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Title:
FUEL INJECTOR WITH CLOSED LOOP DETECTION
Document Type and Number:
WIPO Patent Application WO/2020/025262
Kind Code:
A1
Abstract:
A nozzle assembly of a fuel injector comprises a nozzle with a body extending along a main axis, in which a needle (30) is axially moveable between a closed position, in which a first end (34) of said needle rests on a valve seat to prevent fuel injection through one or more injection orifices of said nozzle, and an open position in which said needle is lifted from said seat to allow injection. The needle extends along a needle axis (A) and has an overall shape with symmetry of revolution about the needle axis (A). The needle comprises a shaft portion (32) which is tapered at the first end (34) and defines an annular seating face (44) cooperating with a seating face on the valve seat. The needle assembly further includes a detection circuit in which said needle forms a switch. The needle (30) is designed to include a local dissymmetry (59) in the region of the annular seating face (44), which is configured to cause, in use, an unbalance of forces resulting in a transversal force exerted by the fuel about the needle first end (34).

Inventors:
COCHET THIERRY (FR)
MEISSONNIER GUILLAUME (FR)
LAURENT ALEXIS (FR)
TAPIN CHRISTOPHE (FR)
BERLEMONT JEAN-FRANÇOIS (BE)
VIT ROMAIN (FR)
Application Number:
PCT/EP2019/068279
Publication Date:
February 06, 2020
Filing Date:
July 08, 2019
Export Citation:
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Assignee:
DELPHI TECH IP LTD (BB)
DELPHI FRANCE SAS (FR)
International Classes:
F02M47/02; F02M51/00; F02M57/00; F02M61/12; F02M61/18; F02M65/00
Domestic Patent References:
WO2017167627A12017-10-05
WO2017167627A12017-10-05
Foreign References:
EP3208456A12017-08-23
EP1283336A22003-02-12
Attorney, Agent or Firm:
DELPHI FRANCE SAS (FR)
Download PDF:
Claims:
CLAIMS:

1. A nozzle assembly of a fuel injector comprising:

a nozzle (12) with a body (24) extending along a main axis, said body having a peripheral wall (26) and defining an internal bore (28) in which a needle (30) is axially moveable between a closed position, in which a first end (34) of said needle rests on a valve seat to prevent fuel injection through one or more injection orifices (20) of said nozzle, and an open position in which said needle is lifted from said seat to allow injection;

wherein said needle extends along a needle axis (A) and has an overall shape with symmetry of revolution about said needle axis (A), said needle comprising a shaft portion (32) which is tapered at said first end (34) and defines an annular seating face (44) cooperating with a seating face (46) on said valve seat;

wherein said nozzle assembly further includes a detection circuit in which said needle forms a switch;

characterized in that said needle is designed to include a local dissymmetry (59) in the region of said annular seating face (44), which is configured to cause, in use, an unbalance of forces resulting in a transversal force exerted by the fuel about said needle first end (34) and, wherein said tapering first end includes an intermediate section (34.1 ) connected at one end to said needle shaft portion (32) and at the other end to a conical section (34.2) defining said annular seating face (44).

2. The nozzle assembly as claimed in claim 1 , wherein said conical section (34.2) is configured to define a contact line (60) in a plane substantially perpendicular to said needle axis (A) and wherein said local dissymmetry (59) is located adjacent said contact line, on the side of said intermediate section (34.1 ).

3. The nozzle assembly as claimed in claim 2, wherein said conical section (34.2) has circular symmetry about said needle axis (A) except over a predetermined angular section that is less than 180°.

4. The nozzle assembly as claimed in claim 3, wherein said predetermined angular section is in the range of 20 to 90°, in particular 35 to 60°.

5. The nozzle assembly as claimed in claim 3 or 4, wherein said local dissymmetry is formed by a truncated peripheral portion of said conical section, for example removed by machining.

