EP0249313A2 - Brennstoff-Einspritzvorrichtung - Google Patents

Brennstoff-Einspritzvorrichtung Download PDF

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Publication number
EP0249313A2
EP0249313A2 EP87303128A EP87303128A EP0249313A2 EP 0249313 A2 EP0249313 A2 EP 0249313A2 EP 87303128 A EP87303128 A EP 87303128A EP 87303128 A EP87303128 A EP 87303128A EP 0249313 A2 EP0249313 A2 EP 0249313A2
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EP
European Patent Office
Prior art keywords
fuel
discharge passages
fuel discharge
valve
air
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
EP87303128A
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English (en)
French (fr)
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EP0249313A3 (en
EP0249313B1 (de
Inventor
Ernest Richard Stettner
Donald Dibble Stoltman
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.)
Motors Liquidation Co
Original Assignee
Motors Liquidation Co
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Filing date
Publication date
Application filed by Motors Liquidation Co filed Critical Motors Liquidation Co
Priority to AT87303128T priority Critical patent/ATE73903T1/de
Publication of EP0249313A2 publication Critical patent/EP0249313A2/de
Publication of EP0249313A3 publication Critical patent/EP0249313A3/en
Application granted granted Critical
Publication of EP0249313B1 publication Critical patent/EP0249313B1/de
Anticipated expiration legal-status Critical
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M69/00—Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel
    • F02M69/46—Details, component parts or accessories not provided for in, or of interest apart from, the apparatus covered by groups F02M69/02 - F02M69/44
    • F02M69/50—Arrangement of fuel distributors, e.g. with means for supplying equal portion of metered fuel to injectors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M51/00—Fuel-injection apparatus characterised by being operated electrically
    • F02M51/02—Fuel-injection apparatus characterised by being operated electrically specially for low-pressure fuel-injection
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M69/00—Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel
    • F02M69/08—Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel characterised by the fuel being carried by compressed air into main stream of combustion-air

