GB2404693A - Minimising deposit formation in high pressure fuel injection valves - Google Patents

Minimising deposit formation in high pressure fuel injection valves Download PDF

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Publication number
GB2404693A
GB2404693A GB0318164A GB0318164A GB2404693A GB 2404693 A GB2404693 A GB 2404693A GB 0318164 A GB0318164 A GB 0318164A GB 0318164 A GB0318164 A GB 0318164A GB 2404693 A GB2404693 A GB 2404693A
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GB
United Kingdom
Prior art keywords
angle
volume
edge
needle orifice
central axis
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
GB0318164A
Other versions
GB2404693B (en
GB0318164D0 (en
Inventor
Brian A Gorman
William James Imoehl
John Nally
Wei-Min Ren
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.)
Siemens AG
Original Assignee
Siemens AG
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 Siemens AG filed Critical Siemens AG
Priority to GB0318164A priority Critical patent/GB2404693B/en
Publication of GB0318164D0 publication Critical patent/GB0318164D0/en
Priority to EP04017821A priority patent/EP1505342B1/en
Publication of GB2404693A publication Critical patent/GB2404693A/en
Application granted granted Critical
Publication of GB2404693B publication Critical patent/GB2404693B/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
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/16Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
    • F02M61/18Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
    • F02M61/188Spherical or partly spherical shaped valve member ends
    • 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
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/16Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
    • F02M61/18Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
    • 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
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/16Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
    • F02M61/18Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
    • F02M61/1806Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for characterised by the arrangement of discharge orifices, e.g. orientation or size
    • 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
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/16Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
    • F02M61/18Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
    • F02M61/1806Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for characterised by the arrangement of discharge orifices, e.g. orientation or size
    • F02M61/1833Discharge orifices having changing cross sections, e.g. being divergent
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D11/00Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/36Details, e.g. burner cooling means, noise reduction means
    • F23D11/38Nozzles; Cleaning devices therefor
    • F23D11/386Nozzle cleaning
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D2900/00Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
    • F23D2900/00016Preventing or reducing deposit build-up on burner parts, e.g. from carbon
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D2900/00Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
    • F23D2900/31018Nozzles and cleaning devices therefor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23NREGULATING OR CONTROLLING COMBUSTION
    • F23N2235/00Valves, nozzles or pumps
    • F23N2235/26Fuel nozzles
    • F23N2235/28Spray fuel nozzles

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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

A fuel injector comprises a fuel flow passage about a central axis 2 of the fuel injector, the passage including a valve seat 3 inclined at a first angle a , eg 51 degrees, to the central axis; and a needle orifice 6. The flow passage further comprises a truncated conical volume between the valve seat 3 and the needle orifice 6 and a first edge 9 between the valve seat 3 and the truncated conical volume. The wall 8 of the truncated conical volume is inclined at a second angle b , eg 15 degrees, to the central axis, the second angle being chosen such that fuel flow remains substantially laminar as it passes over the first edge 9. An annulus 10 in a plane perpendicular to the central axis 2 is provided at the base of the truncated conical volume radially outwardly of the needle orifice producing a sharp second edge 11 at the entrance to the needle orifice 6. Fluid passing over the second edge 11 is caused to cavitate whereby deposits in the needle orifice are substantially removed.

