GB2112871A - Miniaturized unit fuel injector - Google Patents

Miniaturized unit fuel injector Download PDF

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Publication number
GB2112871A
GB2112871A GB08234524A GB8234524A GB2112871A GB 2112871 A GB2112871 A GB 2112871A GB 08234524 A GB08234524 A GB 08234524A GB 8234524 A GB8234524 A GB 8234524A GB 2112871 A GB2112871 A GB 2112871A
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United Kingdom
Prior art keywords
injector
fuel
plunger
supply
central bore
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
GB08234524A
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GB2112871B (en
Inventor
Julius P Perr
Lester L Peters
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.)
Cummins Inc
Original Assignee
Cummins Engine Co Inc
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Filing date
Publication date
Priority claimed from US06/332,249 external-priority patent/US4471909A/en
Priority claimed from US06/336,334 external-priority patent/US4441654A/en
Application filed by Cummins Engine Co Inc filed Critical Cummins Engine Co Inc
Publication of GB2112871A publication Critical patent/GB2112871A/en
Application granted granted Critical
Publication of GB2112871B publication Critical patent/GB2112871B/en
Expired 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
    • F02M57/00Fuel-injectors combined or associated with other devices
    • F02M57/02Injectors structurally combined with fuel-injection pumps
    • F02M57/021Injectors structurally combined with fuel-injection pumps the injector being of valveless type, e.g. the pump piston co-operating with a conical seat of an injection nozzle at the end of the pumping stroke
    • 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
    • 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
    • F02M57/023Injectors structurally combined with fuel-injection pumps characterised by the pump drive mechanical
    • 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
    • F02M59/102Mechanical drive, e.g. tappets or cams
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B2275/00Other engines, components or details, not provided for in other groups of this subclass
    • F02B2275/14Direct injection into combustion chamber
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

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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 unit injector (2) of the cam actuated, open nozzle type is disclosed in which an extremely compact injector body (4) has a minimum number of internal flow passages (66, 72) designed to reduce the complexity and cost of manufacture of the injector and in which the injector is actuated by a cam lobe (42) having a stepped profile for causing fuel to be metered into an injection chamber (52) of the injector (2) without blow back of gas into the supply passage (66) feeding fuel to the injector. The invention is characterized by an injector body (4) having an exterior shape designed to form a fuel supply flow path (22) and an isolated fuel drain flow path (24) between the exterior surface of the injector body (4) and the interior surface of the recess (6) in which the injector (2) is designed to be received. This arrangement allows a very simple pattern of radial passages (66, 72) to be formed in the injector body (4) even though the injector (2) is designed to provide scavenging fuel flow previously requiring a much more complex injector design. <IMAGE>