Definitions

  • This invention relates to a fuel injection apparatus for a multi-cylinder internal combustion engine in which a plurality of injection nozzles discharge fuel adjacent the inlet ports of the engine and a single fuel injector meters the fuel to all of the injection nozzles, to a fuel injector, and to an injection nozzle.
  • Throttle body fuel injection apparatus employ one or two fuel injectors that deliver the fuel into the air flowing through the engine throttle body, and the mixture of air and fuel then flows through the engine inlet manifold to the inlet ports of the engine combustion chambers.
  • Port fuel injection apparatus typically employ individual fuel injectors to deliver fuel directly to each of the inlet ports.
  • a throttle body fuel injection apparatus with only one or two fuel injectors has a cost advantage over a port fuel injection apparatus with its several fuel injectors and the associated fuel rails.
  • port fuel injection apparatus offer advantages in engine operation. Those comparative advantages present incentive for a fuel injection apparatus in which a single fuel injector meters fuel and a plurality of injection nozzles deliver the fuel to the engine inlet ports.
  • This invention permits a fuel injection apparatus to deliver fuel through a plurality of injection nozzles directly to the inlet ports and to employ a single fuel injector to meter the fuel to all of the injection nozzles.
  • a single fuel injector meters fuel through an annular region into a cylindrical chamber defined between a bore in the injector base and a plug received in the bore, and a plurality of fuel discharge passages open from the cylindrical chamber to direct fuel to injection nozzles.
  • a solenoid operated valve in the fuel injector may meter fuel to the fuel discharge passages with very little motion.
  • a fuel injector meters fuel through an annular region to a plurality of fuel discharge passages that direct the fuel to injection nozzles, and the fuel injector includes a valve member with an aperture opening into the centre of the annular region.
  • a single fuel injector meters fuel to a plurality of fuel discharge passages that direct the fuel to injection nozzles, and a rectifier valve allows air to flow into the fuel discharge passages when the fuel injector is not metering fuel into the fuel discharge passages.
  • the fuel maintains its discharge velocity through the fuel discharge passages to the injection nozzles.
  • This feature also reduces the propagation of pressure waves through the fuel discharge passages as the fuel injector initiates and terminates fuel flow into the fuel discharge passages.
  • a fuel injector has a base with a plurality of fuel discharge passages that receive the ends of fuel discharge lines through which fuel is directed to injection nozzles, the injector base has an air inlet surrounding the ends of the fuel discharge lines, and air lines surround the fuel discharge lines and direct air to the injection nozzles.
  • the fuel discharge lines are thermally insulated.
  • a single fuel injector l0 receives fuel from a source of fuel at a desired pressure and meters fuel into six fuel discharge lines l2.
  • Each fuel discharge line l2 leads to an injection nozzle l4 that delivers the metered fuel into the stream of air flowing through one of the inlet manifold runners l6 and one of the inlet ports l8 to one of the combustion chambers 20 of a six cylinder engine 2l.
  • Fuel injector l0 has a housing 22 with a fuel inlet port 24 and an excess fuel outlet port 26 that establish a path for fuel flow through housing 22. Housing 22 is secured to an injector base 28. A valve member 30 which is solenoid operated controls fuel flow from housing 22 through an annular region 32 of injector base 28 to six fuel discharge passages 34 that receive fuel discharge lines l2.
  • Injector base 28 has a central bore 36 and includes a plug 38 received in central bore 36 to define a cylindrical fuel distribution chamber 40 between plug 38 and central bore 36.
  • the upper portion of plug 38 has a hexagonal configuration, the points 44 of which engage central bore 36 to divide cylindrical fuel distribution chamber 40 into six sectors 46. Each sector 46 opens into one of the fuel discharge passages 34.
  • the surface 48a surrounding central bore 36 and the surface 48b at the perimeter of plug 38 form an annular valve surface bounding annular region 32.
  • a spring 50 biases valve member 30 into engagement with surfaces 48a,b to interrupt fuel flow through annular region 32.
  • a solenoid coil 52 lifts valve member 30 against the bias of spring 50 to permit fuel flow through annular region 32 and the sectors 46 of cylindrical fuel distribution chamber 40 to fuel discharge passages 34 and fuel discharge lines l2.
  • valve member 30 When valve member 30 is lifted from surfaces 48a,b, fuel flows through a cylindrical area between valve member 30 and surface 48a. That cylindrical area is determined both by the radius of central bore 36 and by the height to which valve member 30 is lifted above surfaces 48a,b. As the radius of central bore 36 is increased, the height to which valve member 30 must be lifted may be decreased without restricting fuel flow into annular region 32.
  • plug 38 By using plug 38 to form the fuel flow region as an annular region 32 and to form the fuel distribution chamber as a cylindrical fuel distribution chamber 40, the radius is increased without increasing the desired area for the fuel flow region and the desired volume for the fuel distribution chamber.
  • the use of an annular fuel flow region accordingly reduces the motion of the valve member 30 as it is lifted by solenoid coil 52.
  • valve member 30 has an aperture 54 opening from housing 22 to a space 56 beneath valve member 30 within surface 48b.
  • fuel flows into annular region 32 both around valve member 30 and through aperture 54 and space 56. It will be understood, therefore, that the clearance required between valve member 30 and surface 48a is less with aperture 54 providing a path for fuel flow between valve member 30 and surface 48b into annular region 32 than would be required if it were necessary for all fuel flow into annular region 32 to pass around valve member 30 and between valve member 30 and surface 48a.
  • Fuel injector l0 is controlled to meter fuel in a conventional manner by energizing solenoid coil 52 with a pulse width modulated current. As the pulse width is increased, valve member 30 is lifted for an increased length of time to increase the duration of fuel flow into fuel discharge lines l2.
  • Plug 38 has a recess 58 open to the atmosphere and six ports 60 opening slightly downwardly from recess 58 into the sectors 46 of cylindrical fuel distribution chamber 40.
  • a hollow valve seat member 62 is received in recess 58 and has a valve seat 64 which is upwardly facing.