6. The nozzle assembly as claimed in claim 5, wherein said conical section comprises a further truncated peripheral portion on the opposite side of said contact line.

7. The nozzle assembly as claimed in claim 1 , wherein said conical section (234.2) is configured to define a contact line (260) in a plane tilted with respect to said needle axis (A) and the outer shape of said tapered tip is defined, above said contact line, by a generatrix parallel to said needle axis and following said contact line.

8. The nozzle assembly as claimed in claim 1 , wherein said intermediate section (334.1 ) and said conical section (334.2) have an axis of symmetry referred to as tip axis (B) that is parallel to said needle axis (A) and offset therefrom.

9. The nozzle assembly as claimed in claim 8, wherein said intermediate section and said conical section have circular symmetry about said tip axis.

10. The nozzle assembly as claimed in any one of the preceding claims, wherein said needle shaft (32) has a symmetry of revolution about axis (A); and preferably comprises at least one collar member (46) that has a symmetry of revolution about axis (A) or about a plane passing through axis (A).

1 1 . A fuel injector comprising a nozzle assembly as claimed in any one of the preceding claims.

Description:
FUEL INJECTOR WITH CLOSED LOOP DETECTION

FIELD OF THE INVENTION

The present invention generally relates to the field of fuel injection, in particular in internal combustion engines. The invention more particularly relates to fuel injectors featuring a closed loop detection function enabling detection of needle opening or closing.

BACKGROUND OF THE INVENTION

In a diesel fuel injector, the displacements of a valve member, or needle, between an open position and a closed position enable, or forbid, fuel injection through spray holes provided in the nozzle body of the injector. The needle is an elongated shaft-like member extending from a head portion, protruding in a control chamber, to a pointy extremity provided with a (moving) seating face that cooperates with a (fixed) seating face integral to the nozzle body. The needle is slidably guided in the nozzle body and, in closed position the moving seating face is in sealing contact against the fixed seating face closing fluid communication to the spray holes and thus forbidding fuel injection. In open position the moving seating face is lifted away from the fixed seating face thus opening said fluid communication and enabling fuel injection through the spray holes.

In order to comply with emissions standards, a proper operation of a fuel-injected engine requires that the fuel injectors and their controller allow for a timely, precise and reliable fuel injection, whatever the operating condition and during all injector lifecycle.

It is now known that major improvement in the control of fuel injection equipment and of the injection event is obtained with a so called closed-loop control method. WO2017/167627, for example, discloses a fuel injector designed with a switch function for detecting needle opening and closing. The needle is axially guided in its upper region by a guide member that is set to a predetermined electric potential. The needle is mounted in the nozzle body so as to be able to move therein while being electrically isolated from the nozzle body, except for the region of the nozzle body seat, so that the needle is in electric contact with the nozzle body only in closed position.

More generally, closed loop control methods are typically executed by an electronic control unit (ECU) that controls the operation of the fuel injection equipment and in particular the control valve of the fuel injector. Depending on embodiments, the close loop means enable for an electrical signal to be measured at a specific value when the needle gets in closed position, or the signal can also take a specific value when the needle is in fully open position. Overall, the closed loop detection functions permits determining the opening time, and thus estimating the injected fuel quantity which is dependent on needle opening time and fuel pressure.

It has been observed that certain operating conditions may cause an erroneous detection of the needle opening. During early opening of the needle (i.e. within the first few microns of lift), cavitation may appear between the needle and the nozzle seat, leading to a hesitating electrical contact. Sometimes, the distance between the needle tip and valve seat is sufficient to open the electric link. Sometimes the distance is insufficient and the electric link remains closed due to the electric field. Still another possibility is that the needle tip deviates from its axis to be in contact with the seat, so that the electric link is closed. These phenomena are thus at the origin of an unstable switching signal.

OBJECT OF THE INVENTION

The object of the present invention is to provide a fuel injector of improved design, wherein a stable closed loop detection signal is ensured. This object is achieved by a fuel injector as claimed in claim 1 .