Description

SPECIFICATION Miniaturized unit fuel injector Technical field This invention relates to a low cost, miniaturized unit fuel injector of the type having an open nozzle and a reciprocating injector plunger mechanically actuated by an engine camshaft.
Background art Internal combustion engine designers have increasingly come to realize that substantially improved fuel supply systems are required in order to obtain higher levels of pollution abatement and increased fuel economy. Among the known options, direct fuel injection appears to be one of the best candidates for achieving improved performance but higher initial costs have tended to discourage its general adoption.
This situation is accentuated by the fact that only the more sophisticated, and therefore normally the more expensive, direct injection systems are capable of achieving the increasingly higher performance goals of engine manufacturers.
Up to the present, attempts to provide a low cost fuel injection system have tended to center on distributor type fuel injection systems having a single centralized high pressure pump and a distributor valve for metering and timing fuel flow from the pump to each of a plurality of injection nozzles, such as disclosed in U.S. Patent No.
3,557,765. Although simple in design concept, systems of this type generally suffer defects inherent with separation of the injector nozzles from the centralized pump. Unit injector systems avoid the inherent defects of distributor type systems by providing each engine cylinder with its own cam-actuated pump such as disclosed in U.S. Patent No. 3,544,008. Nevertheless, the performance advantage of unit injectors have generally not outweighed the detriment of greater costs except for heavy duty compression ignition engine applications.
While unit injectors have not normally been employed in low cost fuel systems, numerous refinements have been proposed over the years in an attempt to lessen their cost while retaining their inherent advantages. For example, the assignee of this application. Cummins Engine Company, Inc., has developed an open nozzle, pressure/time unit injector (see U.S. Patent Nos.
3,351,288 and 3,554,008) which is characterized by the need for only a single supply line (common rail) for supplying fuel to all of the injectors. Because fuel is metered into each injector through a separate feed orifice, the time during which each feed orifice is open and the pressure within the common rail can be relied upon to control the quantity of fuel metered for injection during each injection cycle. Additional cost reductions are realized because an open nozzle unit injector does not require a pressure relief valve at the injection orifice.
While effective in providing cost reductions, certain precautions are usually required in pressure/time, open nozzle injector systems to insure that combustion gases and spurious pressure signals do not enter the fuel supply system. These precautions may include the use of a check valve such as illustrated in U.S. Patent Nos. 3,355,108 and 2,984,231, upstream from the feed orifice of the injector to discourage combustion gases (known as blow-back) from entering the fuel supply. It is also common to provide for scavenging flow of fuel through the injector to remove gases which may have entered the fuel supply line. Scavenging flow additionally serves the function of cooling the injector and would be useful even if it were unnecessary to remove blow-back gases.Thus, a commercially acceptable unit injector, even when designed in accordance with principles intended to simplify the injector structure, is typically a labyrinth of axial and radial drillings. As used in this application, "axial" means parallel with the longitudinal axis of the injector and "radial" means perpendicular to the longitudinal axis of the injector. Moreover, the injector body is usually formed of multiple components requiring very close tolerance controls.
Still other attempts have been made to control blow-back gases in open nozzle unit injectors by employing a stepped cam for closing off a fuel feed port in the injector prior to a build up of compression pressure within the combustion chamber served by the injector. See, for example Fig. 9 and col. 5, lines 49-71 of U.S. Patent No.
2,984,231. Implementation of such blow-back control concepts as disclosed in U.S. Patent No.
2,984,231 require axial passages in both the injector body and in the cam actuated plunger mounted within the injector body. The need for such passages can add significantly to the cost and complexity of an injector.
In very simple cam actuated injectors such as illustrated in Australian Patent No. 202,734, axial drillings have been eliminated from the injector body by forming a flow path between the exterior of the injector body and the interior of the recess in which the injector body is received. By this arrangement, an easily formed radial bore may be provided in the injector body to act as a feed passage from the supply flow path surrounding the injector body into the injector chamber of the unit injector. If the injector is capable of providing a scavenging fuel flow as illustrated in U.S. Patent No. 3,351,288 or 2,984,231, the number of necessary flow passages increases and the overall size of the injector must increase to accommodate such passages. Multi-function injectors of this type normally require at least one or more axial passages.Such passages are more difficult and costly to form and have not been eliminated even in injector designs in which the supply and drain lines leading to and from the injector are formed entirely within the engine head such as is illustrated in U.S. Patent No.
3,351,288.