  • a rectifier valve disc 66 of lightweight Mylar rests on valve seat 64. Recess 58, valve seat 64 and rectifier valve disc 66 define air valve means.
  • Injector base 28 has a larger recess 68 open to the atmosphere and six air passages 70 surrounding fuel discharge lines l2. Air passages 70 receive air lines 72 that are disposed concentrically about fuel discharge lines l2.
  • Each injection nozzle l4 has a fluted insert 74 with a tapered tip 76 engaged in the end of fuel discharge line l2 and a tapered base 78 engaged in the end of air line 72.
  • Fluted insert 74 aligns fuel discharge line l2 within air line 72, and its flutes 80 deliver the fuel and air into the stream of air flowing through the inlet manifold runner l6.
  • the atmospheric pressure in larger recess 68 induces air to flow through air lines 72 to the subatmospheric pressure in the inlet ports l8, and the atmospheric pressure in recess 58 induces air to flow past rectifier valve disc 66 and through ports 60, sectors 46 of cylindrical fuel distribution chamber 40, and fuel discharge passages 34 and fuel discharge lines l2 to the subatmospheric pressure in inlet ports l8.
  • solenoid coil 52 lifts valve member 30 and fuel flows through annular region 32 into the sectors 46 of cylindrical fuel distribution chamber 40, the increased pressure in cylindrical fuel distribution chamber 40 stops air flow through ports 60 from recess 58 and engages rectifier valve disc 66 with its valve seat 64.
  • solenoid coil 52 When solenoid coil 52 is deenergized and spring 50 engages valve member 30 against surfaces 48a,b, air will again be induced to flow from recess 58 past rectifier valve disc 66 and through ports 60, sectors 46 of cylindrical fuel distribution chamber 40, and fuel discharge passages 34 and fuel discharge lines l2.
  • Air flow through the sectors 46 of cylindrical fuel distribution chamber 40 and the fuel discharge passages 34 and fuel discharge lines l2 allows the inertia of the fuel to maintain its discharge velocity, and reduces propagation of pressure waves through fuel discharge lines l2 as valve member 30 is lifted from and engaged with surfaces 48a,b.
  • Such air flow also provides a source of air at substantially atmospheric pressure immediately below valve member 30, thereby providing an essentially constant pressure in the annular region 32 to which valve member 30 delivers fuel.
  • Fuel discharge passages 60 open from the bottom of sectors 46, while ports 60 open slightly downwardly into the upper portion of sectors 46. With this construction, it is thought that fuel flow through sectors 46 past ports 60 will create a suction tending to assist in quickly lifting rectifier valve disc 66 from its valve seat 64.
  • Air flow through air lines 72 thermally insulates fuel discharge lines l2, and provides a source of air at substantially atmospheric pressure at the tip of injection nozzles l4 where the fuel is introduced into the stream of air flowing through the inlet ports l8.
  • injection nozzle l4 is proportioned so that the vacuum in a zone 82 within air line 72 at the end of fuel discharge line l2 is about l0% of the vacuum in the intake port l8 at the end of the injection nozzle l4 (that is, the difference between the pressure in zone 82 and the atmospheric pressure is about l0% of the difference between the pressure in intake port l8 and the atmospheric pressure).
  • fuel discharge line l2 is formed of tubing with a 0.864mm (0.034in) inside diameter and a l.60 mm (0.063in) outside diameter
  • air line 72 is formed of tubing with a 2.36mm (0.093in) inside diameter and a 3.00mm (0.ll8in) outside diameter.
  • Other parts are sized accordingly.
  • a single fuel injector ll0 receives fuel from a source of fuel at a desired pressure and meters fuel into four fuel discharge lines ll2.
  • Each fuel discharge line ll2 leads to an injection nozzle that delivers the metered fuel into the stream of air flowing through one of the inlet manifold runners and one of the inlet ports to one of the combustion chambers of a four cylinder engine.
  • Fuel injector ll0 has a housing l22 with a fuel inlet port l24 and an excess fuel outlet port that establish a path for fuel flow through housing l22.
  • Housing l22 is secured to an injector base l28.
  • a valve member l30 which is solenoid operated controls fuel flow from housing l22 through an annular region l32 of injector base l28 to four fuel discharge passages l34 that receive fuel discharge lines l22.
  • Injector base l28 has a central bore l36 and includes a plug l38 received in central bore l36 to define a cylindrical fuel distribution chamber l40 between plug l38 and central bore l36.
  • the upper portion of plug l38 differs from the upper portion of plug 38 shown in Figures 2 and 3; plug l38 has a circular configuration, the circumference l44 of which is uniformly spaced from central bore l36.
  • Cylindrical fuel distribution chamber l40 opens into the fuel discharge passages l34.
  • a spring l50 biases valve member l30 into engagement with surfaces l48a,b to interrupt fuel flow through annular region l32.
  • a solenoid coil l52 lifts valve member l30 against the bias of spring l50 to permit fuel flow through annular region l32 and cylindrical fuel distribution chamber l40 to fuel discharge passages l34 and fuel discharge lines ll2.
  • valve member l30 When valve member l30 is lifted from surfaces l48a,b, fuel flows through a cylindrical area between valve member l30 and surface l48a. That area is determined both by the radius of central bore l36 and by the height to which valve member l30 is lifted above surfaces l48a,b. As the radius of central bore l36 is increased, the height to which valve member l30 must be lifted may be decreased without restricting fuel flow into annular region l32. By using plug l38 to form the fuel flow region as an annular region l32 and to form the fuel distribution chamber as a cylindrical fuel distribution chamber l40, the radius is increased without increasing the desired area for the fuel flow region and the desired volume for the fuel distribution chamber. The use of an annular fuel flow region accordingly reduces the motion of the valve member l30 as it is lifted by solenoid coil l52.
  • valve member l30 has an aperture l54 opening from housing l22 to a space l56 beneath valve member l30 within surface l48b.
  • fuel flows into annular region l32 both around valve member l30 and through aperture l54 and space l56.
  • valve member l30 and surface l48a are less with aperture l54 providing a path for fuel flow between valve member l30 and surface l48b into annular region l32 than would be required if it were necessary for all fuel flow into annular region l32 to pass around valve member l30 and between valve member l30 and surface l48a.
  • Plug l38 has a recess l58 open to the atmosphere and four ports l60 opening horizontally from recess l58 into cylindrical fuel distribution chamber l40 opposite fuel discharge passages l34.
