is fixed to the end of the tubular body 1 which is opposite that to which the pressure regulator 7 is fixed.
is 6 In accordance with the invention, the damping unit 13 is disposed in the manifold in such a manner that the diaphragm 14 essentially forms one wall of the fuel supply duct 4 and any vibrations which occur in the fuel within the duct itself are damped by the deformation of the diaphragm. Conveniently, two discs 17 are fixed to the central part of the diaphragm, one of the discs providing an abutment for one end of the spring 15 while the other is arranged to bear on a stop rod 18 when the damping unit is in the rest condition shown in Figure 1.
Moreover, the periphery of the diaphragm 14 bears against an annular seat 19 at the said end of the tubular body 1 and the edge of the cup-shaped body 16 is bent back towards the seat itself so as to clamp it to the manifold together with the diaphragm.
In the embodiment of Figure 1, the first tubular body comprises two interconnected parts indicated la and ib; the second of these includes, essentially, a portion of a supply duct 20 and a pair of discharge ports 21 connected to the duct 9 within the second tubular body 3. As is clearly seen in Figure 1, the damping unit 13 is fixed to one end of the part la while the pressure regulator 7 is fixed to one end of the part lb.
The manifold also includes a fuel inlet connector 22 7 which communicates with the supply duct 4 and a discharge connector 23 connected to the ports 21: in the embodiment of Figure 1, the axes of the inlet and discharge connectors are parallel to each other and disposed at the right-hand end of the manifold.
In the embodiments of Figures 3 and 4, the damping unit 13 is fixed to the seat 10 formed at one end of the part la of the first tubular body 1 while the pressure regulator 7 is fixed in a second seat 26 formed in the part lb of the body; the axes of the seats 10 and 26 are perpendicular to each other. In the embodiment of Figures 3 and 4, the second tubular body 3 puts the fuel supply duct 4 in communication with the inlet port 7i of the pressure regulator 7; for this purpose, the left-hand end of the body 3 is located at a certain distance from the diaphragm 14 of the damping unit 13 and the righthand end of the body communicates with the ports 27 formed in the part lb which in turn communicate with the inlet port 7i of the pressure regulator 7.
Moreover, the seat 10 of the damping unit 13 houses a bush 28 for keeping the left-hand end of the tubular body 3 centred and for constituting a stop for the diaphragm 14 of the damping unit 13.
The fuel supply duct 4 communicates with a fuel inlet 8 connector 29 formed in the part lb; fuel discharge ports 30 are formed in this same part and communicate with a discharge connector 31.
The embodiments 3 and 4 differ from each other solely in the f orm of the part lb of the tubular body 1; in the embodiment of Figure 3, the righthand end of the tubular body 3 is inserted in a seat 32 formed in the part lb while in the embodiment of Figure 4, a sleeve 33 projecting axially from the part lb is inserted in the right hand-end of the tubular body 3; moreover, in the two cases, the angles between the axes of the inlet and outlet connectors 29 and 31 differ.
The embodiment of Figure 2 differs from that of Figure 1 solely in the form of the part lb of the tubular body 1; in fact, while in Figure 1 the outlet connector 23-is perpendicular to the axis of the part 1b and is parallel to that of the inlet connector 22, in the embodiment of Figure 2, the axes of the inlet and outlet connectors 22 and 23 are not parallel to each other nor to the longitudinal axis of the manifold.
The manifold described above operates as follows. The fuel is supplied to the supply duct 4 through the inlet connector 22 and from this duct passes through the connectors 2 to the fuel metering and atomising valves; 9 when the pressure in the duct 4 exceeds a predetermined value, the obturator member (not shown) of the pressure regulator 7 puts the inlet port 7i in communication with the outlet port 7u of the regulator itself and hence a certain quantity of fuel may be delivered to the exhaust through the discharge duct 9, the ports 21 and the connector 23.
When there are sharp, rapid variations in the fuel pressure in the duct 4, triggered for example by a high rate of flow of the fuel which is to be supplied to the fuel metering and atomising valves whenever these initiate the injection phases at the same instant, or because of sharp pressure variations generated by the fuel-supply pump, the damping unit 13 can intervene to damp these vibrations. Since the diaphragm 14 of this unit constitutes essentially a wall of the fuel supply duct 4, the pressure reigning at any instant within the duct acts on this diaphragm: hence, when vibrations are triggered, these are damped by the deformability of the diaphragm itself which is loaded by the spring 15 and which, essentially, allows the volume of the supply duct 4 to increase by small amounts.
The operation of the manifold of the embodiments of Figures 3 and 4 is similar to that just described and may easily be determined from the drawings themselves.
It is clear that the described embodiments of the present invention may be modified and varied, both in form and in the arrangement of the various parts, without thereby departing from the scope of the invention.
11

Claims (9)