In short, fuel injectors capable of meeting rigorous operation specifications have invariably been highly complex, costly to manufacture, and/or relatively large in size.
Disclosure of the invention The first object of this invention is to overcome, the deficiencies of the prior art described above by providing a fuel injector of greatly simplified design but which is capable of performing a variety of functions, including blow-back gas control, previously associated only with more complex designs.
The second object of this invention is to provide a highly compact, unit injector formed of multi-function components including an injector body having a minimal number of fluid flow passages, most of which are arranged in a generally radial direction to decrease manufacturing costs.
The third object of this invention is to provide a unit injector in which individual components and passages are shaped and organized to perform multiple functions previously requiring a significantly greater number of injector components. In particular, a radially directed supply passage containing a feed orifice for metering fuel into the injector may also serve to supply fuel to the injector for scavenging and cooling purpose.
The fourth object of the subject invention is to provide a stepped cam structure for actuating a simplified unit injector designated to cooperate with the stepped cam in a manner to cause an early termination of injector metering prior to the desired time for fuel injection to prevent thereby back flow gases from entering the fuel supply line while at the same time eliminating the need for a check valve upstream from the feed orifice of the injector.
Still other and more specific objects of this invention may be understood from an examination of the following Brief Description of the Drawings and Best Mode for Carrying Out the Invention.
Brief description of the drawings Fig. 1 is a partially broken away cross-sectional view of one embodiment of the subject invention employing a greatly simplified arrangement of fuel supply and drainage passages.
Fig. 2 is a partially broken away cross-sectional view of the unit injector illustrated in Fig. 1 in which the injector plunger has been moved by a cam actuation means to an outermost position.
Fig. 3 is a diagrammatic illustration of a stepped cam having a profile which reduces combustion gas back flow in the unit injector of the subject invention.
Fig. 4 is a chart showing valve motion and cylinder pressure within a typical internal combustion engine.
Figs. 5a--5e illustrate various phases in the operation of a unit injector of the type illustrated in Figs. 1 and 2.
Fig. 6 is a chart illustrating operation of the stepped cam of Fig. 3 as is used to prevent combustion gas back flow.
Best mode for carrying out the invention Throughout this application, the words "inward" and "outward" will correspond to the directions, respectively, toward and away from the point at which fuel from an injector is actually injected into the combustion chamber of an engine. To further aid in an understanding of this invention, an index of the elements identified by reference numerals in the drawings is listed at the end of this description of the Best Mode for Carrying Out the Invention.
Fig. 1 illustates an open nozzle, pressure/time unit injector designed in accordance with the subject invention. In particular, Fig. 1 shows a unit injector 2 including an injector body 4 received in a recess 6 contained in the head 8 (only partially illustrated) of an internal combustion engine.
Injector body 4 is actually formed in two sections including an upper section of barrel 5 and lower section or cup 7 which is integrally joined to barrel 5. As is apparent from Fig. 1, injector body 4 is held within the recess 6 by means of mating screw threads 4a and may be placed in position by means of a torque applying wrench adapted to mate with a hexagonal socket 4b contained in the upper end of the injector body 4.
Fuel supply and drainage is provided for the injector through passages contained entirely within head 8. In particular, a supply channel 10 (sometimes referred to as a common rail) is adapted to supply fuel to the unit injector 2 while a drain channel 1 2 is adapted to receive fuel discharged from the injector for return to the fuel supply system. Both channel 10 and channel 12 may be formed to communicate with each of a plurality of injector receiving recesses positioned within head 8 to eliminate all external flow passages to and from the injectors. As illustrated in Fig. 1, the intersection of channel 10 with recess 6 defines a supply port 14. Similarly, the intersection of channel 12 and recess 6 defines a drain port 16.
The exterior surface of the injector body 4 is shaped to provide first and second annular recesses 1 8 and 20 axially spaced to communicate with channels 10 and 12 through supply port 14 and drain port 16, respectively. By this arrangement, a supply flow path 22 is formed between supply port 14 and the exterior surface of the injector body 4 defining first annular recess 18. Similarly, a drain flow path 24 is formed between drain port 16 and the exterior surface of the injector body 4 which defines second annular recess 20. In order to isolate flow paths 22 and 24, a circumferential seal 26 is positioned between the injector body 2 and the interior surface of recess 6. As is apparent from Fig. 1, the circumferential seal 26 may be positioned within a first annular groove 28 located between annular recesses 1 8 and 20. A similar type of circumferential seal 30 is positioned within a second annular groove 32 located above the drain flow path 24 to insure against fuel leakage. The inner end of supply flow path 22 is sealed by means of a washer-like seal element 33 compressibly held between a radially directed lip 35 formed in recess 6 and a radially directed surface 37 formed on injector body 4. To prevent particles from entering the injector body 4, first annular recess 18 may contain an annular undercut 19 covered by a filter screen 21 through which fuel entering the injector body 4 must pass.
