EP3418551B1 - Method to calibrate a fuel injection pump - Google Patents
Method to calibrate a fuel injection pump Download PDFInfo
- Publication number
- EP3418551B1 EP3418551B1 EP18176648.6A EP18176648A EP3418551B1 EP 3418551 B1 EP3418551 B1 EP 3418551B1 EP 18176648 A EP18176648 A EP 18176648A EP 3418551 B1 EP3418551 B1 EP 3418551B1
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- EP
- European Patent Office
- Prior art keywords
- air
- fuel injection
- injection pump
- fuel
- engine
- 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.)
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- 239000000446 fuel Substances 0.000 title claims description 145
- 238000002347 injection Methods 0.000 title claims description 83
- 239000007924 injection Substances 0.000 title claims description 83
- 238000000034 method Methods 0.000 title claims description 27
- 239000012528 membrane Substances 0.000 claims description 25
- 238000002485 combustion reaction Methods 0.000 claims description 22
- 239000012530 fluid Substances 0.000 claims description 14
- 238000004891 communication Methods 0.000 claims description 12
- 230000008878 coupling Effects 0.000 claims description 4
- 238000010168 coupling process Methods 0.000 claims description 4
- 238000005859 coupling reaction Methods 0.000 claims description 4
- 238000012544 monitoring process Methods 0.000 claims description 2
- 238000012360 testing method Methods 0.000 description 5
- 230000004044 response Effects 0.000 description 3
- 230000008859 change Effects 0.000 description 2
- 230000001276 controlling effect Effects 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 230000002093 peripheral effect Effects 0.000 description 2
- 230000009467 reduction Effects 0.000 description 2
- 238000012546 transfer Methods 0.000 description 2
- 239000003638 chemical reducing agent Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000005065 mining Methods 0.000 description 1
- 238000010248 power generation Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 238000010998 test method Methods 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
Images
Classifications
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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
- F02M65/00—Testing fuel-injection apparatus, e.g. testing injection timing ; Cleaning of fuel-injection apparatus
- F02M65/002—Measuring fuel delivery of multi-cylinder injection pumps
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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
- F02M65/00—Testing fuel-injection apparatus, e.g. testing injection timing ; Cleaning of fuel-injection apparatus
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D1/00—Controlling fuel-injection pumps, e.g. of high pressure injection type
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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
- F02M59/00—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B49/00—Control, e.g. of pump delivery, or pump pressure of, or safety measures for, machines, pumps, or pumping installations, not otherwise provided for, or of interest apart from, groups F04B1/00 - F04B47/00
- F04B49/08—Regulating by delivery pressure
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B49/00—Control, e.g. of pump delivery, or pump pressure of, or safety measures for, machines, pumps, or pumping installations, not otherwise provided for, or of interest apart from, groups F04B1/00 - F04B47/00
- F04B49/12—Control, e.g. of pump delivery, or pump pressure of, or safety measures for, machines, pumps, or pumping installations, not otherwise provided for, or of interest apart from, groups F04B1/00 - F04B47/00 by varying the length of stroke of the working members
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B51/00—Testing machines, pumps, or pumping installations
Definitions
- This present disclosure relates to a method and a system for calibrating fuel injection pumps for start of fuel delivery into an engine.
- Japanese patent no. JPH10220323 relates to an inspecting device for a fuel injection pump capable of accurately judging the GO/NO-GO of a clearance between a pump body and a plunger.
- the inspecting device comprises a supplying pump for feeding out fuel to a clearance between the outer peripheral face of a plunger and inner peripheral face of the pump body.
- the weight and flow rate of the fuel passing through the clearance are measured in the relative position by changing the relative position between the pump body and the plunger.
- the GO/NO-GO of the clearance is judged based on the measurement result.
- Document GB 1 439 932 relates to an apparatus for testing fuel injector pumps.
- apparatus for testing fuel injector pumps.
- it is customary to provide apparatus incorporating a drive for the injector pump to be tested and a fuel system for supplying test fluid to the injector pump.
- Document GB 736,781 relates to the calibration of fuel-injection pumps for internal combustion engines, particularly diesel engines.
- a method of testing or calibrating a high pressure fuel-injection pump is described in which the pump is caused to deliver into a container which is pressurized to substantially the pressure to be encountered in the cylinders of the engine with which the pump is to be used.
- the conditions of measurement approximate to the conditions of use.
