US3785354A - Fuel injection system - Google Patents
Fuel injection system Download PDFInfo
- Publication number
- US3785354A US3785354A US00227461A US3785354DA US3785354A US 3785354 A US3785354 A US 3785354A US 00227461 A US00227461 A US 00227461A US 3785354D A US3785354D A US 3785354DA US 3785354 A US3785354 A US 3785354A
- Authority
- US
- United States
- Prior art keywords
- air inlet
- electronic means
- fins
- engine
- passage
- 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.)
- Expired - Lifetime
Links
Images
Classifications
-
- 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
- F02M51/005—Arrangement of electrical wires and connections, e.g. wire harness, sockets, plugs; Arrangement of electronic control circuits in or on fuel injection apparatus
-
- 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
- F02M51/06—Injectors peculiar thereto with means directly operating the valve needle
- F02M51/061—Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means
- F02M51/0625—Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means characterised by arrangement of mobile armatures
- F02M51/0664—Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means characterised by arrangement of mobile armatures having a cylindrically or partly cylindrically shaped armature, e.g. entering the winding; having a plate-shaped or undulated armature entering the winding
- F02M51/0671—Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means characterised by arrangement of mobile armatures having a cylindrically or partly cylindrically shaped armature, e.g. entering the winding; having a plate-shaped or undulated armature entering the winding the armature having an elongated valve body attached thereto
- F02M51/0675—Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means characterised by arrangement of mobile armatures having a cylindrically or partly cylindrically shaped armature, e.g. entering the winding; having a plate-shaped or undulated armature entering the winding the armature having an elongated valve body attached thereto the valve body having cylindrical guiding or metering portions, e.g. with fuel passages
-
- 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
- F02M53/00—Fuel-injection apparatus characterised by having heating, cooling or thermally-insulating means
- F02M53/04—Injectors with heating, cooling, or thermally-insulating means
- F02M53/08—Injectors with heating, cooling, or thermally-insulating means with air cooling
-
- 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
- F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
- F02M61/14—Arrangements of injectors with respect to engines; Mounting of injectors
- F02M61/145—Arrangements of injectors with respect to engines; Mounting of injectors the injection nozzle opening into the air intake conduit
-
- 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
- F02M69/04—Injectors peculiar thereto
- F02M69/042—Positioning of injectors with respect to engine, e.g. in the air intake conduit
- F02M69/044—Positioning of injectors with respect to engine, e.g. in the air intake conduit for injecting into the intake conduit downstream of an air throttle valve
-
- 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
- F02M69/04—Injectors peculiar thereto
- F02M69/047—Injectors peculiar thereto injectors with air chambers, e.g. communicating with atmosphere for aerating the nozzles
-
- 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
- F02M69/462—Arrangement of fuel conduits, e.g. with valves for maintaining pressure in the pipes after the engine being shut-down
- F02M69/465—Arrangement of fuel conduits, e.g. with valves for maintaining pressure in the pipes after the engine being shut-down of fuel rails
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D2200/00—Input parameters for engine control
- F02D2200/02—Input parameters for engine control the parameters being related to the engine
- F02D2200/06—Fuel or fuel supply system parameters
- F02D2200/0606—Fuel temperature
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S261/00—Gas and liquid contact apparatus
- Y10S261/82—Upper end injectors
Definitions
- ABSTRACT 123/32 123/139 123/52 MV in an electronically controlled fuel injection system, [51] Int. Cl. F02m 51/00 the electronic package is mounted on a finned heat [58] Field of s 'i'gii i'"Aw i g i dissipating pad extending horizontally from the air inlet body whereby heat generated during operation of the electronic package may be dissipated through the [56] References Clted fins to the atmosphere and to the air flow through the UNITED STATES PATENTS air inlet body 3,500,803 3 1970 Long 123 32 EA 3,421,825 1/1969 Maycock 123/148 E 2 Claims, 9 Drawing Flgures PATENTED JAN 1 5 H374 sum 1 or 4 FUEL INJECTION SYSTEM This invention relates to a fuel injection system having numerous advantages of construction and operation over those available heretofore.
- one surface of the pad has a plurality of recesses defining fins which dissipate heat to the atmosphere ambient the pad, and in addition, the pad conducts heat to the air inlet body for dissipation to the air flow therethrough.