SUMMARY OF THE INVENTION

According to the present invention, a nozzle assembly for a fuel injector comprises a nozzle with a body extending along a main axis, the body having a peripheral wall and defining an internal bore in which a needle is axially moveable between a closed position, in which a first end of the needle rests on a valve seat to prevent fuel injection through one or more injection orifices of the nozzle, and an open position in which the needle is lifted from its seat to allow injection.

The needle extends along a needle axis (A) and has an overall shape with symmetry of revolution about the needle axis (A), the needle comprising a shaft portion which is tapered at the first end and defines an annular seating face cooperating with a seating face on the valve seat.

The needle assembly further includes a detection circuit in which the needle forms a switch.

It shall be appreciated that the needle is designed to include a local dissymmetry in the region of the annular seating face, which is configured to cause, in use, an unbalance of forces resulting in a transversal force exerted by the fuel about the needle’s first end.

The local dissymmetry will come in play at the beginning of the needle opening stroke. During the first microns of needle lift, the needle tip is still in the vicinity of the nozzle seating face and will be pushed transversally/radially (in a given direction) due to the imbalance of forces. The needle tip will thus remain in contact with the nozzle seating face until the needle stroke is sufficient. That is, the needle tip is forced, by the design of the dissymmetry, to remain in contact with the nozzle seating face. A clean electric contact can thus be obtained and the opening time can be more reliably detected. As used herein, the term “symmetry of revolution” is used in its conventional meaning, and is equivalent to“circular symmetry”. The needle axis is thus an axis of revolution of the needle.

Advantageously, the tapering first end includes an intermediate section connected at one end to the needle shaft portion and the other end to a conical section defining the annular seating face. The conical section is generally the very end section of the needle. Although referred to as conical section, it may be truncated, i.e. without the apex. In embodiments, the conical section may include two or more sections with different cone angles.

The conical section includes the needle seating face and is configured to define a contact line, which is the line along which the sealing contact will form against the nozzle seating face in closed position.

In a first embodiment, the contact line lies in a plane substantially perpendicular to the needle axis (A) and the local dissymmetry is adjacent the contact line. The local dissymmetry may be provided above and/or below the contact line, but does not cross the contact line. When there are two local dissymmetries, they may be angularly aligned.

Preferably, the local dissymmetry is adjacent the contact line, on the side of the intermediate section. The local dissymmetry may extend to the intermediate section.

Typically, the conical section has circular symmetry about the needle axis (A) except over a predetermined angular section that is less than 180°. Preferably, the predetermined angular section is in the range of

20 to 90°, in particular 35 to 60°.

The local dissymmetry may be formed by a truncated peripheral portion of the conical section, for example removed by machining.

In this embodiment, the local dissymmetry is thus designed as an interruption of the outer circumference of the conical section. The conical section has a symmetrical cross-section profile (in particular circular symmetry), but the local dissymmetry interrupts that symmetry, resulting in an unbalanced cross-section.

The needle shaft generally has a symmetry of revolution about axis (A). It may comprise one or more collar members that have a symmetry of revolution about axis or about a plane passing through axis.

In the first embodiment, the term“local dissymmetry” only concerns a part of the circumference of the conical section. However the local dissymmetry may extend to the whole first end of the needle. Compared to the needle axial extent, it can still be called“local”.

In this context, in a second embodiment, the conical section is configured to define a contact line in a plane tilted with respect to the needle axis (A) and the outer shape of the tapered tip is defined, above the contact line, by a generatrix parallel to the needle axis and following the contact line.

In a third embodiment, the intermediate section and the conical section have an axis of symmetry referred to as tip axis (B) that is parallel to the needle axis (A) and offset therefrom. The intermediate section and the conical section have circular symmetry about the tip axis.

According to another aspect, the invention concerns a fuel injector for an internal combustion engine comprising the herein disclosed nozzle assembly.

