EP1715177B1 - Piezoelectric actuator for the operation of an injection pump for internal-combustion engines, and injector-pump assembly employing said actuator - Google Patents

Piezoelectric actuator for the operation of an injection pump for internal-combustion engines, and injector-pump assembly employing said actuator Download PDF

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Publication number
EP1715177B1
EP1715177B1 EP20060112774 EP06112774A EP1715177B1 EP 1715177 B1 EP1715177 B1 EP 1715177B1 EP 20060112774 EP20060112774 EP 20060112774 EP 06112774 A EP06112774 A EP 06112774A EP 1715177 B1 EP1715177 B1 EP 1715177B1
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Prior art keywords
actuator
rigidity
spring
piezoelectric
combustion engines
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EP20060112774
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German (de)
French (fr)
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EP1715177A1 (en
Inventor
Pierluigi Dell'orto
Pasquale Grassia
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Dell Orto SpA
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Dell Orto SpA
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    • 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
    • F02M51/00Fuel-injection apparatus characterised by being operated electrically
    • F02M51/04Pumps peculiar thereto
    • 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
    • F02M57/00Fuel-injectors combined or associated with other devices
    • F02M57/02Injectors structurally combined with fuel-injection pumps
    • F02M57/022Injectors structurally combined with fuel-injection pumps characterised by the pump drive
    • F02M57/027Injectors structurally combined with fuel-injection pumps characterised by the pump drive electric
    • 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
    • F02M59/00Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps
    • F02M59/02Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps of reciprocating-piston or reciprocating-cylinder type
    • F02M59/10Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps of reciprocating-piston or reciprocating-cylinder type characterised by the piston-drive
    • 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
    • F02M2200/00Details of fuel-injection apparatus, not otherwise provided for
    • F02M2200/21Fuel-injection apparatus with piezoelectric or magnetostrictive elements

Definitions

  • the present invention falls in the sector of fuel supply systems in internal combustion engines. More in particular, the present invention refers to a piezoelectric actuator for the operation of an injection pump of internal combustion engines and to the injector-pump assembly employing said actuator.
  • the present invention proposes to identify an injection system alternative to the ones already proposed, based on an actuator of a piezoelectric type, and such as to allow increased injectable flow rates per cycle, over known systems, given equal dimensions of the actuator and an improved reaction to high operation rpm. It is here reminded that three pump-injector systems are compared in the known art: with an actuator acting on a centrally-loaded membrane, or acting on an annular-load membrane, or piston pump-actuator systems.
  • the object of the present invention is hence to obtain an improvement of the performance of a piston pump-injector system with piezoelectric actuator, essentially by adopting means capable of amplifying the useful run of the piezoelectric actuator.
  • a piezoelectric actuator has a linearly decreasing load/deformation feature. That is to say, at a set supply voltage (phantom lines for 0 V., for 80 V. and for 160 V., respectively), this type of actuator is capable of developing large loads with small piston displacements, but loses its thrust capability as the run increases, down to zero thrust when the maximum idle displacement is reached.
  • the actual feature of the piezoelectric actuator does not perfectly suit the application thereof as a hydraulic pumping element, because the latter one requires the exertion of a constant force throughout the entire compression run. Instead, it has not been possible yet to use the full nominal run of the piezoelectric element, because, as seen with respect to the diagram of fig. 2 , in the final part of the run the loading capability necessary to overcome fluid pressure would not be provided.
  • the piezoelectric actuator cannot exert a force which remains constant throughout the entire work run ⁇ L o , it is provided, according to a first aspect of the present invention, to adopt a compromise between run and load, making use of a part only of the actual total work run. In other words, it is provided to use the piezoelectric element with an average run and an average load. It is possible to prove that this is the best solution, i.e. the one which allows to obtain the maximum work per cycle; as a matter of fact, in such solution the largest quantity of energy is delivered between the one available per work cycle.
  • the piezoelectric material of which commercial actuators are made further has the feature - common to all ceramic materials - of displaying an asymmetric mechanical behaviour in the presence of tensile and compressive stresses; in particular, tensile behaviour is poor, whereas the compressive one is acceptable for applications as actuator, both in static and in dynamic conditions.
  • a preload (assumed to be rigidly constant) does not affect the performance of the actuator, determining only a translation of the work cycle in the plane of fig. 2 , i.e. bringing the work cycle inside the positive half-plane (compressive stress) of the load; thereby, a safety margin is accomplished which serves to safeguard the piezoelectric element from the dynamic tensile actions which are generated during fast operation and which must be neutralised precisely by the presence of the preload.
  • a negative-rigidity spring i.e. a spring supplying a decreasing preload as deformation increases.
  • An actuator deficiency is thereby countered by the special feature of the spring, i.e. the capability of providing high loads only at the beginning of the run.
  • the embodiment comprising springs having a negative rigidity of -9.5 N/ ⁇ m, although theoretically possible, is of no practical usefulness.
  • the diagram gradient of fig. 2 albeit limited to the middle portion where the derivative takes up the absolute minimum value, it would be necessary to resort to diameters of 800 mm with thicknesses of 20 mm.
  • These dimensions are evidently not admissible for use in internal combustion engines, in particular those intended for motor bicycles. The problem has therefore arisen of how to manufacture a spring featuring maximum negative rigidity with the smallest dimensions.
  • a spring capable of providing maximum negative rigidity with respect to material resistance, having dimensions compatible with its application in internal combustion engines.
  • the rigidity thus obtained for the spring dimensioned as above is then doubled with two springs arranged packetwise and further amplified arranging in series a conventional spring with a rigidity of 1,15 N/ ⁇ m.
  • a piezoelectric pump-injector particularly suited to small-powered internal combustion engines - having for example a swept volume of 50 cm 3 - can be manufactured, according to the present invention, also employing a small, inexpensive piezoelectric element such as the Epcos one (table of fig. 1 ), in association with a preload spring having a negative rigidity whose modulus is about half that of the piezoelectric element.