Description

2404693
i
A METHOD OF MINIMISING DEPOSITS IN A FUEL INJECTOR
This invention relates to a method of minimising deposits in a fuel injector, in particular for high pressure fuel injector valves.
Much effort has been expended in the design of fuel injectors to achieve a 5 specific flow velocity and desired spray quality. Different stages of a fuel injector valve seat and injection hole are constructed with carefully chosen geometries to achieve this. However, despite all these efforts, the engine performance and emissions are degraded with time due to build up of deposits in the fuel injector and particularly at the fuel injector tip, from exposure to high temperature gases from the combustion 10 chamber.
Various proposals have been made to deal with deposit build-up. US5941208 describes a method of removing coke deposits from a fuel injector nozzle by changing from compression stroke injection to suction stroke injection for a period, so that the deposits are thermally decomposed. EP-1045202 describes a fuel injector in which an 15 air stream is split into two airstreams interspersed with two fuel streams and also provided with air jets to ensure improved fuel-air mixing, and hence clean burning, to prevent coke formation. However, these proposals increase the complexity of the construction and operation of the injectors.
In accordance with a first aspect of the present invention, a method of 20 minimising deposits in a fuel injector comprises providing a fuel flow passage about a central axis of the fuel injector, the passage including a valve seat and a needle orifice; setting the valve seat to be inclined at a first angle to the central axis; providing a first volume between the valve seat and the needle orifice; and a first edge between the valve seat and the first volume; setting a wall of the first volume to be inclined at a 25 second angle to the central axis, the second angle being chosen such that fuel flow remains substantially laminar as it passes over the first edge; providing an annulus at the base of the first volume, radially outwardly of the needle orifice, and a second edge formed between the annulus and the needle orifice; wherein fluid passing over the second edge is caused to cavitate, such that deposits in the needle orifice are 30 substantially removed.
In accordance with a second aspect of the present invention, a fuel injcctor comprises a fuel flow passage about a central axis of the fuel injector, the passage
including a valve seat inclined at a first angle to the central axis; and a needle orifice; wherein the passage further comprises a first volume between the valve seat and the needle orifice; and a first edge between the valve seat and the first volume; wherein a wall of the first volume is inclined at a second angle to the central axis, the second angle being chosen such that fuel flow remains substantially laminar as it passes over the first edge; the passage further comprising an annulus at the base of the first volume, radially outwardly of the needle orifice, and a second edge between the annulus and the needle orifice; wherein fluid passing over the second edge is caused to cavitate, such that deposits in the needle orifice are substantially removed.
The present invention provides a solution to the problems of deposit build up which does not rely on complex methods of operation or construction.
The first volume could be cylindrical, but preferably, the first volume comprises a truncated cone.
Preferably, the first angle is greater than the second angle.
Typically, the wall of the valve seat is between 45° and 51° to the central axis, but preferably, the first angle is 51° to the central axis.
The wall of the first volume may be parallel to the central axis, or at any suitable angle that allows laminar flow, but typically, the second angle is in the range of 13° to 17°, but preferably 15°.
An example of a fuel injector and a method of minimising deposits in accordance with the present invention will now be described with reference to the accompanying drawings in which:
Figure 1 illustrates a conventional fuel injector;
Figure 2 illustrates an example of a fuel injector adapted to remove deposits during operation;
Figure 3 shows an example of a fuel injector according to the present invention;
and,
Figure 4 illustrates relative performance of a conventional fuel injector and the fuel injector of the present invention.
A key parameter influencing rate of deposit formation is surface temperature of the injector tip, so the most straightforward way to control deposits is to maintain the injector tip temperature below the critical deposit forming temperatures, typically
around 120°C, depending upon the fuel composition. However, the injector tip temperature is not just a function of injector design, but also affected by amongst others, combustion system design, head design and engine operating parameters. Thus it is difficult to design an injector which remains cool in all applications.
Another method of preventing deposits is to carefully control the amount of fuel on the tip available to form deposits, through careful control of orifice and tip geometry. The injector tip plays a role in the reaction which forms deposits. Hence the choice of material and surface treatments affect the rate of deposit formation. Another feature is to use inert materials in injector seats.
If the formation of deposits cannot be prevented, then mechanisms are required to remove them. One method of deposit clean up is to coat the tip surfaces with a material of extremely low surface energy. That way, deposits cannot adhere to the surfaces and are easily washed away by the fuel flow. Alternatively, the injectors could be removed and cleaned with specially designed solvents, but this is unacceptable to the user in terms of cost and inconvenience.
The present invention relies on a mechanical effect, using cavitation as to dislodge deposits. Cavitation occurs when there is a change in the velocity of a liquid, which causes a change in pressure of the liquid. Cavities form in the liquid and then collapse as they pass into a region of higher pressure. The present invention makes use of this mechanism by which the fuel flow through the fuel injector acts to overcome the problem of deposit formation, rather than using a separate cleaning step. The cavitation is set up by providing a sharp edge at the needle orifice giving the fuel flow a mechanical advantage in breaking away deposits as they form on the tip face.
Figure 1 illustrates an example of a fuel injector 1 of a conventional type which is effectively a single cone with a hole in the bottom. The included angle of the cone is typically between 90 and 102 degrees, the angle a to the central axis 2 being between 45° and 51°. However, although manufacturing burrs and a high transition cone angle in the needle orifice can produce cavitation, they also reduce production flow yield because the cavitation begins at various stages of needle lift depending on the most minute details of the interface between the transition cone and the orifice hole. As cavitation occurs, the flow through the orifice is reduced due to the vapour content of the fuel. If on a part to part basis, cavitation occurs differently depending on the needle lift, this will introduce a wide variation in dynamic flow of the injectors.
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« • • • ••••
• • « • • • •
4
Fig. 2 illustrates an example of a design of a step cavitating orifice for a fuel injector. A valve seat 3 is provided at an upstream end of the fuel flow, which in this example is positioned at an angle of 51° to the central axis 2. A first edge 4 is formed between the valve seat and a cylindrical volume 5, such that the transition cone of the 5 conventional production zone of Fig. 1 is replaced with a step. At the base of the cylindrical volume is a needle orifice 6 which joins to the volume 5 via a second edge 7. Sudden expansion causes the flow to separate over the first edge 4 and the contraction at the second edge 7 causes the flow to cavitate. The collapse of the cavitation bubbles happens downstream along the needle orifice side, removing 10 deposits. The cavitation relies on the second edge 7 and since the flow contraction is so dramatic, the cavitation does not rely heavily on the condition of that edge. A problem with this design is that there is still variation in flow from part to part, affecting the injector performance.
Fig. 3 illustrates a flat cavitating orifice in a fuel injector according to the 15 present invention. In the previous step design of Fig. 2, the first and second edges 4, 7 are formed by placement of a cylindrical volume between the sealing cone of the valve seat 3 and the orifice 6. In the flat design of the example of Fig.3, an angled wall 8, at an angle (3 to the central axis 2 forming a cone, replaces the vertical wall of the cylinder present in the stepped design. A first edge 9 is formed between the top of the cone 8 20 and the bottom of the valve seat 3. At the base of the cone there is an annulus 10, in a plane perpendicular to the central axis 2 and a sharp, second edge 11 at the entrance to the orifice 6. The annulus has a maximum diameter which reaches, but does not encroach on the sealing diameter.
The fuel injector has the feature that the fuel flow passage induces cavitation as 25 soon as possible, as the flow accelerates through it. Furthermore, the present invention gives a manufacturable design that will induce cavitation in a repeatable way. The principle behind this design is to reduce or eliminate the separation off the first edge by making the expansion less sudden, while still providing the second edge at the entrance to the needle orifice. As in the step design, the second edge provides a sudden 30 contraction to induce cavitation. By reducing the amount of flow separation from the first edge, there will be less variation in flow from part to part.
Prototype injectors with angle (3 equal to 15° +/- 2° have been manufactured and tested. The results are shown in Fig. 4. Each point represents percentage change in
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5
injector fuel flow at the end of a 6 hour test. The tests are performed at different engine conditions to give the respective injector tip temperatures. The baseline injectors shift lean due to deposit formation and the step injectors have a slight rich shift due to a mechanical durability shift. The results of Fig. 4 indicate that the flat cavitating orifice 5 of Fig. 3 is effective at removing deposits as they form, as the optimum result is to have no change in fuel flow. As the orifice plugs with deposits the flow will increase. The percentage change for the baseline example indicates a noticeably greater reduction in flow than in the present invention.
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6