- the disclosure relates to a method for calibrating a fuel injection pump for a start of a fuel delivery.
- the method includes calibrating a pressure gauge of an air supply system to a target reading by providing an air flow from the air supply system to a calibration nozzle.
- the pressure gauge is configured to monitor a pressure differential across a membrane of the air supply system.
- the method further includes passing the air flow from the air supply-system through an air gap defined by one or more bores of the fuel injection pump, and monitoring a reading of the pressure gauge.
- the method also includes moving a plunger of the fuel injection pump to close, at least partly, the air gap to attain the target reading on the pressure gauge.
- the fuel injection pump is calibrated for the start of the fuel delivery when the target reading is attained.
- the disclosure relates to a calibration system for calibrating a fuel injection pump for a start of a fuel delivery into a combustion chamber of an engine.
- the fuel injection pump includes a cylinder, a plunger, and an air gap defined by one or more bores in the cylinder and the plunger.
- the calibration system includes an air supply system having a housing, a membrane, and a pressure gauge.
- the membrane is disposed within the housing and defines a first chamber and a second chamber within the housing.
- the first chamber and second chamber are configured to receive air from an air source.
- the pressure gauge is configured to monitor a pressure differential across the membrane.
- the pressure gauge is configured to be calibrated to a target reading.
- the air supply system is configured to be coupled to the fuel injection pump to provide an air flow through the air gap such that the second chamber is in fluid communication with the air gap.
- the fuel injection pump is calibrated for start of fuel delivery when the target reading of the pressure gauge is attained upon a movement of the plunger of the fuel injection pump.
- the engine 100 may be applied in machines, such as those that are applicable in a construction industry, a mining industry, a marine industry, an agricultural industry, a transport industry, etc. In some implementations, the engine 100 may be applied in stationary power generating machines, and to machines that are applied in commercial and domestic environments.
- the engine 100 includes a cylinder 102 and a piston 104 slidably disposed within the cylinder 102, and a fuel injection pump 106 configured to inject and deliver fuel into a combustion chamber 108 of the engine 100.
- the combustion chamber 108 is delimited by the piston 104, the cylinder 102, and a cylinder head 110 of the engine 100.
- the piston 104 is coupled to a connecting rod 112 that is in turn rotatably coupled to a crankshaft 114 of the engine 100, such that a reciprocal movement of the piston 104 translates into a rotary movement of the crankshaft 114.
- the crankshaft 114 is operatively coupled to a camshaft 116 of the engine 100 such that a rotary movement of the crankshaft 114 translates into a rotary movement of the camshaft 116.
- the camshaft 116 may be operatively coupled to the crankshaft 114 via a gear assembly 120.
- the gear assembly 120 may include a first gear 122 attached to the crankshaft 114 and a cam gearwheel 124 attached to the camshaft 116.
- an idler gear 126 may be disposed between the first gear 122 and the cam gearwheel 124 to transfer rotation of the first gear 122 to the cam gearwheel 124, and in turn facilitate a rotation/movement of the camshaft 116.
- a rotation/movement of the camshaft 116 facilitates an operation of the fuel injection pump 106, facilitating, and regulating in some cases, a fuel delivery into the combustion chamber 108 of the engine 100, for combustion.
- a fuel cam 130 is mounted on the camshaft 116 to operate the fuel injection pump 106.
- a lobe portion 132 of the fuel cam 130 which extends from a base circle 134 of the fuel cam 130 pushes a plunger 140 of the fuel injection pump 106 to initiate a delivery of fuel from the fuel injection pump 106 to the combustion chamber 108.
- a cam follower 138 may be disposed between the plunger 140 and the fuel cam 130, and contacts the fuel cam 130.
- the cam follower 138 may follow a profile of the fuel cam 130 to cause a movement of the plunger 140.
- the engine 100 may include multiple cylinders, and thus a configuration and working of the single cylinder, as shown, may be applicable to engines that use multiple cylinders, as well.
- the fuel injection pump 106 includes a cylinder 142 having a cylindrical wall 144 defining a cylindrical bore 146, and the plunger 140 slidably disposed within the cylindrical bore 146. Further, the fuel injection pump 106 includes one or more bores, for example, a first bore 150 and a second bore 152 extending in a radial direction relative to a central axis 154 of the cylindrical bore 146. The first bore 150 and second bore 152 extend through the entire thickness of the cylindrical wall 144, and are aligned with each other. The first bore 150, the second bore 152, and the cylindrical bore 146 together define an air gap 160 with the plunger 140, above the plunger 140.