- FIG. 1 is a side elevational view of a fuel injection system, also showing an air cleaner mounted'on the air inlet body but omitting any showing of the inlet manifold and other engine components for clarity of detail;
- FIG. 2 is a front elevational view of the fuel injection system, showing its relationship to the inlet manifold and cylinder heads;
- FIG. 3 is a top plan view of the fuel injection system, showing the bracket securing the air inlet body and the fuel rails into a single package for testing and shipping;
- FIG. 4 is a sectional view, as it would appear along line 44 of FIG. 3, showing one of the injectors mounted in the fuel rails and also showing the relationship of the components to the induction passage in the inlet manifold and cylinder heads;
- FIG. 5 is a sectional view, as it would appear along line 55 of FIG. 3, showing one of the air inlet fittings for the atmospheric air galleries in the fuel rails;
- FIG. 6 is a sectional view along line 6-6 of FIG. 4 showing the constructional details of one of the fuel injectors;
- FIG. 7 is a sectional view along line 77 of FIG. 2 showing the mounting of a fuel temperature thermistor
- FIG. 8 is a bottom plan view of the air inlet body and the heat conducting pad.
- FIG. 9 is a sectional view along line 9-9 of FIG. 8 showing further details of the heat conducting pad.
- the fuel injection system includes an air inlet body 110 and a pair of extruded fuel rails 12 and 14. Mounted on an inlet manifold 16 which in turn is mounted on cylinder heads 18 and 20, air inlet body has a pair of air inlet passages 22 and 24 which register with the induction passage 26 extending through inlet manifold 16 and heads 18 and to the combustion chamber inlet ports. Throttles 28 and 30 are disposed in inlet passages 22 and 24 on a rotatable shaft 32 for controlling air flow through induction passage 26.
- Air inlet body 110 also is provided with a transducer 34, such as that described in US. Ser. No. 202,760, filed Nov. 29, 1971, which measures the absolute pressure in air inlet passages 22 and 24 and induction passage 26 downstream of throttles 28 and 30 and provides an electrical signal proportional thereto.
- a transducer 34 such as that described in US. Ser. No. 202,760, filed Nov. 29, 1971, which measures the absolute pressure in air inlet passages 22 and 24 and induction passage 26 downstream of throttles 28 and 30 and provides an electrical signal proportional thereto.
- Air inlet body 10 also has provision for a curb idle ad justment 36 and a fast idle control valve 38 such as those shown in US. Ser. No. 41,141, filed May 25, 1970.
- air inlet body 18 also may include provision for a transducer 48 which provides an electrical signal indicative of a sudden increase in pressure in air inlet passages 22 and 24 and induction passage 26 downstream of throttles 28 and 38 and thus indicative of engine acceleration.
- air inlet body 18 includes provision for mounting a thermistor 42 which senses the temperature of the air entering air inlet passages 22 and 24 and induction passage 26.
- air inlet body 10 may include provision for an electrical switch 44 which is opened and closed by a throttle lever 46 secured on throttle shaft 32 and which thus indicates the position of throttles 28 and 38.
- An adjusting screw 48 may be provided to limit throttle closing movement of throttle lever 46.
- a heat conducting pad 50 extends horizontally from air inlet body 10 toward the rear of the engine. As shown in FIG. 8, a drilled passage 52 provides a manifold vacuum tap to which the manifold vacuum connection 54 shown in FIG. 3 may be mounted. Other fittings 56 also shown in FIG. 3 may be provided for various vacuum signals created as throttle 30 traverses various ports (not shown) provided in air inlet passage 24.
- vacuum taps such as that shown at 58 in FIG. 2, also may be provided.
- an electronic package 60 is mounted on heat conducting pad 50.
- Electronic package 60 receives electrical signals from the components, such as transducers 34 and 40, throttle switch 44, and thermistor 42, which meter air flow to the engine and controls energization of the injectors which meter fuel flow to the engine as described below.
- electronic package 60 is designed to mate with the heat transfer surface 62 of pad 50 whereby heat generated during operation of electronic package 60 may be conducted into heat conducting pad 50.
- the lower surface pf pad 50 has a plurality of elongated recesses 64 which define a plurality of fins 66 therebetween.
- Fins 66 radiate heat from pad 50 into the atmosphere ambient pad 58, space being provided between the lower portion of pad 50 and inlet manifold 16 to permit air circulation.