  • a hollow valve seat member l62 is received in recess l58 and has a valve seat l64 which is upwardly facing.
  • a rectifier valve disc l66 of lightweight Mylar rests on valve seat l64. Recess l58, valve seat l64 and rectifier valve disc l66 define air valve means.
  • Injector base l28 has a larger recess l68 open to the atmosphere and four air passages l70 surrounding fuel discharge lines ll2. Air passages l70 receive air lines l72 that are disposed concentrically about fuel discharge lines ll2.
  • Fuel injector ll0 is in other respects similar to fuel injector l0, and further details of construction are set forth in US patent 4572436 and will not be repeated here.
  • the atmospheric pressure in larger recess l68 induces air to flow through air lines l72 to the subatmospheric pressure in the inlet ports
  • the atmospheric pressure in recess l58 induces air to flow past rectifier valve disc l66 and through ports l60, across cylindrical fuel distribution chamber l40, and through fuel discharge passages l34 and fuel discharge lines ll2 to the subatmospheric pressure in the inlet ports.
  • solenoid coil l52 lifts valve member l30 and fuel flows through annular region l32 into cylindrical fuel distribution chamber l40
  • the increased pressure in cylindrical fuel distribution chamber l40 stops air flow through ports l60 from recess l58 and engages rectifier valve disc l66 with its valve seat l64.
  • solenoid coil l52 When solenoid coil l52 is deenergized and spring l50 engages valve member l30 against surfaces l48a,b, air will again be induced to flow from recess l58 past rectifier valve disc l66 and through ports l60, cylindrical fuel distribution chamber l40, and fuel discharge passages l34 and fuel discharge lines ll2.
  • Air flow through cylindrical fuel distribution chamber l40 and the fuel discharge passages l34 and fuel discharge lines ll2 allows the inertia of the fuel to maintain its discharge velocity, and reduces propagation of pressure waves through fuel discharge lines ll2 as valve member l30 is lifted from and engaged with surfaces l48a,b.
  • Such air flow also provides a source of air at substantially atmospheric pressure immediately below valve member l30, thereby providing an essentially constant pressure in the annular region l32 to which valve member l30 delivers fuel.
  • Air flow through air lines l72 thermally insulates fuel discharge lines ll2, and provides a source of air at substantially atmospheric pressure at the tip of the injection nozzles where the fuel is introduced into the stream of air flowing through the inlet ports.
  • a single fuel injector 2l0 receives fuel from a source of fuel at a desired pressure and meters fuel into six fuel discharge lines 2l2.
  • Each fuel discharge line 2l2 leads to an injection nozzle that delivers the metered fuel into the stream of air flowing through one of the inlet manifold runners and one of the inlet ports to one of the combustion chambers of a six cylinder engine.
  • Injector 2l0 has a housing 222 with a fuel inlet port 224 and an excess fuel outlet port that establish a path for fuel flow through housing 222.
  • Housing 222 is secured to an injector base 228.
  • a valve member 230 which is solenoid operated controls fuel flow from housing 222 through an annular region 232 of injector base 228 to six fuel discharge passages 234 that receive fuel discharge lines 2l2.
  • Injector base 228 includes a plate 235 that has a central bore 236 leading to annular region 232. Annular region 232 opens directly into the fuel discharge passages 234.
  • the surface 248 surrounding central bore 236 forms an annular valve surface.
  • a spring 250 biases valve member 230 into engagement with surface 248 to interrupt fuel flow through annular region 232.
  • a solenoid coil 252 lifts valve member 230 against the bias of spring 250 to permit fuel flow through annular region 232 to fuel discharge passages 234 and fuel discharge lines 2l2.
  • Injector base 228 has another bore 258 opening from the atmosphere into annular region 232.
  • a diaphragm 266 is sandwiched between the main portion of injector base 228 and its plate 235, overlying a valve seat surface 264 on annular region 232 and separating the central bore 236 from the bore 258.
  • Diaphragm 266 has six apertures 267 aligned with fuel discharge passages 234. Bore 258, valve seat surface 264 and diaphragm 266 define air flow means.
  • Injector base 228 has a larger recess 268 open to the atmosphere and six air passages 270 surrounding fuel discharge lines 2l2. Air passages 270 receive air lines 272 that are disposed concentrically about fuel discharge lines 2l2.
  • Fuel injector 2l0 is in other respects similar to fuel injector l0, and further details of construction are set forth in US patent 4572436 and will not be repeated here.
  • the atmospheric pressure in larger recess 268 induces air to flow through air lines 272 to the subatmospheric pressure in the inlet ports, and the atmospheric pressure in bore 258 induces air to flow beneath diaphragm 266 and through fuel discharge passages 234 and fuel discharge lines 2l2 to the subatomospheric pressure in the inlet ports.
  • solenoid coil 252 lifts valve member 230 and fuel flows through central bore 236, the increased pressure in central bore 236 engages diaphragm 266 with annular region 232, thereby obstructing air flow from bore 258 to fuel discharge passages 234 and fuel discharge lines 2l2.
  • solenoid coil 252 When solenoid coil 252 is deenergized and spring 250 engages valve member 230 against surface 248, air will again be induced to lift diaphragm 266 from annular region 232 and flow from bore 258 through fuel discharge passages 234 and fuel discharge lines 2l2.
  • Air flow through fuel discharge passages 234 and fuel discharge lines 2l2 allows the inertia of the fuel to maintain its discharge velocity, and reduces propagation of pressure waves through fuel discharge lines 2l2 as valve member 230 is lifted from and engaged with surface 248.
  • Such air flow also provides a source of air at substantially atmospheric pressure immediately below valve member 230, thereby providing an essentially constant pressure in the annular region 232 to which valve member 230 delivers fuel.
  • Air flow through air lines 272 thermally insulates fuel discharge lines 2l2, and provides a source of air at substantially atmospheric pressure at the tip of the injection nozzles where the fuel is introduced into the stream of air flowing through the inlet ports.
  • a single fuel injector 3l0 receives fuel from a source of fuel at a desired pressure and meters fuel into six fuel discharge lines 3l2.
  • Each fuel discharge line 3l2 leads to an injection nozzle that delivers the metered fuel into the stream of air flowing through one of the inlet manifold runners and one of the inlet ports to one of the combustion chambers of a six cylinder engine.
  • Fuel injector 3l0 has a housing 322a with a fuel inlet port 324a and an excess fuel outlet port that establish a path for fuel flow through housing 322a.