Claims (10)

CLAIMS 1. A method of minimising deposits in a fuel injector, the method comprising providing a fuel flow passage about a central axis of the fuel injector, the passage including a valve seat and a needle orifice; setting the valve seat to be inclined at a first 5 angle to the central axis; providing a first volume between the valve seat and the needle orifice; and a first edge between the valve seat and the first volume; setting a wall of the first volume to be inclined at a second angle to the central axis, the second angle being chosen such that fuel flow remains substantially laminar as it passes over the first edge; providing an annulus at the base of the first volume, radially outwardly of the 10 needle orifice, and a second edge formed between the annulus and the needle orifice; wherein fluid passing over the second edge is caused to cavitate, such that deposits in the needle orifice are substantially removed. 2. A method according to claim 1, wherein the first volume comprises a truncated 15 cone. 3. A method according to claim 1 or claim 2, wherein the first angle a is 51°. 4. A method according to any preceding claim, wherein the second angle (3 is 15°. 20 5. A fuel injector, the injector comprising a fuel flow passage about a central axis of the fuel injector, the passage including a valve seat inclined at a first angle to the central axis; and a needle orifice; wherein the passage further comprises a first volume between the valve seat and the needle orifice; and a first edge between the valve seat 25 and the first volume; wherein a wall of the first volume is inclined at a second angle to the central axis, the second angle being chosen such that fuel flow remains substantially laminar as it passes over the first edge; the passage further comprising an annulus at the base of the first volume, radially outwardly of the needle orifice, and a second edge between the annulus and the needle orifice; wherein fluid passing over the second edge 30 is caused to cavitate, such that deposits in the needle orifice are substantially removed. 6. A fuel injector according to claim 5, wherein the first volume comprises a truncated cone. I 7. A fuel injector according to claim 5 or claim 6, wherein the first angle is greater than the second angle. 8. A fuel injector according to any of claims 5 to 7, wherein the second angle is 15°+/-2°. % Amendments to the claims have been filed as follows CLAIMS
1. A method of minimising deposits in a fuel injector, the method comprising providing a fuel flow passage about a central axis of the fuel injector, trie passage including a vaive seat and a needle orifice; setting the valve seat to be inclined at a first angle to the central axis; providing a first volume between the valve seat and the needle orifice; and a first edge between the valve seat and the first volume; setting a wall of the first volume such that fuel flow remains substantially laminar as it passes over the first edge; providing an annulus at the base of the first volume, radially outwardly of the needle orifice, and a second edge formed between the annulus and the needle orifice; wherein fluid passing over the second edge is caused to cavitate, such that deposits in the needle orifice are substantially removed.
2. A method according to claim 1, wherein the wall of the first volume is inclined at a second angle to the central axis.
3. A method according to claim 1 or claim 2, wherein the first volume comprises a truncated cone.
4. A method according to any preceding claim, wherein the first angle a is 51 °.
5. A method according to any of claims 2 to 4, wherein the second angle p is 15°.
6. A fuel injector, the injector comprising a fuel flow passage about a central axis of the fuel injector, the passage including a valve seat inclined at a first angle to the central axis; and a needle orifice; wherein the passage further comprises a first volume between the valve seat and the needle orifice; and a first edge between the valve seat and the first volume; wherein a wall of the first volume is chosen such that fuel flow remains substantially laminar as it passes over the first edge; the passage further comprising an annulus at the base of the first volume, radially outwardly of the needle orifice, and a second edge between the annulus and the needle orifice; wTherein fluid passing over the second edge is caused to cavitate, such that deposits in the needle orifice are substantially removed.
7. A fuel injector according to claim 6, wherein the wall of the first volume is inclined at a second angle to the central axis.
8. A fuel injector according to claim 6 or claim 7. wherein the first volume 5 comprises a truncated cone.
9. A fuel injector according to claim 7 or claim 8, wherein the first angle is greater than the second angle.
10. A fuel injector according to any of claims 7 to 9, wherein the second angle is 15°+/- 2°.
10
GB0318164A 2003-08-04 2003-08-04 A method of minimising deposits in a fuel injector Expired - Fee Related GB2404693B (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB0318164A GB2404693B (en) 2003-08-04 2003-08-04 A method of minimising deposits in a fuel injector
EP04017821A EP1505342B1 (en) 2003-08-04 2004-07-28 A method of minimizing deposits in a fuel injector