- Recesses 64 and fins 66 are generally parallel and their major axes extend longitudinally toward air inlet body 10, thus facilitating heat conduction to air inlet passages 22 and 24. Heat generated during operation of electronic package 60 also is dissipated, therefore, into the air flowing through inlet passages 22 and 24 to induction passage
- several ports 68 and 70 provided openings from air inlet passages 22 and 24, below throttles 28 and 30, to manifold pressure chambers 72 and 74.
- Manifold vacuum passage 52 extends from chamber 74, while manifold pressure transducer 34, idle air controls 36 and 38, and acceleration transducer 40, as well as other desired components, are associated with chamber 72.
- Fuel rail 12 extends longitudinally along the righthand bank of combustion chambers while fuel rail 14 extends longitudinally along the left-hand bank of combustion chambers. Rails 12 and 14 are shown in FIG. 2 as being mounted on inlet manifold 16, but provision could be made for mounting the rails on cylinder heads 18 and 20, if desired.
- rails 12 and 14 have fuel passages 76 and air passages or galleries 78 which are formed during the process of extruding rails 12 and 14.
- Air galleries 78 have fittings 80 provided with hoses 82 to receive air from an air cleaner 84.
- air cleaner 84 is supported by an adapter ring 85, received on a ledge 86 formed about air inlet body 10, and is secured by a stud 87.
- Each rail 12 and 14 has a plurality of injectors 88 retained, by clamps 90 as shown in FIG. 3, in sockets 92 formed as shown in FIG. 4. Sockets 92 intersect fuel passages 76, and rings 94 surrounding injectors 88 above and below passages 76 prevent leakage of fuel from sockets 92.
- each injector 88 has a screen 96 through which fuel is received from passage 76. Fuel passes from screen 96 through an opening 98 in the injector body 100 and then through a central bore 102 in the nozzle 103. A valve plunger 104 controls flow of fuel from bore 102 through nozzle opening 106. When energized by electronic package 60, a solenoid coil 108 lifts a magnetically responsive member 110 secured on the end of valve plunger 104, thus metering and delivering fuel from fuel passage 76 through injector socket 92, screen 96, opening 98, bore 102, and opening 106 into the base region 112 of socket 92.
- Nozzle opening 106 sprays the fuel through a critical flow orifice member 114 which is disposed in the outlet 115 opening from base region 112 of socket 92. Orifice members 114 are aimed through induction passage 26 toward the inlet ports for the combustion chambers located at the ends of induction passage 26.
- Branch passages 116 extend from air galleries 78 to base regions 112 of sockets 92 to provide atmospheric pressure regions at the outlets of injectors 88 and to supply a constant flow of air through orifice members 114. Branch passages 116 receive plugs 118 at the outer ends.
- the rearward end of rail 14 is provided with a filter housing 120 which receives fuel through a fitting 122 from a fuel pump such as that set forth in U.S.Ser. No. 211,934, filed Dec. 27, 1971.
- Filter housing 120 supplies fuel to fuel passage 76 in rail 14 and, through a crossover pipe 124, to a similar fuel passage in rail 12.
- a fitting 126 may be provided on the rearward end of rail 12 to receive fuel from crossover pipe 124.
- a fitting 128 houses a fuel temperature responsive thermistor 129 and provides a connection between fuel passage 76 in rail 14 and a crossover pipe 130 which extends to a fitting 132 at the forward end of rail 12.
- Fitting 132 includes means for bleeding fuel vapor from fuel passages 76 in rails 12 and 14 as set forth in U.S. Ser. No. 22l,640, filed Jan. 28, 1972.
- a bracket 134 is bolted at its outboard ends 136 and 138 to rails 12 and 14 and has a central portion 140 which is received on air cleaner adapter ring ledge 86 formed about air inlet body 10.
- a central arm 144 carries a bolt 146 which is received in a hole tapped in body to receive air cleaner stud 87, thereby securing bracket 134 to air inlet body 10.