- the plunger 140 and/or the cam follower 138 may be biased in a downward position by a spring 162.
- the plunger 140 is configured to move in an upward direction when pushed by the cam follower 138 as the cam follower 138 contacts the lobe portion 132 of the fuel cam 130.
- the fuel injection pump 106 is configured to deliver fuel into the combustion chamber 108 in response to a movement of the plunger 140 in the upward direction.
- the fuel injection pump 106 needs to start a delivery of the fuel into a combustion chamber 108 of the engine 100 at a desired time to initiate proper combustion and improved efficiency. To enable such a start of the fuel delivery, the fuel injection pump 106 needs to be calibrated. In certain implementation, the fuel injection pump 106 may be calibrated during an assembly of the engine 100.
- a calibration system 170 (shown in FIG. 3 ) is utilized.
- the calibration system 170 is configured to be connected with the fuel injection pump 106 to calibrate the fuel injection pump 106 for start of the fuel delivery.
- the calibration system 170 includes an air supply system 172, a fixed nozzle 174, and a calibration nozzle 176.
- the fixed nozzle 174 and the calibration nozzle 176 are configured to be coupled to the air supply system 172.
- the air supply system 172 is configured to be coupled to the fuel injection pump 106 for calibrating the fuel injection pump 106.
- the air supply system 172 includes a housing 180 forming an enclosure for receiving an air from an air source 182, a membrane 184 disposed within the housing 180 and dividing the enclosure into a first chamber 186 and a second chamber 188. Therefore, the membrane 184 defines the first chamber 186 towards a first side 187 of the membrane 184, and defines the second chamber 188 towards a second side 189 of the membrane 184.
- the air supply system 172 may further include a supply conduit 190, a first conduit 192 coupled to supply conduit 190 and the first chamber 186, and a second conduit 194 coupled to the supply conduit 190 and the second chamber 188.
- the air supply system 172 is configured to be coupled to the fuel injection pump 106 to provide an air flow through the air gap 160 such that the second chamber 188 is in fluid communication with the air gap 160 for calibrating the fuel injection pump 106.
- the supply conduit 190 is coupled to the air source 182 to receive an air at a pressure from the air source 182.
- the first conduit 192 facilitates a flow of the air received from the air source 182 via the supply conduit 190 to the first chamber 186.
- the second conduit 194 facilitates a flow of the air received from the air source 182 via the supply conduit 190 to the second chamber 188. Therefore, the first chamber 186 is in fluid communication with the air source 182 via the supply conduit 190, and the first conduit 192, while the second chamber 188 is in fluid communication with the air source 182 via the supply conduit 190 and the second conduit 194.
- a pressure reducer 196 may be connected to the supply conduit 190 to control a pressure of air supplied from the air source 182 to the air supply system 172. Further, a control valve 198 may also be coupled to the supply conduit 190 to control an amount of air received by the air supply system 172.
- the air source 182 may be a compressor, a pressurized air reservoir or any other similar system known in the art.
- the air supply system 172 further includes a pressure gauge 200 that is configured to monitor a pressure differential across the membrane 184. Therefore, the pressure gauge 200 is used to monitor a difference in pressures of the air in the first chamber 186 and the second chamber 188.
- the pressure gauge 200 may be a dial gauge (as shown in FIG. 3 ).
- the pressure gauge 200 may be in contact with the membrane 184 to detect the pressure differential across the membrane 184.
- a tip of the pressure gauge 200 which is in abutment with the membrane 184, moves in response to a movement of the membrane 184.
- the membrane 184 may move due the pressure difference that may exist between the first chamber 186 and the second chamber 188.
- a reading of the pressure gauge 200 may change, indicating a value of pressure differential between the first chamber 186 and the second chamber 188 (i.e. across the membrane 184).
- the pressure of air in the first chamber 186 may be controlled by the fixed nozzle 174
- the fixed nozzle 174 may be fluidly coupled to the first chamber 186.
- the pressure in the first chamber 186 may be a function of an air gap (not shown) existing in the fixed nozzle 174.
- the fixed nozzle 174 may be in fluid communication with the air source 182 and the first chamber 186 via a first channel 202 of the air supply system 172.
- the first channel 202 may be coupled to the first conduit 192 and may facilitate an air flow (also referred to as flow of air) from the first conduit 192 to the fixed nozzle 174.