Injector body 4 contains a central bore 34 which is coaxial with the longitudinal axis of the injector body 4. At the inner (lower) end of the injector body 4, one or more small injection orifices 36 are contained to provide a communication path between central bore 34 and a combustion chamber (not illustrated). Fuel is supplied to the combustion chamber through injection orifices 36 in controlled synchronism with the operation of the corresponding cylinder piston (not illustrated). Positioned within central bore 34 is an injector plunger 38 adapted to reciprocate in response to a cam-actuated mechanism 40 including a specially profiled cam lobe 42 connected to the conventional cam shaft (not illustrated) of the engine. Cam actuated mechanism 40 further includes a push rod 44, rocker arm 46 and a link 48.Because cam lobe 42 is rotated in a fixed manner relative to the reciprocating motion of the cylinder piston, injector plunger 38 may have its reciprocating motion very precisely controlled with respect to movement of the cylinder piston by carefully shaping the profile of cam lobe 42. Essentially, injector plunger 38 reciprocates between an innermost position (Fig. 2) in which injection orifices 36 are closed by the inner end 50 of plunger 38 and an outermost position (Fig. 1) in which an injection chamber 52 is formed within central bore 34 between the inner end 50 of injector plunger 38 and the injection orifices 36.
Since this invention relates to injectors of the "open nozzle" type, injection orifices 36 remain open to the combustion chamber whenever injector plunger 38 is moved outwardly from its innermost position. Injectors of this type have an inherent cost advantage over more complex closed nozzle injectors which employ a pressure released tip valve for maintaining the injection orifice in a closed condition except during the injection event. Injector plunger 38 is permanently biased toward its outermost position illustrated in Fig. 1 by a plunger return means 54 including a sleeve-like coupler 56 connected at its lower end 58 to the upper end of injector plunger 38. A radially, outwardly directed flange 60 is positioned adjacent the topmost portion of coupler 56.A fairly high pressure compression spring 62 extends between the upper end of injector body 4 and flange 60 to continually bias injector plunger 38 outwardly.
To control the amount of fuel injected during each inward movement of injector plunger 38, unit injector 2 is provided with a "pressure/time" injection capability in which fuel is metered into the injection chamber before each injection stroke through a fill or feed orifice which has been carefully dimensioned to allow the amount of fuel injected to be varied within a given amount of time by varying the supply line (common rail) pressure. Thus, the amount of fuel actually metered is a function of the supply pressure and the total metering time during which fuel flows through the feed orifice. This principle is applied to unit injector 2 by provision of a supply connecting means 64 for providing a pathway for fuel under pressure to flow from the supply flow path 22 into the portion of the central bore 34 which forms injection chamber 52.The supply connecting means 64 includes a supply passage 66 extending from the exterior surface of the injector body 4 to the interior surface of the central bore 34 along a straight radial path perpendicular to the longitudinal axis of the injector body 4. A restricted portion of supply passage 66 forms a feed orifice 68 which has carefully controlled hydraulic characteristics in order to produce the desired pressure/time metering capability discussed above.
Drain connecting means 70 is formed in the injector body 4 to provide a pathway for fuel to flow from the central bore 34 into the drain flow path 24. In a manner similar to the formation of supply passage 66, the drain connecting means 70 is produced by forming a drain passage 72 extending from the exterior surface of the injector body 4 to the interior surface of central bore 34 along a straight radial path perpendicular to the longitudinal axis of the injector body 4. Radial passages are significantly less expensive to manufacture as compared with axially arranged passages. Thus, the injector design of Fig. 1 achieves significant cost savings by employing the arrangement of flow paths and passages illustrated in Fig. 1.
To achieve the desired injector operation, injector plunger 38 has an exterior cylindrical surface which sealingly contacts the interior surface of central bore 34 to form an injection chamber seal. Injector plunger 38 includes a flow control means 74 for forming a scavenge flow path 84 in which fuel flows through the injector to scavenge blow back gases whenever the injector plunger 38 is less than a first predetermined axial distance from its innermost position. Flow control means 74 also allows fuel to be metered into the injector chamber 52 from the supply passage 66 only when the injector plunger 38 is moved outwardly more than a second predetermined distance from the innermost position.Flow control means 74 includes an annular groove 76 on the exterior surface of the injector plunger 38 extending axially from the supply passage 66 to the drain passage 72 when the injector plunger 38 is at its innermost position as illustrated in Fig.