- An air inlet assembly for an internal combustion engine having an induction passage for air flow to the engine, a nozzle for supplying fuel to the engine, electrically energizable means controlling fuel flow through said nozzle, and electronic means operable to energize said electrically energizable means, said electronic means operating at a temperature higher than the temperature ambient said air inlet assembly, said air inlet assembly comprising a unit having an air inlet body and having a heat conducting pad extending from said body, said body having an air inlet passage adapted for registration with said induction passage and including a throttle disposed in said air inlet passage for controlling air flow to the engine, said pad having one surface adapted for receiving said electronic means in heat exchange relationship and having another surface containing a plurality of elongated recesses which define a plurality of outwardly extending fins, whereby heat generated during operation of said electronic means may be conducted through said pad to said fins for dissipation to the atmosphere ambient said fins and to said air inlet body for dissipation to
- An air inlet assembly for an internal combustion engine having an induction passage for air flow to the engine, a nozzle for supplying fuel to the engine, electrically energizable means controlling fuel flow through said nozzle, and electronic means operable to energize said electrically energizable means, said electronic means operating at a temperature higher than the temperature ambient said air inlet assembly, said air inlet assembly comprising a unit having an air inlet body and having a heat conducting pad extending from said body, said body having an air inlet passage adapted for registration with said induction passage and including a throttle disposed in said air inlet passage for controlling air flow to the engine, said pad having one surface adapted for receiving said electronic means in heat exchange relationship and having another surface containing a plurality of elongated recesses which define a plurality of outwardly extending fins wherein the major axis of said elongated recesses and fins extends toward said air inlet body to maximize the cross-sectional area of said pad available for heat flow to said air inlet body
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Fuel-Injection Apparatus (AREA)
Abstract
In an electronically controlled fuel injection system, the electronic package is mounted on a finned heat dissipating pad extending horizontally from the air inlet body whereby heat generated during operation of the electronic package may be dissipated through the fins to the atmosphere and to the air flow through the air inlet body.
Description
Moulds Jan. 115, 11974 FUEL INJECTION SYSTEM OTHER PUBLICATIONS [75 1 Inventor: John Moulds Penfield Report On Transistor Ignition Systems, Reprinted by [73] Assignee: General Motors Corporation, Permission of Science and Mechanics, Feb. 15, 1963 Detroit, Mich.
Prima Examiner-Laurence M. Goodrid e 2 b. 18 1 72 W g 2] Filed Fe 9 Attorney-C. K. Veenstra [21] App]. No.: 227,461
[57] ABSTRACT [52] 123/32 123/139 123/52 MV in an electronically controlled fuel injection system, [51] Int. Cl. F02m 51/00 the electronic package is mounted on a finned heat [58] Field of s 'i'gii i'"Aw i g i dissipating pad extending horizontally from the air inlet body whereby heat generated during operation of the electronic package may be dissipated through the [56] References Clted fins to the atmosphere and to the air flow through the UNITED STATES PATENTS air inlet body 3,500,803 3 1970 Long 123 32 EA 3,421,825 1/1969 Maycock 123/148 E 2 Claims, 9 Drawing Flgures PATENTED JAN 1 5 H374 sum 1 or 4 FUEL INJECTION SYSTEM This invention relates to a fuel injection system having numerous advantages of construction and operation over those available heretofore.
Particular advantages may be noted in the mounting of the electronic package on a heat conducting pad extending from the induction air inlet body: one surface of the pad has a plurality of recesses defining fins which dissipate heat to the atmosphere ambient the pad, and in addition, the pad conducts heat to the air inlet body for dissipation to the air flow therethrough.
The details as well as other objects and advantages of this invention are set forth in the remainder of the specification and are shown in the drawings in which:
FIG. 1 is a side elevational view of a fuel injection system, also showing an air cleaner mounted'on the air inlet body but omitting any showing of the inlet manifold and other engine components for clarity of detail; FIG. 2 is a front elevational view of the fuel injection system, showing its relationship to the inlet manifold and cylinder heads;
FIG. 3 is a top plan view of the fuel injection system, showing the bracket securing the air inlet body and the fuel rails into a single package for testing and shipping;
FIG. 4 is a sectional view, as it would appear along line 44 of FIG. 3, showing one of the injectors mounted in the fuel rails and also showing the relationship of the components to the induction passage in the inlet manifold and cylinder heads;
FIG. 5 is a sectional view, as it would appear along line 55 of FIG. 3, showing one of the air inlet fittings for the atmospheric air galleries in the fuel rails;
FIG. 6 is a sectional view along line 6-6 of FIG. 4 showing the constructional details of one of the fuel injectors;
FIG. 7 is a sectional view along line 77 of FIG. 2 showing the mounting of a fuel temperature thermistor;
FIG. 8 is a bottom plan view of the air inlet body and the heat conducting pad; and
FIG. 9 is a sectional view along line 9-9 of FIG. 8 showing further details of the heat conducting pad.