- the calibration nozzle 176 may be selectively fluidly coupled to air supply system 172 for controlling the pressure of air in the second chamber 188, and therefore, the pressure of air acting on the second side 189 of the membrane 184.
- the calibration nozzle 176 may be coupled to the air supply system 172 via a second channel 204 of the air supply system 172.
- the second channel 204 facilitates a flow of air from the air source 182 to the calibration nozzle 176 via the second conduit 194. Therefore, the calibration nozzle 176 may be in communication with the air source 182 and the second chamber 188 via the second channel 204.
- the pressure of air in the second chamber 188 may be a function of an air gap (not shown) existing in the calibration nozzle 176.
- the air gap in the calibration nozzle 176 may be selected based on a desired air gap in the fuel injection pump 106 for a desired start of the fuel delivery from the fuel injection pump 106 into the combustion chamber 108 of the engine 100.
- a shut-off valve 208 may be disposed in the second channel 204 upstream of the calibration nozzle 176. By operating the shut-off valve 208, a flow of air from the air source 182 to the calibration nozzle 176 may be started and/or stopped.
- the calibration nozzle 176 may be removably coupled to the second channel 204, and the second channel 204 may be connectable to the one of the bores 150, 152 of the fuel injection pump 106. Such a feature may enable the calibration nozzle 176 to be removed from the second channel 204 to allow the second channel 204 to be directly coupled to the fuel injection pump 106 for calibrating the fuel injection pump 106.
- the calibration nozzle 176 is fluidly coupled to the second chamber 188 to control a pressure of air acting on a second side 189 of membrane 184 to calibrate the pressure gauge 200 to a target reading corresponding to a desired pressure differential across the membrane 184.
- the desired pressure differential and hence the target reading corresponds to a pressure differential that needs to be achieved to calibrate the fuel injection pump 106 for the start of fuel delivery into the combustion chamber 108 of the engine 100.
- the method 400 includes a step 402 that includes calibration of the pressure gauge 200 to the target reading.
- a flow of air from the air supply system 172 to the calibration nozzle 176 is enabled.
- the calibration nozzle 176 is coupled to the second channel 204, thereby providing the flow of air from the air source 182 to the calibration nozzle 176 through the second conduit 194 and the second channel 204.
- the shut-off valve 208 may be actuated to enable the flow of air to the calibration nozzle 176 from the air supply system 172. Further, the air from the air source 182 enters the second chamber 188 via the second conduit 194 and pressurizes the second chamber 188. As the second chamber 188 is also in fluid communication with the calibration nozzle 176, the pressure of air inside the second chamber 188 may be a function of the air gap of the calibration nozzle 176. Owing to the air gap of the calibration nozzle 176, the air in the second chamber 188 may be at a first pressure 'P1'.
- the air from air source 182 enters into the first chamber 186 via the first conduit 192, and pressurize the first chamber 186.
- the pressure of air inside the first chamber 186 may be a function of the air gap of the fixed nozzle 174.
- the air in the first chamber 186 may be at a second pressure 'P2'. Due to the pressure differential across the membrane 184, the pressure gauge 200 will show a reading that corresponds to the target reading. In this manner, the pressure gauge 200 is calibrated to the targeted reading.
- the flow of the air to the calibration nozzle 176 is disabled/stopped before passing the air flow through the air gap 160 of the fuel injection pump 106.
- the air supply system 172 is fluidly decoupled from the calibration nozzle 176 before establishing a fluid coupling between the air supply system 172 and the fuel injection pump 106.
- the air supply system 170 is coupled to the fuel injection pump 106 such that the second chamber 188 is in fluid communication with the air gap 160.
- the calibration nozzle 176 may be removed from the second channel 204.
- the second channel 204 may be directly coupled to the first bore 150 to enable a flow or air through the air gap 160 from the air supply system 172.
- the shut-off valve 208 may be controlled to stop supply of air from the air supply system 172 to the calibration nozzle 176.
- a third channel 210 of the air supply system 172 may be coupled with the first bore 150 to enable a flow or air through the air gap 160 from the air supply system 172.
- the method 400 moves to a step 404 that includes passing the air from the air supply system 172, through the air gap 160 of the fuel injection pump 106.
- the fuel cam 130 may be moved/turned to the base circle 134 such that the cam follower 138 abuts/contacts the base circle 134 of the fuel cam 130.