BRIEF DESCRIPTION OF THE DRAWINGS The present invention will now be described, by way of example, with reference to the accompanying drawings, in which:

Figure 1 : is a cross-section view through a fuel injector comprising a nozzle assembly according to a first embodiment of the invention;

Figure 2: is a perspective view of the tip region of the needle; Figures 3 and 4: are close-up views of the needle tip;

Figure 5: is a principle diagram of a conventional needle;

Figure 6: is a principle diagram of an injector needle according to a second embodiment shown (a) as side view and (b) a view from below; and

Figure 7: is a principle diagram of an injector needle according to a third embodiment.

DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS In reference to Figure 1 is now described a diesel fuel injector 10 having a general elongated shape extending along a main axis A and comprising, from bottom to top, a nozzle assembly 12, a control valve assembly 14 and an actuator assembly 16. These assemblies are fixed to each other via a capnut 15. The details of the actuator assembly 16 and control valve assembly 14 are known in the art and are not shown in the figures, being simply indicated by boxes.

The injector 10 defines an internal high pressure fuel circuit 18 comprising several segments and extending from an inlet section 18 provided in the upper part of the injector to spray holes 20 arranged in a lower spray extremity 22 drawn at the very bottom of the injector 10.

The nozzle assembly 12 comprises a nozzle body 24 having a peripheral wall 26 defining an inner bore 28 in which is slideably arranged a needle 30, forming the valve member, and adapted to translate along the main axis A between a closed position CP and an open position OP.

The needle valve member 30 has an elongated shaft core 32 extending (along needle axis concentric with axis A) between a top head end 33 and a lower end with a tapered tip 34. In between the ends, the needle 30 is provided with a radially protruding collar member 36 that extends toward a circular edge that lies close to the inner face of the inner bore 28 of the nozzle body 26. The collar member 36 divides the inner bore 28 into an upstream chamber 38 and a downstream chamber 40 and, a permanently open fluid communication is defined between these chambers by at least one restricted aperture provided in the collar member 36, or at the periphery of it or, along the circular edge. Reference sign 42 designates a guide collar similar to collar member 36 to guide the needle 30 in the lower region of bore 28.

The spray extremity 22 is the arrangement of the tapered end 34 of the needle defining a male needle seating face 44 cooperating with a corresponding female nozzle seating face 46 defined on the inner face of the nozzle body 24. The needle seating face 44 is also said to be mobile because it moves with the needle, whereas the nozzle seating face 46 is referred to as fixed seating face. In the spray extremity 22, the inner bore 28 that is cylindrical, downwardly narrows forming said female nozzle seating face 46 ending in a small sac 48 wherefrom depart the spray holes 20 extending through the peripheral wall 26 of the nozzle body 24.

As is known in the art, in the closed position (CP) of the needle 30 - illustrated in Fig.1- the male seating face 44 rests sealingly on the female seating face 46 and fuel flow towards the spray orifices 20 is prevented. An opening position (OP) of the needle 30 is a position where the needle 30 is off the valve seat, i.e. there is a space between the male seating face 44 and female seating face 46, whereby fuel can flow through this space downstream of the valve seat to the spray orifices 20, so that fuel is sprayed at the injector tip into the combustion chamber.

Actuation of the needle 30 is performed by energizing the actuator assembly 16, typically a solenoid that acts on a valve member of the control valve assembly 14. The control valve assembly 14 is conventionally connected with a control chamber 50 at the top of the nozzle assembly 12, in which the needle head 33 (opposite tip 34) protrudes. Energizing the actuator 16 will thus cause triggering of the control valve (connected to a mobile armature of the solenoid actuator) that will open an escape path for fuel out of control chamber 50. This will cause a decrease of pressure in the control chamber 50, whereby needle 230 will move upward into the control chamber in OP and thus open the valve seat. This principle of operation is well known.