Throughout the drawings, some portions of the electrical wiring and the air and vacuum hoses are illustrated but most portions of such have been omitted for a clearer illustration of other components of the fuel injection system.
Referring to the drawings, the fuel injection system includes an air inlet body 110 and a pair of extruded fuel rails 12 and 14. Mounted on an inlet manifold 16 which in turn is mounted on cylinder heads 18 and 20, air inlet body has a pair of air inlet passages 22 and 24 which register with the induction passage 26 extending through inlet manifold 16 and heads 18 and to the combustion chamber inlet ports. Throttles 28 and 30 are disposed in inlet passages 22 and 24 on a rotatable shaft 32 for controlling air flow through induction passage 26.
Air inlet body 110 also is provided with a transducer 34, such as that described in US. Ser. No. 202,760, filed Nov. 29, 1971, which measures the absolute pressure in air inlet passages 22 and 24 and induction passage 26 downstream of throttles 28 and 30 and provides an electrical signal proportional thereto.
If desired, air inlet body 18 also may include provision for a transducer 48 which provides an electrical signal indicative of a sudden increase in pressure in air inlet passages 22 and 24 and induction passage 26 downstream of throttles 28 and 38 and thus indicative of engine acceleration.
In addition, air inlet body 18 includes provision for mounting a thermistor 42 which senses the temperature of the air entering air inlet passages 22 and 24 and induction passage 26. Further, air inlet body 10 may include provision for an electrical switch 44 which is opened and closed by a throttle lever 46 secured on throttle shaft 32 and which thus indicates the position of throttles 28 and 38. An adjusting screw 48 may be provided to limit throttle closing movement of throttle lever 46.
A heat conducting pad 50 extends horizontally from air inlet body 10 toward the rear of the engine. As shown in FIG. 8, a drilled passage 52 provides a manifold vacuum tap to which the manifold vacuum connection 54 shown in FIG. 3 may be mounted. Other fittings 56 also shown in FIG. 3 may be provided for various vacuum signals created as throttle 30 traverses various ports (not shown) provided in air inlet passage 24.
Other vacuum taps, such as that shown at 58 in FIG. 2, also may be provided.
As shown in FIGS. 1 and 3, an electronic package 60 is mounted on heat conducting pad 50. Electronic package 60 receives electrical signals from the components, such as transducers 34 and 40, throttle switch 44, and thermistor 42, which meter air flow to the engine and controls energization of the injectors which meter fuel flow to the engine as described below. Referring to FIGS. 8 and 9, electronic package 60 is designed to mate with the heat transfer surface 62 of pad 50 whereby heat generated during operation of electronic package 60 may be conducted into heat conducting pad 50. The lower surface pf pad 50 has a plurality of elongated recesses 64 which define a plurality of fins 66 therebetween. Fins 66 radiate heat from pad 50 into the atmosphere ambient pad 58, space being provided between the lower portion of pad 50 and inlet manifold 16 to permit air circulation. Recesses 64 and fins 66 are generally parallel and their major axes extend longitudinally toward air inlet body 10, thus facilitating heat conduction to air inlet passages 22 and 24. Heat generated during operation of electronic package 60 also is dissipated, therefore, into the air flowing through inlet passages 22 and 24 to induction passage Still referring to FIGS. 8 and 9, it may be noted that several ports 68 and 70 provided openings from air inlet passages 22 and 24, below throttles 28 and 30, to manifold pressure chambers 72 and 74. Manifold vacuum passage 52 extends from chamber 74, while manifold pressure transducer 34, idle air controls 36 and 38, and acceleration transducer 40, as well as other desired components, are associated with chamber 72.
Fuel rail 12 extends longitudinally along the righthand bank of combustion chambers while fuel rail 14 extends longitudinally along the left-hand bank of combustion chambers. Rails 12 and 14 are shown in FIG. 2 as being mounted on inlet manifold 16, but provision could be made for mounting the rails on cylinder heads 18 and 20, if desired.