- the air supply system 172 is coupled to the fuel injection pump 106 such that the air gap 160 is in fluid communication with the second chamber 188 and the air source 182 though the first bore 150.
- the air supply system 172 may be coupled to the fuel injection pump 106 by coupling the second channel 204 to the first bore 150 after removing the calibration nozzle 176 from the air supply system 172.
- the third channel 210 may be coupled to the first bore 150 to enable a flow of air provided by the air source 182 and the air supply system 172 through the air gap 160. In such a case, the flow of air to the calibration nozzle 176 may be disabled by controlling the shut-off valve 208.
- a valve 212 may be disposed on the third channel 210 to control a flow of air from the air source 182 through the air supply system 172 to the air gap 160. Upon enabling the flow of air through the air gap 160 a reading of the pressure gauge 200 is monitored.
- the method 400 moves to step 406.
- the plunger 140 of the fuel injection pump 106 is moved to, at least partially, close the air gap 160 to attain the target reading on the pressure gauge 200.
- the plunger 140 of the fuel injection pump 106 may be moved by rotating the crankshaft 114 and subsequently the camshaft 116 in a direction that corresponds to a rotation of crankshaft 114 when the engine 100 produces power.
- a control rod of the fuel injection pump 106 may be brought a full load position before moving the crankshaft 114 and camshaft 116.
- the cam follower 138 may come in contact with the lobe portion 132, and may follow the profile of the lobe portion 132 upon further rotation of the camshaft 116.
- the movement of the cam follower 138 may cause the plunger 140 to move in the upward direction, causing reduction of the air gap 160 of the fuel injection pump 106.
- the reduction in the air gap 160 may result in an increase in the pressure into the second chamber 188 of the air supply system 172. In so doing, a reading on the pressure gauge 200 changes and moves towards the target reading.
- the plunger 140 is moved in the upward direction by rotating the camshaft 116 till the reading on the pressure gauge 200 reaches the target reading.
- a graduated disc (not shown) may be mounted on the crankshaft 114 to indicate a position of the piston 104 before a top dead center (TDC) of the cylinder 102.
- the position of the piston 104 indicated by the graduated disc upon attainment of the target reading, may differ from a designed fuel injection timing.
- the designed fuel injection timing may correspond to a specified position of the piston 104 before the TDC.
- the designed fuel injection timing may correspond to a position of the piston 104 which is 10 degrees before the TDC.
- the piston 104 When the position of the piston 104 differs from the specified position, the piston 104 may be moved to the specified position to enable a start of fuel delivery into the combustion chamber 108 at the designed fuel injection timing. For so doing, the camshaft 116 is decoupled from the crankshaft 114 so as to prevent a transfer of a motion of the piston 104/ crankshaft 114 to the camshaft 116, and subsequently to the plunger 140. In certain implementations, the decoupling of the camshaft 116 from the crankshaft 114 may be achieved by decoupling the cam gearwheel 124 from the camshaft 116.
- decoupling of the cam gearwheel 124 from the camshaft 116 is performed by hydraulically expanding the cam gearwheel 124 attached to the camshaft 116.
- the crankshaft 114 may be moved to move the piston 104 to the specified position before TDC.
- the specified position may correspond to the position of the piston 104 at the designed fuel injector timing, and therefore the start of the fuel delivery into the combustion chamber 108 of the engine 100.
- the specified position of the piston 104 may be indicated by the graduated disc.
- the crankshaft 114 is again coupled to the camshaft 116. In this manner, the fuel injection pump 106 is calibrated for start of fuel delivery into the combustion chamber 108 of the engine 100 at the designed fuel injection timing.
- the piston 104 may be moved away from the specified position by rotating the crankshaft 114 in a direction opposite to the direction of a rotation of the crankshaft 114 in which the crankshaft 114 rotates when the engine 100 generates power. This results into a change in the reading of the pressure gauge 200. Thereafter, the piston 104 may be moved at the specified position by rotating the crankshaft 114 in the direction of rotation of the crankshaft 114 that results into generation of power. As the piston 104 reaches the specified positon, the reading indicated by the pressure gauge 200 reaches the target reading and therefore confirms an accurate calibration of the fuel injection pump 106 for the start of the fuel delivery at the designed fuel injection timing.