  • Housing 322a is secured to an injector base 328.
  • a valve member 330a which is solenoid operated controls fuel flow from housing 322a through an annular region 332a of injector base 328 to six fuel discharge passages 334a that extend to fuel discharge lines 3l2.
  • Annular region 332a includes a surface 348a.
  • a spring 350a biases valve member 330a into engagement with surface 348a to interrupt fuel flow through annular region 332a.
  • a solenoid coil 352a lifts or retracts valve member 330a against the bias of spring 350a to permit fuel flow through annular region 332a to fuel discharge passages 334a and fuel discharge lines 3l2.
  • Fuel injector 3l0 also has a housing 322b with an air inlet port 324b. Housing 322b is secured to injector base 328. A valve member 330b which is solenoid operated controls air flow from housing 322b through an annular region 332b of injector base 328 to six air discharge passages 334b that extend to fuel discharge lines 3l2.
  • Annular region 332b includes a surface 348b.
  • a spring 350b biases valve member 330b into engagement with surface 348b to interrupt air flow through annular region 332b.
  • a solenoid coil 352b retracts valve member 330b against the bias of spring 350b to permit air flow through annular region 332b to air discharge passages 334b and fuel discharge lines 3l2.
  • Annular region 332b, surface 348b, valve member 330b and solenoid coil 352b define air valve means.
  • valve members 330a,b To reduce the motion of valve members 330a,b as they are retracted by solenoid coils 352a,b, valve members 330a,b have apertures 354a,b opening from housings 322a,b to the centre of annular regions 332a,b. Thus when valve members 330a,b, are retracted by solenoid coils 352a,b, fuel and air flow into annular regions 332a,b both around valve members 330a,b and through apertures 354a,b.
  • valve members 330a,b and surfaces 348a,b are less with apertures 354a,b providing paths for fuel and air flow between valve members 330a,b and surfaces 348a,b into annular regions 332a,b than would be required if it were necessary for all fuel and air flow into annular regions 332a,b to pass around valve members 330a,b.
  • Fuel injector 3l0 is in other respects similar to fuel injector l0, and further details of construction are set forth in US patent 4572436 and will not be repeated here.
  • solenoid coils 352a,b are energized alternately.
  • solenoid coil 352b When solenoid coil 352b is energized, the pressure in housing 322b induces air to flow through air discharge passages 334b and fuel discharge lines 3l2 to the subatmospheric pressure in the inlet ports.
  • solenoid coil 352a When solenoid coil 352a is energized, fuel flows through annular region 332a to fuel discharge passages 334a and fuel discharge lines 3l2.
  • Air flow through the fuel discharge lines 3l2 allows the inertia of the fuel to maintain its discharge velocity, and reduces propagation of pressure waves through fuel discharge lines 3l2 as valve member 330a is lifted from and engaged with surface 348a. Such air flow also creates an essentially constant pressure in the annular region 332a to which valve member 330a delivers fuel.
  • a single fuel injector 4l0 receives fuel from a source of fuel at a desired pressure and meters fuel into three fuel discharge lines 4l2.
  • Each fuel discharge line 4l2 leads to an injection nozzle 4l4 that delivers the metered fuel into the stream of air flowing through one of the inlet manifold runners 4l6 and one of the inlet ports 4l8 to one of the combustion chambers 420 of a three cylinder engine 42l.
  • Fuel injector 4l0 has a housing 422 with a fuel inlet port 424 and an excess fuel outlet port that establish a path for fuel flow through housing 422. Housing 422 is secured to an injector base 428. A valve member 430 which is solenoid operated controls fuel flow from housing 422 through an annular region 432 of injector base 428 to three fuel discharge passages 434 that receive fuel discharge lines 4l2.
  • Injector base 428 has a central bore 436 and includes a plug 438 received in central bore 436 to define a cylindrical fuel distribution chamber 440 between plug 438 and central bore 436.
  • the upper portion of plug 438 has a cylindrical configuration, the circumference 444 of which is evenly spaced from central bore 436.
  • Cylindrical fuel distribution chamber 440 opens into the fuel discharge passages 434.
  • the surface 448a surrounding central bore 436 and the surface 448b at the perimeter of plug 438 form an annular valve surface bounding annular region 432.
  • a spring 450 biases valve member 430 into engagement with surfaces 448a,b to interrupt fuel flow through annular region 432.
  • a solenoid coil 452 lifts valve member 430 against the bias of spring 450 to permit fuel flow through annular region 432 and cylindrical fuel distribution chamber 440 to fuel discharge passages 434 and fuel discharge lines 4l2.
  • valve member 430 When valve member 430 is lifted from surfaces 448a,b, fuel flows through a cylindrical area between valve member 430 and surface 448a. That cylindrical area is determined both by the radius of central bore 436 and by the height to which valve member 430 is lifted above surfaces 448a,b. As the radius of central bore 436 is increased, the height to which valve member 430 must be lifted may be decreased without restricting fuel flow into annular region 432.
  • plug 438 to form the fuel flow region as an annular region 432 and to form the fuel distribution chamber as a cylindrical fuel distribution chamber 440, the radius is increased without increasing the desired area for the fuel flow region and the desired volume for the fuel distribution chamber.
  • the use of an annular fuel flow region accordingly reduces the motion of the valve member 430 as it is lifted by solenoid coil 452.
  • valve member 430 has an aperture 454 opening from housing 422 to a space 456 beneath valve member 430 within surface 448b.
  • fuel flows into annular region 432 both around valve member 430 and through aperture 454 and space 456. It will be understood, therefore, that the clearance required between valve member 430 and surface 448a is less with aperture 454 providing a path for fuel flow between valve member 430 and surface 448b into annular region 432 than would be required if it were necessary for all fuel flow into annular region 432 to pass around valve member 430 and between valve member 430 and surface 448a.
  • Injector base 428 has a recess 468 open to the atmosphere and three air passages 470 surrounding fuel discharge lines 4l2. Air passages 470 receive air lines 472 that are disposed concentrically about fuel discharge lines 4l2.
  • Fuel injector 4l0 is in other respects similar to fuel injector l0, and further details of construction are set forth in US patent 4572436 and will not be repeated here.