As shown in FIGS. 4 and 5, rails 12 and 14 have fuel passages 76 and air passages or galleries 78 which are formed during the process of extruding rails 12 and 14. Air galleries 78 have fittings 80 provided with hoses 82 to receive air from an air cleaner 84. As shown in FIG. 1, air cleaner 84 is supported by an adapter ring 85, received on a ledge 86 formed about air inlet body 10, and is secured by a stud 87.
Each rail 12 and 14 has a plurality of injectors 88 retained, by clamps 90 as shown in FIG. 3, in sockets 92 formed as shown in FIG. 4. Sockets 92 intersect fuel passages 76, and rings 94 surrounding injectors 88 above and below passages 76 prevent leakage of fuel from sockets 92.
As shown in FIG. 6, each injector 88 has a screen 96 through which fuel is received from passage 76. Fuel passes from screen 96 through an opening 98 in the injector body 100 and then through a central bore 102 in the nozzle 103. A valve plunger 104 controls flow of fuel from bore 102 through nozzle opening 106. When energized by electronic package 60, a solenoid coil 108 lifts a magnetically responsive member 110 secured on the end of valve plunger 104, thus metering and delivering fuel from fuel passage 76 through injector socket 92, screen 96, opening 98, bore 102, and opening 106 into the base region 112 of socket 92. Nozzle opening 106 sprays the fuel through a critical flow orifice member 114 which is disposed in the outlet 115 opening from base region 112 of socket 92. Orifice members 114 are aimed through induction passage 26 toward the inlet ports for the combustion chambers located at the ends of induction passage 26.
As best shown in FIG. 3, the rearward end of rail 14 is provided with a filter housing 120 which receives fuel through a fitting 122 from a fuel pump such as that set forth in U.S.Ser. No. 211,934, filed Dec. 27, 1971. Filter housing 120 supplies fuel to fuel passage 76 in rail 14 and, through a crossover pipe 124, to a similar fuel passage in rail 12. A fitting 126 may be provided on the rearward end of rail 12 to receive fuel from crossover pipe 124. At the forward end of rail 14, a fitting 128 houses a fuel temperature responsive thermistor 129 and provides a connection between fuel passage 76 in rail 14 and a crossover pipe 130 which extends to a fitting 132 at the forward end of rail 12. Fitting 132 includes means for bleeding fuel vapor from fuel passages 76 in rails 12 and 14 as set forth in U.S. Ser. No. 22l,640, filed Jan. 28, 1972.
As shown in FIG. 3, a bracket 134 is bolted at its outboard ends 136 and 138 to rails 12 and 14 and has a central portion 140 which is received on air cleaner adapter ring ledge 86 formed about air inlet body 10. A central arm 144 carries a bolt 146 which is received in a hole tapped in body to receive air cleaner stud 87, thereby securing bracket 134 to air inlet body 10. By this means, air inlet body 10 and rails 12 and 14 are secured in a single package whereby both air and fuel metering components of the fuel injection system may be tested and shipped as a single unit. If desired, the bracket may be removed during installation of the air inlet body 10 and rails 12 and 14 on the engine.
I claim:
1. An air inlet assembly for an internal combustion engine having an induction passage for air flow to the engine, a nozzle for supplying fuel to the engine, electrically energizable means controlling fuel flow through said nozzle, and electronic means operable to energize said electrically energizable means, said electronic means operating at a temperature higher than the temperature ambient said air inlet assembly, said air inlet assembly comprising a unit having an air inlet body and having a heat conducting pad extending from said body, said body having an air inlet passage adapted for registration with said induction passage and including a throttle disposed in said air inlet passage for controlling air flow to the engine, said pad having one surface adapted for receiving said electronic means in heat exchange relationship and having another surface containing a plurality of elongated recesses which define a plurality of outwardly extending fins, whereby heat generated during operation of said electronic means may be conducted through said pad to said fins for dissipation to the atmosphere ambient said fins and to said air inlet body for dissipation to air flow through said air inlet passage when the temperature of said electronic means is higher than the temperature ambient said air inlet assembly.