- the calibration of the fuel injection pump 106 for start of fuel delivery into the combustion chamber 108 of the engine 100 can be performed on an assembly line. Further, calibration system 170 and the method 400 as explained above reduces the overall time required for calibration of fuel injection pump 106 for start of fuel delivery into the combustion chamber 108 of the engine 100.
- an engine may include multiple cylinders.
- the start of the fuel delivery from a fuel injection pump for a first cylinder is calibrated in a manner explained above.
- the steps 402, 404, and 406, are performed. Thereafter, shims of appropriate thickness may be utilized.
- the engine with multiple cylinders may include a lower valve drive that may include one or more blocks to which cam followers of the fuel injection pumps are mounted. In such a case, shims may be inserted between the block and an engine block defining the cylinders of the engine.
- the engine may be a right turning engine.
- shims of greater thickness are inserted to enable a late start of delivery of fuel relative to the start of fuel delivery in the first cylinder.
- shims of reduced thickness may be inserted to enable an early start of fuel delivery relative to the start of fuel delivery into the first cylinder.
- the engine may be a left turning engine.
- shims of greater thickness are inserted to enable an early start of delivery of fuel relative to the start of fuel delivery in the first cylinder.
- shims of greater thickness may be inserted to enable a late start of fuel delivery relative to the start of fuel delivery into the first cylinder.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Fuel-Injection Apparatus (AREA)
Description
- This present disclosure relates to a method and a system for calibrating fuel injection pumps for start of fuel delivery into an engine.
- It is a common practice for conventional fuel injection systems, applied in various power generation systems, such as engines, to be calibrated for a start of fuel delivery. Typically, a start of fuel delivery from such fuel injection pumps is calibrated in standardized environment settings, such by mounting the engine on a test bench. Moving the engine to the test bench may be tedious and time consuming. Further, such a process also involves a wastage of fuel.
- Japanese patent no.
JPH10220323 - Document
GB 1 439 932 - Document
GB 736,781 - In one aspect, the disclosure relates to a method for calibrating a fuel injection pump for a start of a fuel delivery. The method includes calibrating a pressure gauge of an air supply system to a target reading by providing an air flow from the air supply system to a calibration nozzle. The pressure gauge is configured to monitor a pressure differential across a membrane of the air supply system. The method further includes passing the air flow from the air supply-system through an air gap defined by one or more bores of the fuel injection pump, and monitoring a reading of the pressure gauge. The method also includes moving a plunger of the fuel injection pump to close, at least partly, the air gap to attain the target reading on the pressure gauge. The fuel injection pump is calibrated for the start of the fuel delivery when the target reading is attained.
- In another aspect, the disclosure relates to a calibration system for calibrating a fuel injection pump for a start of a fuel delivery into a combustion chamber of an engine. The fuel injection pump includes a cylinder, a plunger, and an air gap defined by one or more bores in the cylinder and the plunger. The calibration system includes an air supply system having a housing, a membrane, and a pressure gauge. The membrane is disposed within the housing and defines a first chamber and a second chamber within the housing. The first chamber and second chamber are configured to receive air from an air source. The pressure gauge is configured to monitor a pressure differential across the membrane. The pressure gauge is configured to be calibrated to a target reading. The air supply system is configured to be coupled to the fuel injection pump to provide an air flow through the air gap such that the second chamber is in fluid communication with the air gap. The fuel injection pump is calibrated for start of fuel delivery when the target reading of the pressure gauge is attained upon a movement of the plunger of the fuel injection pump.