Description

  • The present invention falls in the sector of fuel supply systems in internal combustion engines. More in particular, the present invention refers to a piezoelectric actuator for the operation of an injection pump of internal combustion engines and to the injector-pump assembly employing said actuator.
  • Supply systems are widely known, in particular for the supply of fuel injectors; they generally use controlled alternative pumps, also called vibrating pumps, which are based on the use of an actuator in the shape of a piston of ferromagnetic material controlled by an electromagnet supplied with alternate current. One of these pumps is described for example in patent MARELLI EP-0.953.764 , which concerns, however, the oil supply in a two-stroke engine. Another example is described in US 6 079 636 .
  • The present invention proposes to identify an injection system alternative to the ones already proposed, based on an actuator of a piezoelectric type, and such as to allow increased injectable flow rates per cycle, over known systems, given equal dimensions of the actuator and an improved reaction to high operation rpm. It is here reminded that three pump-injector systems are compared in the known art: with an actuator acting on a centrally-loaded membrane, or acting on an annular-load membrane, or piston pump-actuator systems.
  • It is evident from the results of the studies carried out on these systems that, in terms of deliverable fuel flow rate per stroke, in ideal conditions (perfectly uncompressible fluid, absence of blow-by, infinitely rigid container, ideal valves), the volume of injectable fluid, in the case of a piston pump-injector, may be obtained through the following mathematical expression: Δ V max = F z b f Δ L 0 4 Δ p
    Figure imgb0001