2. An air inlet assembly for an internal combustion engine having an induction passage for air flow to the engine, a nozzle for supplying fuel to the engine, electrically energizable means controlling fuel flow through said nozzle, and electronic means operable to energize said electrically energizable means, said electronic means operating at a temperature higher than the temperature ambient said air inlet assembly, said air inlet assembly comprising a unit having an air inlet body and having a heat conducting pad extending from said body, said body having an air inlet passage adapted for registration with said induction passage and including a throttle disposed in said air inlet passage for controlling air flow to the engine, said pad having one surface adapted for receiving said electronic means in heat exchange relationship and having another surface containing a plurality of elongated recesses which define a plurality of outwardly extending fins wherein the major axis of said elongated recesses and fins extends toward said air inlet body to maximize the cross-sectional area of said pad available for heat flow to said air inlet body, whereby heat generated during operation of said electronic means may be conducted through said pad to said fins for dissipation to the atmosphere ambient said fins and to said air inlet body for dissipation to air flow through said air inlet passage when the temperature of said electronic means is higher than the temperature ambient said air inlet assembly.
Claims (2)
1. An air inlet assembly for an internal combustion engine having an induction passage for air flow to the engine, a nozzle for supplying fuel to the engine, electrically energizable means controlling fuel flow through said nozzle, and electronic means operable to energize said electrically energizable means, said electronic means operating at a temperature higher than the temperature ambient said air inlet assembly, said air inlet assembly comprising a unit having an air inlet body and having a heat conducting pad extending from said body, said body having an air inlet passage adapted for registration with said induction passage and including a throttle disposed in said air inlet passage for controlling air flow to the engine, said pad having one surface adapted for receiving saId electronic means in heat exchange relationship and having another surface containing a plurality of elongated recesses which define a plurality of outwardly extending fins, whereby heat generated during operation of said electronic means may be conducted through said pad to said fins for dissipation to the atmosphere ambient said fins and to said air inlet body for dissipation to air flow through said air inlet passage when the temperature of said electronic means is higher than the temperature ambient said air inlet assembly.
2. An air inlet assembly for an internal combustion engine having an induction passage for air flow to the engine, a nozzle for supplying fuel to the engine, electrically energizable means controlling fuel flow through said nozzle, and electronic means operable to energize said electrically energizable means, said electronic means operating at a temperature higher than the temperature ambient said air inlet assembly, said air inlet assembly comprising a unit having an air inlet body and having a heat conducting pad extending from said body, said body having an air inlet passage adapted for registration with said induction passage and including a throttle disposed in said air inlet passage for controlling air flow to the engine, said pad having one surface adapted for receiving said electronic means in heat exchange relationship and having another surface containing a plurality of elongated recesses which define a plurality of outwardly extending fins wherein the major axis of said elongated recesses and fins extends toward said air inlet body to maximize the cross-sectional area of said pad available for heat flow to said air inlet body, whereby heat generated during operation of said electronic means may be conducted through said pad to said fins for dissipation to the atmosphere ambient said fins and to said air inlet body for dissipation to air flow through said air inlet passage when the temperature of said electronic means is higher than the temperature ambient said air inlet assembly.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US22746172A | 1972-02-18 | 1972-02-18 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3785354A true US3785354A (en) | 1974-01-15 |
Family
ID=22853206
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US00227461A Expired - Lifetime US3785354A (en) | 1972-02-18 | 1972-02-18 | Fuel injection system |
Country Status (1)
Country | Link |
---|---|