2. Flow control means 74 further includes a cylindrical land 78 formed below or inwardly of groove 76 to cooperate with the interior surface of the central bore 34 to form a seal between the scavenge flow path 84 formed by groove 76 and the injector chamber 52. Thus, cylindrical land 78 is the innermost portion of the exterior cylindrical surface of injector plunger 38 which is in direct contact with the interior surface of central bore 34.
Injector plunger 38 is positioned at the first predetermined distance from its innermost position when the upper (outer) edge of cylindrical land 78 is located slightly inwardly from the upper (outer) edge of feed orifice 68.
In this position, fuel may begin to flow into the scavenge flow path 84 formed by annular groove 76. Alternatively, injector plunger 38 is positioned at the second predetermined distance when the lower (inner) edge of cylindrical land 78 is located slightly outwardly of the lower (inner) edge of feed orifice 68 to allow fuel to begin to flow into injector chamber 52. Obviously, the first predetermined distance is less than the second predetermined distance by an amount approximately equal to the axial extent of the cylindrical land 78 plus the axial extent of the opening of the feed orifice 68 into central bore 34.
The operation of the embodiment illustrated in Fig. 1 can now best be understood by also referring to Fig. 2 which discloses the same injector in which the injector plunger 38 has been moved to its innermost position. As illustrated by arrows 80 in Fig. 2, fuel enters through supply port 14 into the supply flow path 22 formed by annular groove 18 and then enters supply passage 66 for passage subsequently into scavenge flow passage 84 formed by groove 76 and is discharged through drain passage 72. The scavenging flow performs two very useful functions which are to cool the injector and to remove any combustion gases which may have entered through open injection orifices 36 into the fuel supply line.When the injector plunger 38 is moved outwardly sufficiently to open feed orifice 68, as illustrated in Fig. 1, fuel will flow into injection chamber 52 in an amount dependent upon the pressure in supply channel 10 and the length of time which feed orifice 68 remains open.
In the absence of any specialized timing control capability, the amount time which the injector plunger 38 dwells in either the innermost or outermost position depends upon the profile of cam lobe 42. As is apparent from Figs. 1 and 2, a possible design for cam lobe 42 includes a first sector 88 comprising more than 1 80C of the total circumference of cam lobe 42.
Sector 88 causes the injector plunger 38 to assume the innermost position. A second sector 90 of almost 90C causes the plunger to assume an outermost position as illustrated in Fig. 1.
Separating first sector 88 and second sector 90 is a third sector 92 (Fig. 1), the function of which will be described in greater detail below. Essentially, sector 92 functions to move the injector plunger 38 to a supply passage blocking position in which the injector plunger 38 is moved inwardly sufficiently to close off feed orifice 68 but does not move the injector plunger 38 sufficiently to actually initiate fuel injection. Third sector 92 is shaped to cause feed orifice 68 to be closed during the time that combustion chamber pressures are arising to a sufficiently high level to cause significant back flow of combustion gases into the fuel supply line. A fourth small sector 94 of the cam lobe 42 represents approximately that portion of the cam lobe 42 which causes actual fuel injection.The actual point at which injection begins is approximate since it depends in part upon the amount of fuel metered into chamber 52 during each cycle.
Reference is now made to Fig. 3 wherein the relationship of the profile of cam lobe 42 to the conventional four cycle stroke movements of the associated engine piston is illustrated. In particular, first sector 88 engages the lower end of push rod 44 (Figs. 1 and 2) at the point just before the engine piston executes its power stroke and continues to engage rod 44 throughout the exhaust stroke and a portion of the intake stroke of the piston. Second sector 90 engages rod 44 approximately halfway through the intake stroke of the piston and ceases to engage rod 44 approximately halfway into the compression stroke. Second sector 90 defines the time during each injector cycle when fuel is metered into the injection chamber 52.Third sector 92 which causes the injector plunger 38 to move towards its innermost position sufficiently to close the feed orifice 68 but not to cause injection is positioned to engage push rod 44 approximately halfway through the compression stroke and to continue this engagement up to the point at which injection commences. The fourth small sector 94 is that portion of cam lobe 42 which causes injector plunger 38 to its innermost position to force the metered fuel in injection chamber 52 through injection orifices 36 into the combustion chamber of the engine. A slightly raised dimple 95 (exaggerated in Figs. 1 and 2) is formed on cam lobe 42 near the end of fourth sector 94 to place "crush load" on injector plunger 38 at the end of the injection event in order to hold the injector plunger 38 tightly against the injector cup 7. This ability to hold injector plunger 38 very tightly against the injector cup 7 insures that injection orifices 36 will be sharply closed and will remain closed at the end of each injection period.
The dashed line 96 in Fig. 3 represents a more conventional cam profile in which the injector plunger would not be moved outwardly quite as far during the metering phase of operation.
Moreover, the metering phase is shown as continuing throughout a much greater portion of the compression stroke of the engine piston.