Fuel injector 10 further comprises a detection circuit for detecting needle opening and closing, which is also referred to as closed loop. In the present embodiment, this is achieved by a simple switch function. The needle 30 is axially guided in its upper region by a guide member 54 that is set to a predetermined electric potential. The guide member 54 has an axial bore in which the needle head 33 is received. The needle 30 is mounted in the nozzle body 24 so as to be able to move therein while being electrically isolated from the nozzle body 24, except for the region of the nozzle body seat 46, so that the needle 30 is in electric contact with the nozzle body 24 only in CP. The needle 30 is electrically insulated from the body 24 by means of insulating sheeting or coatings indicated 56 provided at the collars 40, 42 and at the interface with the guide member 54.

When the needle is in CP, the circuit is closed and an electric current can flow from the upper guide 56 through the length of the needle 30 to pass into the body 24 at the needle tip in contact with the female seating face 46. This detection circuit and flow path is indicated by line 58 in Fig .1. When the needle 30 is in OP, the detection circuit is open and no current can flow to the body 24. There, in CP the voltage may thus be 0 V whereas in OP the circuit is open a predetermined voltage, e.g. 5 V, is measured. This is only one way of performing closed loop detection and a variety of voltages and designs may be used, e.g. including detection of the fully open needle position, as will be clear to those skilled in the art.

In order to ensure a clean electric contact at opening or closing of the needle 30, the needle 30 is designed to include a local dissymmetry in the region above the male seating face 44. The local dissymmetry is configured to cause, in use, a transversal force exerted by the fuel in the region of the needle tip 34.

The needle tip 34 is shown in more details at Figs. 2 to 4. It may be noted that a general rule of design of an injector needle is to have an overall symmetrical shape in order to maintain balance of the opening forces and to avoid lateral forces applied to the needle. This is the case in the present embodiment and the needle 30 has an overall symmetrical shape. In particular the core shaft 32 exhibits a symmetry of revolution (i.e. circular symmetry) about the needle axis A. Depending on the embodiments, this may also be the case for the annular collars 36, 42. In other embodiments, as is the case here, the collar members 36 and 42 may not have an axial symmetry but a symmetry with respect to a plane passing through the needle axis A, still chosen to maintain a proper balance of forces.

It will be noticed that at the lower end of needle 30, the core shaft 32 terminates with the tapering end 34 which comprises an intermediate section 34.1 followed by a conical section 34.2.

The intermediate section 34.1 and conical section 34.2 generally have circular symmetry about axis A, except for a certain portion of the periphery at 59 that is modified to provide a local dissymmetry configured to cause, in use, a transversal force (in a given direction) exerted by the fuel about the needle tip 34.

In this first embodiment, the local dissymmetry 59 is obtained by machining (milling or grinding) a part of the outer periphery of the conical section 34.2. The conical section 34.2 is initially a cone, or more precisely a cone with truncated apex, and the milling thus results in an interruption of the axial symmetry of the conical section 34.2.

In other words, the conical section 34.2 has a symmetry of revolution about axis A (i.e. a circular cross-section) except over a predetermined angular section that may be generally in the range of 35° to 60°. As is known, although the male and female seating faces 44 and 46 have a certain axial extent, in the CP the configuration is such that there is a continuous, circumferential contact line that forms the actual sealing contact between the seating faces. In fig .4 the contact line on the male seating face 44 is represented by dashed line 60.

It may be noted that the local dissymmetry is provided on the male seating face 44 of the needle 30, above the contact line 60 (adjacent thereto on the side of the intermediate section 34.1 ). When the needle is in CP, this local dissymmetry does not have any effect. However, the local dissymmetry causes, at opening, an unbalance of forces on the needle tip that results in a transversal/radial force. This will impact the injector operation at the very beginning of the needle opening, i.e. within the first microns of the lift-off stroke. Due to the transversal forces, the needle is pushed on the side and remains in contact with the female seating face.