1.. A fuel supply manifold f or a fuel supply line f or an internal combustion engine which is arranged to supply fuel under pressure to a plurality of electromagnetically-operated fuel metering and atomising valves, comprising essentially; a first tubular body (1) having a plurality of connectors (2) for the valves; a f irst tubular body (1) having a plurality of connectors (2) for the valves; a second tubular body (3) disposed within the first and defining therewith a duct (4) for supplying the fuel to the connectors, the duct being bounded by the inner surface (5) and the outer surface (6) respectively of the first and second tubular bodies; a pressure regulator (7) for maintaining the fuel pressure in the supply duct (4) at a predetermined value, the pressure regulator comprising essentially an inlet port (7i) and an outlet port (7u) for the fuel - communicating respectively with the fuel supply duct (4) and with a fuel discharge duct (9) and another obturator member for allowing the fuel to flow from the inlet port (7i) to the outlet port (7u) when the pressure in the supply duct exceeds a predetermined value, the pressure regulator being disposed in a seat (10) in the manifold; 12 characterised in that it includes:
a vibration damping unit (13) for damping the pressure waves in the fuel in the supply duct (4), the unit comprising essentially a deformable diaphragm (14) acted apon by a spring (15), the diaphragm forming one wall defining the fuel supply duct (4) so that the vibrations in the fuel within the duct are damped by the deformation of the diaphragm (14).
2. A manifold according to claim 1 characterised in that the damping unit (13) is f ixed to one end of the first tubular body (1) so that the diaphragm (14) of the unit defines one end of the supply duct.
3. A manifold according to claim 1, characterised in that the damping unit (13) includes a cup-shaped housing (16) which houses the spring (15) and against the edge of which bears the diaphragm (14), the housing being fixed to an annular seat (19) at the end of the first tubular body 1.
4. A manifold according to one of the preceding claims, characterised in that the first tubular body (1) includes two interconnected parts (1a and 1b), the pressure regulator (7) being f ixed in a seat (10) formed at one end of a f irst (1a) of the parts of the f irst tubular body (1) and the damping unit (13) being f ixed to one end 13 of the second (ib) of the parts of the first tubular (1) -
5. A manifold according to claim 4, characterised in that the outlet port of the pressure regulator (7u) communicates with the chamber within the second tubular body (3) which forms the fuel discharge duct (9).
6. A manifold according to claim 4 or claim 5, characterised in that the second tubular body (3) communicates with dispharge ports (21) formed in the second part (1b) of the tubular body (1).
is
7. A manifold according to one of claims 1 to 3, characterised in that the first tubular body (1) includes two interconnected parts (1a, 1b), the damping unit (13) being fixed to a first seat (10) formed at one end of a first (1a) of the parts of the first tubular body (1) and the pressure regulator (13) being fixed in a second seat (2 6) in the second (ib) of the parts of the first tubular body (1), the axes of the seats (10, 26) being perpendicular to each other.
8. A manifold according to claim 7, characterised in that the second tubular body (3) puts the fuel supply duct (4) into communication with the inlet port (7i) of the pressure regulator (7), the fuel discharge port (30) 4 j - 14 being formed in the second part (1b) of the f irst tubular body (1).
9. A fuel supply manifold for a fuel supply line of an internal combustion engine, substantially as described and illustrated in the appended drawings.
GB9120374A 1990-09-28 1991-09-25 Fuel supply manifold for a supply line for an internal combustion engine, of the type having electromagnetically-operated fuel metering and atomising valves Expired - Fee Related GB2248274B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT67731A IT1241694B (en) 1990-09-28 1990-09-28 FUEL SUPPLY MANIFOLD FOR A FUEL DEVICE FOR AN INTERNAL COMBUSTION ENGINE OF THE TYPE PROVIDED WITH METERING VALVES AND FUEL PULVERIZERS WITH ELECTROMAGNETIC ACTUATED FUEL

Publications (3)

Publication Number Publication Date
GB9120374D0 GB9120374D0 (en) 1991-11-06
GB2248274A true GB2248274A (en) 1992-04-01
GB2248274B GB2248274B (en) 1994-11-16

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ID=11304853

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9120374A Expired - Fee Related GB2248274B (en) 1990-09-28 1991-09-25 Fuel supply manifold for a supply line for an internal combustion engine, of the type having electromagnetically-operated fuel metering and atomising valves

Country Status (4)

Country Link
DE (1) DE4131967C2 (en)
FR (1) FR2667360B1 (en)
GB (1) GB2248274B (en)
IT (1) IT1241694B (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0575752A1 (en) * 1992-05-21 1993-12-29 MAGNETI MARELLI S.p.A. Manifold for a system for supplying fuel to an internal-combustion engine
US5609138A (en) * 1995-06-17 1997-03-11 Robert Bosch Gmbh Pressure regulating device for a fuel delivery system
US6809696B1 (en) 1999-10-18 2004-10-26 Polymer Kompositer I Goteborg Ab Microwave components