Because the metering phase has been reduced in the subject invention, it is necessary to enlarge the feed orifice 68 to accommodate a somewhat higher rate of fuel flow into the injection chamber during the shortened metering period. Tests have shown that the combination of a stepped cam profiled and shortened metering period in combination with the scavenging flow is fully adequate to prevent blow back gases from interfering with satisfactory operation of the injector plunger 38 illustrated in Figs. 1 and 2 without the use of a conventional check valve upstream from the feed orifice 68.
Figs. 4, 5a--5e and 6 illustate even more clearly the various phases of injector operation as compared with valve motion and cylinder pressure. In particular, Fig. 4 specifically illustrates the movement of an exhaust valve (line 98) and the movement of an intake valve (line 100) with the cylinder pressure (line 102) occurring during the four stroke movements of an engine piston.
Figs. 5a--5e disclose the corresponding conditions of the injector plunger relative to the engine piston movement illustrated in Fig. 4. Fig.
5a thus shows the condition of an injector plunger during the exhaust stroke of a piston while Fig. 5b discloses the condition of the injector plunger upon initial opening of feed orifice 68 which thereby commences metering of fuel 1 04 into the injection chamber when the combustion chamber pressure is relatively low. Fig. Sc shows the condition of the injector toward the end of the metering period in which a greater quantity of fuel 106 has entered the injector chamber. It should be noted that a small clearance exists between the shank portion 108 of the innermost end of the injector plunger and the corresponding portion 110 of the central bore to allow fuel to flow from the upper portion to the lower portion of injection chamber 52.
Fig. 5d illustrates the condition of the injector when the third sector 92 of cam lobe 42 has caused the injector plunger to advance sufficiently to close feed orifice 68, but has not yet advanced the injector plunger sufficiently to force the metered fuel through the injector orifices 36.
Thus, Fig. 5d illustrates the condition of the injector during the period that the cylinder pressure begins to increase substantially. Note that feed orifice 68 is closed to prevent combustion gas back flow. Fig. 5e shows the condition of the injector as the injector plunger is moved toward its innermost position to cause fuel injection through injection orifices 36.
Fig. 6 is a graph of injector plunger travel versus time. The corresponding top dead center (TDC) and bottom dead center (BDC) positions of the associated engine piston are also indicated in Fig. 6. The schematic illustrations of a feed orifice labeled 68' and 68" in Fig. 6 disclose the points along the solid line representative of injection plunger motion at which scavenging commences and ends, respectively. Similarly, the feed orifice illustrations labeled 68"' and 68"" represent the commencement and termination of fuel metering at corresponding points along the solid line in Fig.
6 representative of injector plunger travel. The dashed line of Fig. 6 illustrates the injector plunger motion which would result if a more conventional cam lobe profile were employed rather than the profile illustrated in Figs. 1-3.
The feed orifice would also be repositioned as shown with the dashed lines.
An especially simple unit injector has been described which combines a simplified flow passage arrangement with a stepped cam profile to provide a multi-function, high performance injector which requires far fewer components than conventionally designed injectors. Moreover, a unit injector has been described which uses the space between the injector body and the recess within which it is positioned during use to eliminate the need for axial flow passages within the injector body. Only relatively inexpensive radial passages are required to provide both pressure/time metering and scavenge fuel flow in the injector.
Index to reference numbers 2 unit injector 4 injector body 4a screw threads 4b hexagonal socket 5 upper section or barrel 6 recess 7 lower section or cup 8 head 10 supply channel 12 drain channel 14 supply port 1 6 drain port 18 first annular recess 19 annular undercut 20 second annular recess 21 filter screen 22 supply flow path 24 drain flow path 26 circumferential seal 28 first annular groove 30 circumferential seal 32 second annular groove 33 washer-like seal element 34 central bore 35 lip 36 injection orifice 37 radially directed surface 38 injector plunger 40 cam actuated mechanism 42 cam lobe 44 push rod 46 rocker arm 48 link 50 forward end 52 injection chamber 54 plunger return means 56 coupler 58 lower end of coupler 60 flange 62 compression spring 64 supply connecting means 66 supply passage 68 feed orifice 70 drain connecting means 72 drain passage 74 flow control means 76 annular groove 78 cylindrical land 80 arrows 84 scavenge flow path 88 first sector 90 second sector 92 third sector 94 fourth sector 95 raised dimple 96 conventional cam profile 98 exhaust valve movement 100 intake valve movement 102 cylinder pressure 104 metered fuel 106 metered fuel 108 shank portion 110 central bore portion Industrial applicability A miniaturized unit injector designed in accordance with this invention would find application in a very large variety of internal combustion engines. One particularly important application would be for small compression ignition engines adapted for powering automobiles. Lighter truck engines and medium range horsepower engines could also benefit from the use of injectors designed in accordance with the subject invention.