This design thus promotes the contact between the needle tip 34, precisely the conical section 34.2, and the female seating face 46, thereby avoiding oscillations or random needle behavior that may be observed under certain conditions. The needle tip 34 is forced to remain in contact with the female seat 46 until it has been sufficiently lifted. Accordingly, the seat detection circuit remains closed during this initial period, leading to a stable electric signal.

It may be noted that the local dissymmetry may extend into the the intermediate section 34.1 , as seen in Figs 3 and 4. This is due here to the use of the grinding tool that attacks the conical section 34.2 parallel to axis A.

In embodiments, the conical tip 34.2 may comprise several conical sections along axis A with different angles. This is e.g. the case in this embodiment where the cone angle of the section downstream (on the right) of the contact line 60 is larger than the upstream one (on the left). In some embodiments, the conical section 34.2 may also be configured with a local dissymmetry in the region below of the contact line 60 (towards the free end). Such dissymmetry should correspond angularly to the one above the contact line 60. The additional dissymmetry will promote flow on one side of the needle at opening and hence increase the transversal force on the needle.

The local dissymmetry is here obtained by an interruption in the circular outer shape of the conical section, over a minor part of the circumference. The needle being typically made in one piece, it is a solid of revolution and the dissymmetry is obtained here by removing material at one location of the periphery. The aim is to modify the outer shape of the intermediate section to cause an unbalance of forces that pushes the needle in one direction. In general the intermediate section will thus have, over at least part of its length, a circular cross-section except at the position of the removed material 59 at the tip, preferably just above contact line 60.

Those skilled in the art may devise other shapes to generate a transverse force at the needle tip. Cross-sections differing from a circle but retaining some symmetry and thus keeping force balance such as e.g. strict elliptical or polygonal shapes are thus to be avoided, unless they are modified with a flattened portion as described above.

Two further embodiments are represented in Figs. 6 and 7, and will be explained with comparison to Fig .5, which illustrates the conventional needle design. In Fig.5 one will recognize a conventional needle 130 having a shaft core 132 with tapering end 134 extending along a main axis A. The tapering end includes an intermediate section 135.1 extending between the core end and a conical section 135.2. The needle has a symmetry of revolution about axis A. Intermediate section 135.1 and conical section 135.2 are also symmetrical about axis A; they have a strictly circular cross-section in a plane perpendicular to axis A, this over their entire axial extent. In the embodiment of Fig.6, the needle 230 has a core 232 with a symmetry of revolution about axis A. This is however not the case for the intermediate section 232.1. In fact, in this embodiment the seat line 260 is configured to be tilted relative to the needle axis A. The outer shape of the tapering end 234 is made, above the seat line, based on a generatrix parallel to axis A and following the seat line 60 (which thus forms the directrix). The region of the conical section 234.2 is thus symmetrical below the seat line, with a circular cross-section. However the transition section does not have a circular cross-section. In the view from below the dotted circle represents the cross-section of a circular intermediate section as in Fig. 5. Here however the design of a needle tip 234 results in an dissymmetric intermediate section 234.1. The dashed surface 259 represents the removed portion compared to a circular design.

Compared to the embodiment of Fig.5, there is more horizontal surface on the right of intermediate section 234.1 (i.e. the surface 259) and a larger vertical surface on the right as well. This leads to an imbalance of forces acting on the needle 230 that will push the needle tip 234 to the left, as indicated by the arrow in Fig.6 a).

In the embodiment of Fig.7, the tapering end 334 has been offset from the main axis A of needle 330. The shaft core 332 has a symmetry of revolution about axis A. The intermediate section 334.1 and conical section 334.2 have a symmetry of revolution about an axis B parallel to axis A but offset therefrom. Here again, there is more surface at the core bottom 332.1 on the right of intermediate section 334.2 than on the left, which at opening of the needle 330 will cause transversal forces on the needle tip 334 pushing the needle towards the left (as indicated by the arrow).