  • Each lateral aperture 477 includes a small aperture 479 opening from fuel discharge line 4l2 into air line 472 and a larger aperture 48l opening from air line 472.
  • the atmospheric pressure in recess 468 induces air to flow through air lines 472 to the subatmospheric pressure in the inlet manifold runners 4l6.
  • solenoid coil 452 lifts valve member 430, fuel flows through annular region 432, cylindrical fuel distribution chamber 440, and fuel discharge passages 434 and fuel discharge lines 4l2 and is injected through the zone 482 within air line 472 at the end of fuel discharge line 4l2.
  • Air flow through air lines 472 thermally insulates fuel discharge lines 4l2, and provides a source of air at substantially atmospheric pressure at the tip of injection nozzles 4l4 where the fuel is introduced into the stream of air flowing through the inlet manifold runner 4l6.
  • fuel discharge line 4l2 is formed of tubing with a 0.864mm (0.034in) inside diameter and a l.60mm (0.063in) outside diameter
  • air line 472 is formed of tubing with a 2.95mm (0.ll6in) inside diameter and a 3.96mm (0.l56in) outside diameter.
  • Apertures 479 are 0.356mm (0.0l4in) in diameter
  • apertures 48l are l.02mm (0.040in) in diameter.
  • Other parts are sized accordingly.
  • injection nozzle 5l4 fuel discharge line 5l2 and air line 572 terminate in injection nozzle 5l4.
  • the end 575 of injection nozzle 5l4 is closed by an insert 574, and the injection nozzle has four lateral apertures 577 to deliver the fuel and air into the stream of air flowing through the inlet manifold runner.
  • Each lateral aperture 577 includes a small aperture 579 opening from fuel discharge line 5l2 into air line 572 and a larger aperture 58l opening from air line 572.
  • fuel discharge line 5l2 is formed of tubing with a 0.7llmm (0.028in) inside diameter and a l.60mm (0.063in) outside diameter
  • air line 572 is formed of tubing with a 2.36mm (0.093in) inside diameter and a 3.00mm (0.ll8in) outside diameter.
  • Small apertures 579 are 0.356mm (0.0l4in) in diameter
  • larger apertures 58l are 0.635mm (0.025in) in diameter.
  • a single fuel injector 6l0 receives fuel from a source of fuel at a desired pressure and meters fuel into six fuel discharge lines 6l2.
  • Each fuel discharge line 6l2 leads to an injection nozzle 6l4 that delivers the metered fuel into the stream of air flowing through one of the inlet manifold runners 6l6 and one of the inlet ports 6l8 to one of the combustion chambers 620 of a six cylinder engine 62l.
  • Fuel injector 6l0 has a housing 622 with a fuel inlet port 624 and an excess fuel outlet port 626 that establish a path for fuel flow through housing 622. Housing 622 is secured to an injector base 628. A valve member 630 which is solenoid operated controls fuel flow from housing 622 through an annular region 632 of injector base 628 to six fuel discharge passages 634 that extend to fuel discharge lines 6l2.
  • Annular region 632 includes a surface 648.
  • a spring 650 biases valve member 630 into engagement with surface 648 to interrupt fuel flow through annular region 632.
  • a solenoid coil 652 lifts valve member 630 against the bias of spring 650 to permit fuel flow through annular region 632 to fuel discharge passages 634 and fuel discharge lines 6l2.
  • valve member 630 has an aperture 654 opening from housing 622 to the centre of annular region 632.
  • fuel flows into annular region 632 both around valve member 630 and through aperture 654. It will be understood, therefore, that the clearance required between valve member 630 and surface 648 is less with aperture 654 providing a path for fuel flow between valve member 630 and surface 648 into annular region 632 than would be required if it were necessary for all fuel flow into annular region 632 to pass around valve member 630 and between valve member 630 and surface 648.
  • Fuel injector 6l0 is in other respects similar to fuel injector l0, and further details of construction are set forth in US patent 4572436 and will not be repeated here.
  • Each fuel discharge line 6l2 terminates in an orifice 679 in an injection nozzle 6l4.
  • Each injection nozzle 6l4 has an air line 672 opening from the atmosphere and terminating in an orifice 68l. Injection nozzles 6l4 deliver the fuel and air into the stream of air flowing through the inlet ports 6l8.
  • the atmospheric pressure induces air to flow through air lines 672 to the subatmospheric pressure in the inlet ports 6l8.
  • solenoid coil 652 When solenoid coil 652 is energized, fuel flows through annular region 632 to fuel discharge passages 634 and fuel discharge lines 6l2.
  • Air flow through air lines 672 provides a source of air at substantially atmospheric pressure at the tip of injector nozzles 6l4 where the fuel is introduced into the stream of air flowing through the inlet ports 6l8.
  • fuel discharge line 7l2 and air line 772 terminate in injection nozzle 7l4.
  • the open end 775 of each air line 772 is reduced, and the open end of each fuel line 7l2 is spaced from the open end 775 of the associated air line 772.
  • Each fuel line 7l2 is formed with a helically coiled section 783 that embraces the inner wall 785 of the associated air line 772 to support the fuel discharge line 7l2 within the air line 772.
  • fuel discharge line 7l2 is formed of tubing with a 0.864mm (0.034in) inside diameter and a l.57mm (0.062in) outside diameter
  • air line 772 is formed of tubing with a 3.05mm (0.l20in) inside diameter and a 3.96mm (0.l56in) outside diameter
  • the helically coiled section 783 has a free overall diameter of at least 3.l8mm (0.l25in) to assure that it will be compressively engaged with the inside wall 785 of the air line 772.
  • each air line 772 is reduced to an inside diameter of l.4mm (0.055in) over a length of l.02mm (0.04in), and the spacing between the end of the fuel discharge line 7l2 and the open end 775 of the air line 772 is adjusted for the desired fuel spray characteristic.
  • Injection nozzles 7l4 may be employed to directly replace injection nozzles l4 in the Figure l embodiment.
  • the fuel injector shown in figure 2 is mounted in the top of an inlet manifold plenum with the terminals for the solenoid coil projecting outside and the concentric fuel and air lines extending inside the manifold through the manifold plenum and runners to injection nozzles 7l4.
  • Such a construction presents an improved appearance and protects the concentric fuel and air lines against damage, while still allowing injection nozzles 7l4 to deliver metered fuel into the stream of air flowing through the inlet ports to the engine combustion chambers.
  • an air supply line must extend from a source of clean air to the base of the fuel injector.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
EP87303128A 1986-05-02 1987-04-10 Brennstoff-Einspritzvorrichtung Expired - Lifetime EP0249313B1 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AT87303128T ATE73903T1 (de) 1986-05-02 1987-04-10 Brennstoff-einspritzvorrichtung.