US (1) | US3785354A (en) |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4416241A (en) * | 1980-08-26 | 1983-11-22 | Robert Bosch Gmbh | Mixture formation system for mixture-compressing internal combustion engines with externally supplied ignition |
US4475486A (en) * | 1982-02-18 | 1984-10-09 | General Motors Corporation | Engine induction system |
US4503826A (en) * | 1981-04-22 | 1985-03-12 | General Motors Corporation | Fuel injection apparatus |
US4510909A (en) * | 1984-04-05 | 1985-04-16 | General Motors Corporation | Fuel rail assembly |
US4512314A (en) * | 1982-01-14 | 1985-04-23 | Mitsubishi Denki Kabushiki Kaisha | Fuel control apparatus for an internal combustion engine |
EP0141883A1 (en) * | 1983-07-06 | 1985-05-22 | General Motors Corporation | Fuel injection apparatus |
US4543914A (en) * | 1983-10-01 | 1985-10-01 | Lucas Industries Public Limited Company | Fuel pumping apparatus |
US4601275A (en) * | 1982-08-23 | 1986-07-22 | General Motors Corporation | Fuel rail |
US4763611A (en) * | 1985-11-22 | 1988-08-16 | Diesel Kiki Co., Ltd. | Electronically controlled fuel injection pump |
US4766869A (en) * | 1986-04-22 | 1988-08-30 | Weber S.R.L. | Housing system for a central electronic processing unit of a heat engine |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3421825A (en) * | 1965-06-03 | 1969-01-14 | Ass Elect Ind | Electric spark ignition units |
US3500803A (en) * | 1969-02-19 | 1970-03-17 | Gillett Tool Co | Electronic modulator circuit for precision fuel metering systems |
-
1972
- 1972-02-18 US US00227461A patent/US3785354A/en not_active Expired - Lifetime
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3421825A (en) * | 1965-06-03 | 1969-01-14 | Ass Elect Ind | Electric spark ignition units |
US3500803A (en) * | 1969-02-19 | 1970-03-17 | Gillett Tool Co | Electronic modulator circuit for precision fuel metering systems |
Non-Patent Citations (1)
Title |
---|
Report On Transistor Ignition Systems, Reprinted by Permission of Science and Mechanics, Feb. 15, 1963 * |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4416241A (en) * | 1980-08-26 | 1983-11-22 | Robert Bosch Gmbh | Mixture formation system for mixture-compressing internal combustion engines with externally supplied ignition |
US4503826A (en) * | 1981-04-22 | 1985-03-12 | General Motors Corporation | Fuel injection apparatus |
US4512314A (en) * | 1982-01-14 | 1985-04-23 | Mitsubishi Denki Kabushiki Kaisha | Fuel control apparatus for an internal combustion engine |
US4475486A (en) * | 1982-02-18 | 1984-10-09 | General Motors Corporation | Engine induction system |
US4601275A (en) * | 1982-08-23 | 1986-07-22 | General Motors Corporation | Fuel rail |
EP0141883A1 (en) * | 1983-07-06 | 1985-05-22 | General Motors Corporation | Fuel injection apparatus |
US4543914A (en) * | 1983-10-01 | 1985-10-01 | Lucas Industries Public Limited Company | Fuel pumping apparatus |
US4510909A (en) * | 1984-04-05 | 1985-04-16 | General Motors Corporation | Fuel rail assembly |
US4763611A (en) * | 1985-11-22 | 1988-08-16 | Diesel Kiki Co., Ltd. | Electronically controlled fuel injection pump |
US4766869A (en) * | 1986-04-22 | 1988-08-30 | Weber S.R.L. | Housing system for a central electronic processing unit of a heat engine |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3788287A (en) | Fuel injection system | |
JP2662007B2 (en) | Fuel injection system for multi-cylinder internal combustion engine | |
US3783844A (en) | Fuel injection system | |
US5357931A (en) | Supply device with built-in pipework | |
US3789819A (en) | Fuel rail vapor bleed | |
US3785354A (en) | Fuel injection system | |
US5533485A (en) | Fuel injection device for internal combustion engines | |
JPH0252101B2 (en) | ||
JPH04113778U (en) | vehicle fuel cooling system | |
JPS59155564A (en) | Fuel distributing pipe for fuel injection type engine | |
US4561396A (en) | Fuel control apparatus for an internal combustion engine | |
US4976462A (en) | Water cooling means for engine | |
US4924834A (en) | Integral device for forming and metering a mixture of air and fuel in an internal combustion engine fed by a multipoint injection system | |
US4512314A (en) | Fuel control apparatus for an internal combustion engine | |
JPH06501088A (en) | Devices for fuel lines in internal combustion engines | |
JP2002349384A (en) | V-type twin cylinder engine | |
US6688290B2 (en) | Integrated fuel delivery and electronic powertrain control module and method of manufacture | |
JPH0220829B2 (en) | ||
US11131279B1 (en) | Intake manifold | |
US4972808A (en) | Arrangement of cooling system for transversely mounted internal combustion engine | |
US2966344A (en) | Carburetor construction having a removable small venturi cluster | |
JP4253824B2 (en) | Engine intake system | |
US4041918A (en) | Fuel injection system | |
JP2512488B2 (en) | Fuel passage structure of fuel injection device | |
CA1274130A (en) | Fuel injection system |