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FIG. 1 is a diagrammatic view of an engine, in accordance with an aspect of the present disclosure; -
FIG. 2 is a diagrammatic view depicting certain components of the engine, in accordance with an aspect of the present disclosure; -
FIG. 3 is a schematic view of a calibration system connected to a fuel injection pump of the engine, in accordance with an aspect of the present disclosure; and -
FIG. 4 is a flowchart depicting a method to calibrate the fuel injection pump, in accordance with an aspect of the present disclosure. - Referring to
FIG. 1 andFIG. 2 anengine 100 is illustrated. Theengine 100 may be applied in machines, such as those that are applicable in a construction industry, a mining industry, a marine industry, an agricultural industry, a transport industry, etc. In some implementations, theengine 100 may be applied in stationary power generating machines, and to machines that are applied in commercial and domestic environments. - The
engine 100 includes acylinder 102 and apiston 104 slidably disposed within thecylinder 102, and afuel injection pump 106 configured to inject and deliver fuel into acombustion chamber 108 of theengine 100. Thecombustion chamber 108 is delimited by thepiston 104, thecylinder 102, and acylinder head 110 of theengine 100. Thepiston 104 is coupled to a connectingrod 112 that is in turn rotatably coupled to acrankshaft 114 of theengine 100, such that a reciprocal movement of thepiston 104 translates into a rotary movement of thecrankshaft 114. Thecrankshaft 114 is operatively coupled to acamshaft 116 of theengine 100 such that a rotary movement of thecrankshaft 114 translates into a rotary movement of thecamshaft 116. Thecamshaft 116 may be operatively coupled to thecrankshaft 114 via agear assembly 120. Thegear assembly 120 may include afirst gear 122 attached to thecrankshaft 114 and acam gearwheel 124 attached to thecamshaft 116. In an embodiment, anidler gear 126 may be disposed between thefirst gear 122 and thecam gearwheel 124 to transfer rotation of thefirst gear 122 to thecam gearwheel 124, and in turn facilitate a rotation/movement of thecamshaft 116. - A rotation/movement of the
camshaft 116 facilitates an operation of thefuel injection pump 106, facilitating, and regulating in some cases, a fuel delivery into thecombustion chamber 108 of theengine 100, for combustion. To this end, afuel cam 130 is mounted on thecamshaft 116 to operate thefuel injection pump 106. As thecamshaft 116 is rotated, alobe portion 132 of thefuel cam 130 which extends from abase circle 134 of thefuel cam 130 pushes aplunger 140 of thefuel injection pump 106 to initiate a delivery of fuel from thefuel injection pump 106 to thecombustion chamber 108. Acam follower 138 may be disposed between theplunger 140 and thefuel cam 130, and contacts thefuel cam 130. As thefuel cam 130 rotates, thecam follower 138 may follow a profile of thefuel cam 130 to cause a movement of theplunger 140. Although a single cylinder is shown, theengine 100 may include multiple cylinders, and thus a configuration and working of the single cylinder, as shown, may be applicable to engines that use multiple cylinders, as well. - Referring to
FIGS. 1 and3 , thefuel injection pump 106 includes acylinder 142 having acylindrical wall 144 defining acylindrical bore 146, and theplunger 140 slidably disposed within thecylindrical bore 146. Further, thefuel injection pump 106 includes one or more bores, for example, afirst bore 150 and asecond bore 152 extending in a radial direction relative to acentral axis 154 of thecylindrical bore 146. Thefirst bore 150 andsecond bore 152 extend through the entire thickness of thecylindrical wall 144, and are aligned with each other. Thefirst bore 150, thesecond bore 152, and thecylindrical bore 146 together define anair gap 160 with theplunger 140, above theplunger 140. Theplunger 140 and/or thecam follower 138 may be biased in a downward position by aspring 162. Theplunger 140 is configured to move in an upward direction when pushed by thecam follower 138 as thecam follower 138 contacts thelobe portion 132 of thefuel cam 130. Further, thefuel injection pump 106 is configured to deliver fuel into thecombustion chamber 108 in response to a movement of theplunger 140 in the upward direction. Thefuel injection pump 106 needs to start a delivery of the fuel into acombustion chamber 108 of theengine 100 at a desired time to initiate proper combustion and improved efficiency. To enable such a start of the fuel delivery, thefuel injection pump 106 needs to be calibrated. In certain implementation, thefuel injection pump 106 may be calibrated during an assembly of theengine 100. - To calibrate the