    wherein ΔVmax = injectable fuel volume per cycle;
    ΔL0 = idle displacement of the actuator;
    Δp = difference between injection pressure and supply pressure
    Fzbf = load which may be developed by the actuator at the maximum voltage, locked between two non-yielding restraints (Zero Blocking Force)
  • By applying formula (1) to the case of piezoelectric actuators available on the market with a reference pressure of 75 bar, very modest volumes are obtained, as can be seen from the table of fig. 1, wherein:
  • L
    is the length of the piezoelectric actuator,
    W
    is the actuator diameter
    Fzbf
    is the theoretical load which can be developed by the actuator,
    ΔL0
    is the idle actuator displacement,
    whereas in the last column the displaced volumes are shown according to the type of piston actuator taken into consideration; it is immediately apparent that these volumes are insufficient, in the majority of cases, to supply even a 50 cc engine. An exception is only the actuator called EPCOS a which, in the embodiment showing two specimens arranged stacked (line 2 of the table of fig. 1), is sufficient for the power of a motorbicycle.
  • Due to obvious reasons of greater efficiency, but also for ease of description, here and in the following reference is always made to a piezoelectric-type actuator applied to a piston actuator, but it is intended that the teaching of the invention may be applied also to the other systems mentioned above.
  • The object of the present invention is hence to obtain an improvement of the performance of a piston pump-injector system with piezoelectric actuator, essentially by adopting means capable of amplifying the useful run of the piezoelectric actuator.
  • Such object is achieved by means of a structure of the piezoelectric actuator as defined in claim 1), as well as by an injection pump structure as defined in claim 4).
  • Further features and advantages of the invention will in any case be more evident from the following detailed description of a preferred embodiment, given purely by way of non-limiting example and shown in the accompanying drawings, wherein:
    • fig. 1 is a table showing, as already mentioned above, the data of some commercial types of piezoelectric actuators;
    • fig. 2 is a diagram showing the mechanical behaviour feature of a piezoelectric actuator;
    • fig. 3 diagrammatically shows, in an axial section, a piston pump-injector assembly with piezoelectric actuator according to the present invention;
    • fig. 4 shows in an extremely enlarged axial section a Belleville washer used in the device of fig. 3; and
    • fig. 5 shows a diagram of the operation feature of a Belleville washer, as it is used according to the invention.
  • As known, and as is evident from the diagram of fig. 2, a piezoelectric actuator has a linearly decreasing load/deformation feature. That is to say, at a set supply voltage (phantom lines for 0 V., for 80 V. and for 160 V., respectively), this type of actuator is capable of developing large loads with small piston displacements, but loses its thrust capability as the run increases, down to zero thrust when the maximum idle displacement is reached.
  • The diagram of fig. 2 is very easily interpreted: on the y axis the points idle operation are found, which represent the ideal case set forth earlier, wherein deformation is due only to the applied voltage (the maximum deformation value corresponding to the maximum supply voltage is commonly reported as the idle run of the actuator ΔLo ).
  • On the x axis, all the zero-deformation points are found; they represent an extreme situation referring to the non-ideal case, i.e. when the deformation imparted by the electrical control is fully neutralised by the elastic deformation. At the extreme point of the y axis, in correspondence of the maximum voltage, it is possible to guess that the corresponding electrical deformation (for the case set out in the drawing) at 60 µm at 160 V be neutralised by the elastic deformation equal to F/k, where F is the load and k is actuator rigidity.
  • As can again be guessed from the diagram of fig. 2, to the load of 1140 N a deformation of 60 µm, i.e. a rigidity of 19 N/µm, must correspond.
  • In intermediate situations between idle and zero-deformation, a progressive improvement of one performance is accomplished at the expense of the other, according to the linear law of fig. 2.
  • As can be easily guessed, the actual feature of the piezoelectric actuator does not perfectly suit the application thereof as a hydraulic pumping element, because the latter one requires the exertion of a constant force throughout the entire compression run. Instead, it has not been possible yet to use the full nominal run of the piezoelectric element, because, as seen with respect to the diagram of fig. 2, in the final part of the run the loading capability necessary to overcome fluid pressure would not be provided.
  • Since the piezoelectric actuator cannot exert a force which remains constant throughout the entire work run ΔLo, it is provided, according to a first aspect of the present invention, to adopt a compromise between run and load, making use of a part only of the actual total work run. In other words, it is provided to use the piezoelectric element with an average run and an average load. It is possible to prove that this is the best solution, i.e. the one which allows to obtain the maximum work per cycle; as a matter of fact, in such solution the largest quantity of energy is delivered between the one available per work cycle.
  • The piezoelectric material of which commercial actuators are made further has the feature - common to all ceramic materials - of displaying an asymmetric mechanical behaviour in the presence of tensile and compressive stresses; in particular, tensile behaviour is poor, whereas the compressive one is acceptable for applications as actuator, both in static and in dynamic conditions.
  • In order to have a duration and reliability compatible with automotive industry requirements, it is hence imperative, in the light of what has been set forth above, that the actuators employed always work under a compressive stress. According to another aspect of the present invention, it is therefore provided to achieve this result by applying a preload to the piezoelectric element. Such technical practice allows to remarkably increase the useful life of the actuator.
  • From a functional point of view, the presence of a preload (assumed to be rigidly constant) does not affect the performance of the actuator, determining only a translation of the work cycle in the plane of fig. 2, i.e. bringing the work cycle inside the positive half-plane (compressive stress) of the load; thereby, a safety margin is accomplished which serves to safeguard the piezoelectric element from the dynamic tensile actions which are generated during fast operation and which must be neutralised precisely by the presence of the preload.
  • Should the preload be accomplished through a contrast spring, which is the simplest and cheapest solution, it must be noted, however, that when a contrast spring is added, the performance of a pump actuated by a piezoelectric actuator worsens as contrast spring rigidity increases.
  • According to an essential aspect of the present invention, however, it is suggested to adopt a negative-rigidity spring, i.e. a spring supplying a decreasing preload as deformation increases. An actuator deficiency is thereby countered by the special feature of the spring, i.e. the capability of providing high loads only at the beginning of the run.
  • In the case of the EPCOS actuator identified in line 3 of the table of fig. 1, if it is intended to work with a fixed preload of 500 N, with an idle displacement of 60 µm and a (fixed) load of 1140 N, only 50% of the run can be exploited. However, if, according to the present invention, a spring having a rigidity for example of -9,5 N/µm is used, which is capable of giving an initial-run load of 900 N and a final-run load of 900 N 9 , 5 N / μm × 60 μm = 330 N
    Figure imgb0002
    it was possible to ascertain that the load loss which may be developed by the actuator is compensated by the spring feature, and 100% of the run can be exploited, thereby doubling performance.
  • Among the springs widespread in the technical practice, the ones capable of displaying a negative rigidity are conical disc springs, or so-called Belleville washers (see fig. 4). In this kind of springs, upon varying of the ratio η between the free height h of the conical disc and its thickness t, different curve trends are obtained; the diagram of fig. 5 shows an example, wherein:
    • if η < 1.41, the load increases in the deformation direction,
    • if <1.41 η < 2.83, there is a deformation area, around the free height value, where the load decreases (negative rigidity);
    • if η > 2.83 the previous behaviour is heightened and even a load sign inversion is obtained (the spring pulls instead of pushing and, if it is not constrained, jumps into a stable position with higher deformation values).
  • The most suitable behaviour for the application of the present invention is evidently the one where 1.41 < η < 2,83.
  • However, the embodiment comprising springs having a negative rigidity of -9.5 N/µm, although theoretically possible, is of no practical usefulness. As a matter of fact, in order to obtain a similar value of the diagram gradient of fig. 2, albeit limited to the middle portion where the derivative takes up the absolute minimum value, it would be necessary to resort to diameters of 800 mm with thicknesses of 20 mm. These dimensions are evidently not admissible for use in internal combustion engines, in particular those intended for motor bicycles. The problem has therefore arisen of how to manufacture a spring featuring maximum negative rigidity with the smallest dimensions.
  • According to another important aspect of the present invention, it was therefore resorted to the idea of artificially amplifying the negative rigidity of the spring, arranging two springs in series and precisely one negative-rigidity spring coupled with a positive-rigidity spring. It is known that the overall rigidity of two springs arranged in series is given by the formula: k = k 1 k 2 k 1 + k 2
    Figure imgb0003