Claims (11)

Claims
1. A fuel injector for use in an injector receiving recess of an internal combustion engine for injecting periodically into a combustion chamber of the engine a portion of the fuel received from a supply port opening into the recess and for returning the remaining portion of the fuel received from the supply port to an axially spaced rain port which also opens into the recess said fuel injector comprising:: (a) an injector body shaped to be inserted into the recess to form a supply flow path extending between the supply port and the exterior surface of said injector body and to form a drain flow path, isolated from the supply flow path, extending between the drain port and the exterior surface of said injector body, said injector body containing (1) a central bore, and (2) an open injection orifice located adjacent the inner end of said central bore; (b) supply connecting means providing a pathway for fuel under pressure to flow from the supply flow path into the central bore, said supply connecting means containing a supply passage extending from the exterior surface of said injector body to the interior surface of the central bore along a straight radial path perpendicular to the longitudinal axis of said injector body;; (c) drain connecting means for providing a pathway for fuel to flow from the central bore into the drain flow path; and (d) an injector plunger mounted for reciprocal movement within the central bore between an innermost position in which the injection orifice is closed by the inner end of said injector plunger and an outermost position in which an injection chamber is formed within the central bore between the inner end of said injector plunger and the open injection orifice, said injector plunger including flow control means for forming a scavenge flow path to cause scavenge flow of fuel through said injector body whenever said injector plunger is less than a first predetermined axial distance from the innermost position and for allowing fuel to be metered into the injection chamber from the supply passage whenever said injector plunger is moved more than a second predetermined axial distance from the innermost position.
2. A fuel injector as defined in claim 1, in which said flow control means includes an annular groove on the exterior surface of said injector plunger for forming the scavenge flow path extending axially from the supply passage to the drain passage whenever said injector plunger is in the innermost position and a cylindrical land cooperating with the interior surface of the central bore to form a seal between the scavenge flow path and the injection chamber.
3. A fuel injector as defined in claim 1 or 2, in which said drain connecting means includes a drain passage extending from the exterior surface of said injector body to the interior surface of the central bore along a straight radial path perpendicular to the longitudinal axis of said injector body.
4. A fuel injector as defined in claim 2, in which the shape of the supply passage defined by said supply connecting means is chosen to cause the amount of fuel metered into the injection chamber during each injection cycle to be dependent on both the pressure of the fuel supplied through the supply port and the total time during which said injector plunger is more than the first predetermined axial distance from its innermost position.
5. A fuel injector as defined in claim 2, in which the first predetermined distance is less than the second predetermined distance by an amount equal to the axial extent of said cylindrical land plus the axial extent of the opening of the supply passage into the central bore.
6. A fuel injector as defined in claim 1, in which said injector body contains on its exterior surface first and second annular recesses axially spaced along said injector body to communicate with the supply port and the drain port, respectively, when said injector body is operatively positioned within the injector receiving recess.
7. A fuel injector as defined in claim 6, further including seal means for forming circumferential seals between the exterior of said injector body and the interior surface of the injector receiving recess to isolate the supply flow path from the drain flow path.
8. A fuel injector as defined in claim 1, in which said injector body includes exterior screw threads on its outer end for mating with interior screw threads on the interior of the injector receiving recess and wherein said injector body contains a socket at its outer end shaped to receive a torque applying wrench.
9. A fuel injector assembly for injecting periodically into a combustion chamber of an internal combustion engine fuel received from a fuel supply flow path, comprising: (a) an injector body containing (1) a central bore, and (2) an open injection orifice located to provide a communication path between the central bore and the combustion chamber; (b) supply connecting means for providing a pathway for fuel to flow from the supply flow path into the central bore, said supply connecting means containing a supply passage which communicates with the central bore through a feed orifice;; (c) an injector plunger mounted for reciprocal movement within the central bore between an innermost position in which the injection orifice is closed by the inner end of said injector plunger and an outermost position in which an injection chamber is formed within the central bore between the inner end of said injector plunger and the injection orifice, said injector plunger including a cylindrical surface in direct sealing contact with the interior surface of the central bore to form an injection chamber seal; and (d) cam actuating means for reciprocating said injector plunger in timed sequence with the movement of a piston within the combustion chamber in a manner to cause fuel to be metered into the injection chamber without blow back of gas into the supply passage by moving said cylindrical surface outwardly beyond the feed orifice to cause the feed orifice to open directly into the injection chamber only when the combustion chamber pressure is relatively low and by terminating fuel metering substantially before fuel injection commences by moving said injector plunger inwardly to a supply passage blocking position in which said cylindrical surface is positioned over the feed orifice to seal the supply passage from the injection chamber during the period that combustion chamber pressure otherwise is increasing sufficiently to cause blowback of gases into the supply passage if the supply passage were left unblocked.
10. A fuel injector assembly as defined in claim 9, in which said cam actuating means includes a cam lobe for controlling the position of said injector plunger, said cam lobe including a first sector having a radial extent for holding said injector plunger in its innermost position, a second sector having a radial extent for holding said injector plunger in its outermost position and a third sector having a radial extent intermediate the radial extents of said first and second sectors for moving said injector plunger to its supply passage blocking position.
11. A fuel injector assembly as defined in claim 9, in which said third sector has a circumferential extent which causes it to hold said injector plunger in the supply passage blocking position from approximately the midpoint of the compression stroke of the corresponding piston to the commencement of injection.
1 2. A fuel injector substantially as hereinbefore described and as shown in the accompanying drawings.
GB08234524A 1981-12-18 1982-12-03 Miniaturized unit fuel injector Expired GB2112871B (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US06/332,249 US4471909A (en) 1981-12-18 1981-12-18 Miniaturized unit fuel injector
US06/336,334 US4441654A (en) 1981-12-31 1981-12-31 Fuel injector assembly including a blow-back prevention cam