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US5513613A (en) * 1994-07-15 1996-05-07 Ford Motor Company Automotive fuel rail end closure device with temperature sensor for returnless fuel system
DE19618791C1 (en) * 1996-05-10 1997-12-11 Mtu Friedrichshafen Gmbh Fuel injection system for diesel engine
DE19729392C2 (en) * 1997-07-09 1999-05-06 Siemens Ag Fuel storage with seal
DE19737600A1 (en) * 1997-08-28 1999-03-04 Bayerische Motoren Werke Ag Fuel pressure regulator for internal engine
DE19927467A1 (en) * 1999-06-16 2000-12-21 Volkswagen Ag Fuel distributor for IC engines has tubular insert to form throttle between fuel feed channel/pipe and fuel return pipe
DE19938864C1 (en) * 1999-08-17 2000-09-28 Siemens Ag Fuel-injection system for combustion engine
US6148798A (en) * 1999-10-01 2000-11-21 Delphi Technologies, Inc. Coaxial flow through fuel rail with a damper for a recirculating fuel system
DE102011118756A1 (en) * 2011-11-17 2013-05-23 L'orange Gmbh Pressure reservoir for fuel injection device of combustion engine, has fuel flow path that is defined in inlet-outlet end and remote end of pressure reservoir housing with respect to flow return point

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US4679537A (en) * 1984-12-19 1987-07-14 Robert Bosch Gmbh Damping device
US4955409A (en) * 1988-04-18 1990-09-11 Suzuki Jidosha Kogyo Kabushiki Kaisha Fuel supply system
EP0403871A1 (en) * 1989-06-13 1990-12-27 WEBER S.r.l. A fuel manifold preferably of plastics material adapted to supply fuel to the injectors of an internal combustion engine fuel injection device

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US4205637A (en) * 1976-12-13 1980-06-03 Toyota Jidosha Kogyo Kabushiki Kaisha Electronic fuel injection system for an internal combustion engine having electromagnetic valves and a fuel damper upstream thereof
US4601275A (en) * 1982-08-23 1986-07-22 General Motors Corporation Fuel rail
DE3322547C2 (en) * 1983-06-23 1987-03-12 Dr.Ing.H.C. F. Porsche Ag, 7000 Stuttgart Arrangement for damping vibrations in the fuel supply of an internal combustion engine
DE3536814A1 (en) * 1985-10-16 1987-04-16 Knecht Filterwerke Gmbh Injection device for an injection internal combustion engine
US4649884A (en) * 1986-03-05 1987-03-17 Walbro Corporation Fuel rail for internal combustion engines
IT208360Z2 (en) * 1986-11-18 1988-05-28 Weber Srl GROUP FOR A FUEL COLLECTOR WITH INTEGRATED PRESSURE REGULATOR FOR INJECTION FUEL OF INTERNAL COMBUSTION ENGINES
US4836246A (en) * 1987-08-03 1989-06-06 Colt Industries Inc. Manifold for distributing a fluid and method for making same
IT214868Z2 (en) * 1988-09-30 1990-07-04 Weber Srl SEMI-FINISHED TO CREATE A FUEL SUPPLY MANIFOLD FOR AN INTERNAL COMBUSTION ENGINE POWER SUPPLY

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4679537A (en) * 1984-12-19 1987-07-14 Robert Bosch Gmbh Damping device
US4955409A (en) * 1988-04-18 1990-09-11 Suzuki Jidosha Kogyo Kabushiki Kaisha Fuel supply system
EP0403871A1 (en) * 1989-06-13 1990-12-27 WEBER S.r.l. A fuel manifold preferably of plastics material adapted to supply fuel to the injectors of an internal combustion engine fuel injection device

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0575752A1 (en) * 1992-05-21 1993-12-29 MAGNETI MARELLI S.p.A. Manifold for a system for supplying fuel to an internal-combustion engine
US5333587A (en) * 1992-05-21 1994-08-02 Weber S.R.L. Manifold for a system for supplying fuel to an internal-combustion engine
US5609138A (en) * 1995-06-17 1997-03-11 Robert Bosch Gmbh Pressure regulating device for a fuel delivery system
US6809696B1 (en) 1999-10-18 2004-10-26 Polymer Kompositer I Goteborg Ab Microwave components
US7573430B2 (en) 1999-10-18 2009-08-11 Polymer Kompositer I Goteborg Ab Microwave components

Also Published As

Publication number Publication date
IT9067731A1 (en) 1992-03-28
GB9120374D0 (en) 1991-11-06
IT9067731A0 (en) 1990-09-28
FR2667360B1 (en) 1995-05-19
DE4131967A1 (en) 1992-04-02
DE4131967C2 (en) 1998-05-14
IT1241694B (en) 1994-01-31
FR2667360A1 (en) 1992-04-03
GB2248274B (en) 1994-11-16

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PCNP Patent ceased through non-payment of renewal fee

Effective date: 20030925