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US85901486A 1986-05-02 1986-05-02
US859014 1986-05-02
US1029687A 1987-02-02 1987-02-02
US10296 1998-01-21

Publications (3)

Publication Number Publication Date
EP0249313A2 true EP0249313A2 (de) 1987-12-16
EP0249313A3 EP0249313A3 (en) 1989-11-15
EP0249313B1 EP0249313B1 (de) 1992-03-18

Family

ID=26681005

Family Applications (1)

Application Number Title Priority Date Filing Date
EP87303128A Expired - Lifetime EP0249313B1 (de) 1986-05-02 1987-04-10 Brennstoff-Einspritzvorrichtung

Country Status (4)

Country Link
EP (1) EP0249313B1 (de)
BR (1) BR8702114A (de)
CA (1) CA1292651C (de)
DE (1) DE3777454D1 (de)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1990006438A1 (en) * 1988-12-07 1990-06-14 Siemens-Bendix Automotive Electronics L.P. Fuel injection device with air-assisted fuel diffusion
US4958773A (en) * 1980-06-21 1990-09-25 General Motors Corporation Fuel injection
US4958774A (en) * 1989-06-21 1990-09-25 General Motors Corporation Fuel injection
EP0303344B1 (de) * 1987-08-03 1991-07-17 General Motors Corporation Brennstoffeinspritzvorrichtung
EP0490418A2 (de) * 1990-12-07 1992-06-17 General Motors Corporation Brennstoffeinspritzvorrichtung
US5207205A (en) * 1988-12-07 1993-05-04 Siemens Automotive L.P. Fuel injection device with air-assisted fuel diffusion

Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2623786A (en) * 1948-10-01 1952-12-30 Rudolf L Wille Method for atomizing fuel and nozzle for carrying out this method
US2957682A (en) * 1957-05-13 1960-10-25 Holley Carburetor Co Fuel system
DE1933514A1 (de) * 1968-07-04 1970-01-08 Brico Eng Brennstoffeinspritzsystem fuer Brennkraftmaschinen
US4325341A (en) * 1978-11-06 1982-04-20 Hitachi, Ltd. Fuel control device for fuel injection system for internal combustion engine
DE3033644A1 (de) * 1980-09-06 1982-04-29 Robert Bosch Gmbh, 7000 Stuttgart Kraftstoffeinspritzanlage
EP0083516A1 (de) * 1981-12-31 1983-07-13 Orbital Engine Company Proprietary Limited Verfahren und Vorrichtung für die Zufuhr von flüssigem Brennstoff mittels Gasdruck zu einem Motor
US4465050A (en) * 1981-05-19 1984-08-14 Nippon Soken, Inc. Device for atomizing the fuel for an internal-combustion engine
WO1984004568A1 (en) * 1983-05-19 1984-11-22 Wisdom Shirley A Apparatus for the uniform distribution of fuel to a multi-cylinder spark ignition engine
DE3320469A1 (de) * 1983-06-07 1984-12-13 Volkswagenwerk Ag, 3180 Wolfsburg Vorrichtung zur verteilung einer zweiphasenstroemung
US4519370A (en) * 1983-02-23 1985-05-28 Toyota Jidosha Kabushiki Kaisha Fuel injector electronically controlled engine
EP0163198A1 (de) * 1984-05-29 1985-12-04 Volkswagen Aktiengesellschaft Verfahren zur kontinuierlichen Kraftstoffeinspritzung und Einrichtung zur Durchführung des Verfahrens
US4570598A (en) * 1985-04-15 1986-02-18 Ford Motor Company Air assist fuel distributor type fuel injection system
US4572436A (en) * 1984-12-24 1986-02-25 General Motors Corporation Electromagnetic fuel injector with tapered armature/valve
GB2175952A (en) * 1985-05-24 1986-12-10 Orbital Eng Pty Supplying metered quantities of fuel to an I.C. engine

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4033644C1 (en) * 1990-10-23 1992-04-30 Maschinenfabrik Alfred Schmermund Gmbh & Co, 5820 Gevelsberg, De Cigarette group forming machine - incorporates accumulator with outlet guide system

Patent Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2623786A (en) * 1948-10-01 1952-12-30 Rudolf L Wille Method for atomizing fuel and nozzle for carrying out this method
US2957682A (en) * 1957-05-13 1960-10-25 Holley Carburetor Co Fuel system
DE1933514A1 (de) * 1968-07-04 1970-01-08 Brico Eng Brennstoffeinspritzsystem fuer Brennkraftmaschinen
US4325341A (en) * 1978-11-06 1982-04-20 Hitachi, Ltd. Fuel control device for fuel injection system for internal combustion engine
DE3033644A1 (de) * 1980-09-06 1982-04-29 Robert Bosch Gmbh, 7000 Stuttgart Kraftstoffeinspritzanlage
US4465050A (en) * 1981-05-19 1984-08-14 Nippon Soken, Inc. Device for atomizing the fuel for an internal-combustion engine
EP0083516A1 (de) * 1981-12-31 1983-07-13 Orbital Engine Company Proprietary Limited Verfahren und Vorrichtung für die Zufuhr von flüssigem Brennstoff mittels Gasdruck zu einem Motor
US4519370A (en) * 1983-02-23 1985-05-28 Toyota Jidosha Kabushiki Kaisha Fuel injector electronically controlled engine
WO1984004568A1 (en) * 1983-05-19 1984-11-22 Wisdom Shirley A Apparatus for the uniform distribution of fuel to a multi-cylinder spark ignition engine
DE3320469A1 (de) * 1983-06-07 1984-12-13 Volkswagenwerk Ag, 3180 Wolfsburg Vorrichtung zur verteilung einer zweiphasenstroemung
EP0163198A1 (de) * 1984-05-29 1985-12-04 Volkswagen Aktiengesellschaft Verfahren zur kontinuierlichen Kraftstoffeinspritzung und Einrichtung zur Durchführung des Verfahrens
US4572436A (en) * 1984-12-24 1986-02-25 General Motors Corporation Electromagnetic fuel injector with tapered armature/valve
US4570598A (en) * 1985-04-15 1986-02-18 Ford Motor Company Air assist fuel distributor type fuel injection system
GB2175952A (en) * 1985-05-24 1986-12-10 Orbital Eng Pty Supplying metered quantities of fuel to an I.C. engine

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4958773A (en) * 1980-06-21 1990-09-25 General Motors Corporation Fuel injection
EP0303344B1 (de) * 1987-08-03 1991-07-17 General Motors Corporation Brennstoffeinspritzvorrichtung
WO1990006438A1 (en) * 1988-12-07 1990-06-14 Siemens-Bendix Automotive Electronics L.P. Fuel injection device with air-assisted fuel diffusion
US5207205A (en) * 1988-12-07 1993-05-04 Siemens Automotive L.P. Fuel injection device with air-assisted fuel diffusion
US4958774A (en) * 1989-06-21 1990-09-25 General Motors Corporation Fuel injection
EP0490418A2 (de) * 1990-12-07 1992-06-17 General Motors Corporation Brennstoffeinspritzvorrichtung
EP0490418A3 (en) * 1990-12-07 1992-09-30 General Motors Corporation Fuel injection apparatus

Also Published As

Publication number Publication date
EP0249313A3 (en) 1989-11-15
DE3777454D1 (de) 1992-04-23
EP0249313B1 (de) 1992-03-18
BR8702114A (pt) 1988-02-09
CA1292651C (en) 1991-12-03

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