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0318164A GB2404693B (en) 2003-08-04 2003-08-04 A method of minimising deposits in a fuel injector

Publications (3)

Publication Number Publication Date
GB0318164D0 GB0318164D0 (en) 2003-09-03
GB2404693A true GB2404693A (en) 2005-02-09
GB2404693B GB2404693B (en) 2005-06-22

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Family Applications (1)

Application Number Title Priority Date Filing Date
GB0318164A Expired - Fee Related GB2404693B (en) 2003-08-04 2003-08-04 A method of minimising deposits in a fuel injector

Country Status (2)

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EP (1) EP1505342B1 (en)
GB (1) GB2404693B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10358726B4 (en) * 2003-12-15 2020-02-06 Robert Bosch Gmbh Fuel injector
US10465643B2 (en) 2014-07-31 2019-11-05 Cummins Inc. Method for reducing carbon/coke in fuel injectors in dual fuel applications

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH10281041A (en) * 1997-04-01 1998-10-20 Mitsubishi Heavy Ind Ltd Fuel injection valve
US20020030124A1 (en) * 1999-04-27 2002-03-14 Siemens Automotive Corporation Coating for a fuel injector seat

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2441733A1 (en) * 1978-11-17 1980-06-13 Innota Innovation Tech Avancee ELECTROMAGNETIC INJECTORS AND METHODS OF MAKING THE SAME
DE3714693A1 (en) 1987-05-02 1988-11-10 Bosch Gmbh Robert ELECTROMAGNETICALLY ACTUABLE VALVE
DE19527049A1 (en) 1995-07-25 1997-01-30 Bosch Gmbh Robert Fuel injector
DE19645383B4 (en) 1996-11-04 2004-04-29 Daimlerchrysler Ag Method for operating an Otto internal combustion engine with internal mixture formation
DE19841192A1 (en) * 1998-09-09 2000-03-16 Bosch Gmbh Robert Fuel injection valve for internal combustion engines
US6715292B1 (en) 1999-04-15 2004-04-06 United Technologies Corporation Coke resistant fuel injector for a low emissions combustor
FR2851792B1 (en) * 2003-02-28 2007-02-09 Magneti Marelli Motopropulsion FUEL INJECTOR FOR INTERNAL COMBUSTION ENGINE

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH10281041A (en) * 1997-04-01 1998-10-20 Mitsubishi Heavy Ind Ltd Fuel injection valve
US20020030124A1 (en) * 1999-04-27 2002-03-14 Siemens Automotive Corporation Coating for a fuel injector seat

Also Published As

Publication number Publication date
GB2404693B (en) 2005-06-22
EP1505342B1 (en) 2012-03-07
EP1505342A1 (en) 2005-02-09
GB0318164D0 (en) 2003-09-03

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