    (which among other things is confirmed by the fact that, when two conventional springs are placed in series, rigidity decreases: for example, assuming that k1 = 100 and k2 = 100, the result is k = 50). If, however, according to the present invention, a negative-rigidity spring is arranged in series with a positive-rigidity spring, as mentioned, an overall negative rigidity is obtained, but amplified in its modulus. For example, assuming k1 = 100 and k2 = -95, the result becomes k = 1900).
  • On the basis of such a configuration, it is hence possible to design a spring capable of providing maximum negative rigidity with respect to material resistance, having dimensions compatible with its application in internal combustion engines. As a result of this dimensioning, a spring having the following measures is for example manufactured (see the references of fig. 4) :
    D = 28 mm
    d = 16 mm
    h = 1.3 mm
    t = 0.5 mm
    h/t = 2.6
    kmin = -0.56 N/µm
    phosphate-containing steel material 1.1248 C75S(Ck75)
    wherein a high ratio between the spring height h and the thickness t of the spring disc is highlighted.
  • The rigidity thus obtained for the spring dimensioned as above is then doubled with two springs arranged packetwise and further amplified arranging in series a conventional spring with a rigidity of 1,15 N/µm.
  • From the calculations carried out, it appeared that a piezoelectric pump-injector, particularly suited to small-powered internal combustion engines - having for example a swept volume of 50 cm3 - can be manufactured, according to the present invention, also employing a small, inexpensive piezoelectric element such as the Epcos one (table of fig. 1), in association with a preload spring having a negative rigidity whose modulus is about half that of the piezoelectric element.
  • It is intended, however, that the invention is not to be considered limited to the particular arrangement illustrated above, which represents only an exemplary embodiment thereof, but that several changes are possible, all within the reach of a person skilled in the field, without departing from the scope of protection of the invention, as defined in the following claims.