Publications (2)

Publication Number Publication Date
GB2112871A true GB2112871A (en) 1983-07-27
GB2112871B GB2112871B (en) 1986-05-21

Family

ID=26988131

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08234524A Expired GB2112871B (en) 1981-12-18 1982-12-03 Miniaturized unit fuel injector

Country Status (4)

Country Link
KR (1) KR860001308B1 (en)
BR (1) BR8207376A (en)
GB (1) GB2112871B (en)
MX (1) MX154435A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2642478A1 (en) * 1989-02-02 1990-08-03 Semt Pielstick DEVICE FOR CONTROLLING A FUEL INJECTION PUMP
WO2004055359A1 (en) * 2002-12-18 2004-07-01 Delphi Technologies, Inc. Cam arrangement and fuel pump arrangement incorporating a cam arrangement
EP3358176A4 (en) * 2015-09-30 2018-08-22 Yanmar Co., Ltd. Diesel engine

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2642478A1 (en) * 1989-02-02 1990-08-03 Semt Pielstick DEVICE FOR CONTROLLING A FUEL INJECTION PUMP
EP0381103A1 (en) * 1989-02-02 1990-08-08 S.E.M.T. Pielstick Control device for a fuel injection pump
WO2004055359A1 (en) * 2002-12-18 2004-07-01 Delphi Technologies, Inc. Cam arrangement and fuel pump arrangement incorporating a cam arrangement
US7308888B2 (en) 2002-12-18 2007-12-18 Delphi Technologies, Inc. Cam arrangement and fuel pump arrangement incorporating a cam arrangement
EP3358176A4 (en) * 2015-09-30 2018-08-22 Yanmar Co., Ltd. Diesel engine
US10451015B2 (en) 2015-09-30 2019-10-22 Yanmar Co., Ltd. Diesel engine

Also Published As

Publication number Publication date
BR8207376A (en) 1983-10-18
MX154435A (en) 1987-08-17
KR860001308B1 (en) 1986-09-11
GB2112871B (en) 1986-05-21
KR840002953A (en) 1984-07-21

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Effective date: 19981203