Claims (4)

  1. Piezoelectric actuator for the actuation of an injection pump for internal combustion engines, comprising in combination a piezoelectric element and a contrast spring consisting of at least a Belleville washer, wherein
    said contrast spring comprises at least one Belleville washer having negative rigidity, i.e. providing a decreasing force as deformation increases, and sized so that the ratio between the spring height h and the thickness t of the Belleville washer disc is in the range 1.41 < h / t < 2.83
    Figure imgb0004
    and characterised in that at least a conventional, positive-rigidity spring, is arranged in series with said Belleville washer, said contrast spring supplying a preload of the piezoelectric element.
  2. Piezoelectric actuator as claimed in claim 1), characterised in that said Belleville washer has a negative rigidity whose modulus is about half the rigidity of the piezoelectric element.
  3. Piezoelectric actuator as in claim 1), characterised in that it comprises a pack of three identical negative-rigidity Belleville washers, arranged in parallel with each other and in series with at least a conventional, positive-rigidity spring.
  4. Injection pump for internal combustion engines, in particular small-powered ones, characterised in that it comprises an actuator as in any one of the preceding claims in combination with a piston pump-injector.
EP20060112774 2005-04-21 2006-04-19 Piezoelectric actuator for the operation of an injection pump for internal-combustion engines, and injector-pump assembly employing said actuator Expired - Fee Related EP1715177B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ITMI20050719 ITMI20050719A1 (en) 2005-04-21 2005-04-21 PIEZOELECTRIC ACTUATOR FOR THE ACTIVATION OF AN INJECTION PUMP FOR INTERNAL COMBUSTION ENGINES AND INJECTOR-PUMP COMPLEX WITH IT REALIZED

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Publication Number Publication Date
EP1715177A1 EP1715177A1 (en) 2006-10-25
EP1715177B1 true EP1715177B1 (en) 2009-07-15

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Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007030043A1 (en) 2007-06-26 2009-01-02 Stefan Barten Piezoelectrically operated dosing pump for conveying and dosing small liquid quantity with higher pressure, has movable piston, which is assigned to piezoelectric stack translator, which varies in length in dependence of applied voltage
CN101216027B (en) * 2008-01-11 2010-08-18 吉林大学 Piezoelectric stack pump
EP2450558A1 (en) * 2010-11-03 2012-05-09 Continental Automotive GmbH Injection valve
EP2495428A1 (en) * 2011-03-04 2012-09-05 Continental Automotive GmbH Apparatus for delivering fuel and fuel supply system

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60233363A (en) * 1984-05-03 1985-11-20 Nippon Soken Inc Fuel injection valve
DE19619319A1 (en) * 1996-05-14 1997-11-20 Ruediger Ufermann Piezoelectric fuel injection device for IC engine
DE19712921A1 (en) * 1997-03-27 1998-10-01 Bosch Gmbh Robert Fuel injector with piezoelectric or magnetostrictive actuator
JPH11182446A (en) * 1997-12-24 1999-07-06 Nissan Motor Co Ltd Pump
DE19827293A1 (en) * 1998-06-19 1999-12-23 Ruediger Ufermann Piezoelectric hydraulic pump for delivering fuel
DE10248433B4 (en) * 2002-10-17 2015-01-15 Cummins Ltd. Device for conveying media, in particular injection device for internal combustion engines of motor vehicles
AU2003275676A1 (en) * 2002-10-29 2004-05-25 Bosch Automotive Systems Corporation High flow rate fuel valve and fuel supply pump with the valve

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ITMI20050719A1 (en) 2006-10-22
DE602006007746D1 (en) 2009-08-27

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