fuel injection pump 106 for starting the fuel delivery into thecombustion chamber 108 of theengine 100, a calibration system 170 (shown inFIG. 3 ) is utilized. Thecalibration system 170 is configured to be connected with thefuel injection pump 106 to calibrate thefuel injection pump 106 for start of the fuel delivery. Referring toFIG. 3 , thecalibration system 170 includes anair supply system 172, a fixednozzle 174, and acalibration nozzle 176. The fixednozzle 174 and thecalibration nozzle 176 are configured to be coupled to theair supply system 172. Theair supply system 172 is configured to be coupled to thefuel injection pump 106 for calibrating thefuel injection pump 106. Theair supply system 172 includes ahousing 180 forming an enclosure for receiving an air from anair source 182, amembrane 184 disposed within thehousing 180 and dividing the enclosure into afirst chamber 186 and asecond chamber 188. Therefore, themembrane 184 defines thefirst chamber 186 towards afirst side 187 of themembrane 184, and defines thesecond chamber 188 towards asecond side 189 of themembrane 184. Theair supply system 172 may further include asupply conduit 190, afirst conduit 192 coupled to supplyconduit 190 and thefirst chamber 186, and asecond conduit 194 coupled to thesupply conduit 190 and thesecond chamber 188. Theair supply system 172 is configured to be coupled to thefuel injection pump 106 to provide an air flow through theair gap 160 such that thesecond chamber 188 is in fluid communication with theair gap 160 for calibrating thefuel injection pump 106. - The
supply conduit 190 is coupled to theair source 182 to receive an air at a pressure from theair source 182. Thefirst conduit 192 facilitates a flow of the air received from theair source 182 via thesupply conduit 190 to thefirst chamber 186. Similarly, thesecond conduit 194 facilitates a flow of the air received from theair source 182 via thesupply conduit 190 to thesecond chamber 188. Therefore, thefirst chamber 186 is in fluid communication with theair source 182 via thesupply conduit 190, and thefirst conduit 192, while thesecond chamber 188 is in fluid communication with theair source 182 via thesupply conduit 190 and thesecond conduit 194. - In an embodiment, a
pressure reducer 196 may be connected to thesupply conduit 190 to control a pressure of air supplied from theair source 182 to theair supply system 172. Further, acontrol valve 198 may also be coupled to thesupply conduit 190 to control an amount of air received by theair supply system 172. In an embodiment, theair source 182 may be a compressor, a pressurized air reservoir or any other similar system known in the art. - The
air supply system 172 further includes apressure gauge 200 that is configured to monitor a pressure differential across themembrane 184. Therefore, thepressure gauge 200 is used to monitor a difference in pressures of the air in thefirst chamber 186 and thesecond chamber 188. In certain implementations, thepressure gauge 200 may be a dial gauge (as shown inFIG. 3 ). Thepressure gauge 200 may be in contact with themembrane 184 to detect the pressure differential across themembrane 184. In an embodiment, a tip of thepressure gauge 200 which is in abutment with themembrane 184, moves in response to a movement of themembrane 184. Themembrane 184 may move due the pressure difference that may exist between thefirst chamber 186 and thesecond chamber 188. In response to the movement of the tip of thepressure gauge 200, a reading of thepressure gauge 200 may change, indicating a value of pressure differential between thefirst chamber 186 and the second chamber 188 (i.e. across the membrane 184). - Further, the pressure of air in the
first chamber 186, and therefore, the pressure of air acting on afirst side 187 of themembrane 184, may be controlled by the fixednozzle 174 For this purpose, the fixednozzle 174 may be fluidly coupled to thefirst chamber 186. The pressure in thefirst chamber 186 may be a function of an air gap (not shown) existing in the fixednozzle 174. The fixednozzle 174 may be in fluid communication with theair source 182 and thefirst chamber 186 via afirst channel 202 of theair supply system 172. Thefirst channel 202 may be coupled to thefirst conduit 192 and may facilitate an air flow (also referred to as flow of air) from thefirst conduit 192 to the fixednozzle 174. - In an embodiment, the
calibration nozzle 176 may be selectively fluidly coupled toair supply system 172 for controlling the pressure of air in thesecond chamber 188, and therefore, the pressure of air acting on thesecond side 189 of themembrane 184. Thecalibration nozzle 176 may be coupled to theair supply system 172 via asecond channel 204 of theair supply system 172. Thesecond channel 204 facilitates a flow of air from theair source 182 to thecalibration nozzle 176 via thesecond conduit 194. Therefore, thecalibration nozzle 176 may be in communication with theair source 182 and thesecond chamber 188 via thesecond channel 204. In certain scenarios, when thecalibration nozzle 176 is in fluid communication with thesecond chamber 188 via thesecond channel 204, the pressure of air in thesecond chamber 188 may be a function of an air gap (not shown) existing in thecalibration nozzle 176. In an embodiment, the air gap in thecalibration nozzle 176 may be selected based on a desired air gap in thefuel injection pump 106 for a desired start of the fuel delivery from thefuel injection pump 106 into thecombustion chamber 108 of theengine 100. In an embodiment, a shut-offvalve 208 may be disposed in thesecond channel 204 upstream of thecalibration nozzle 176. By operating the shut-offvalve 208, a flow of air from theair source 182 to thecalibration nozzle 176 may be started and/or stopped. - In an embodiment, the
calibration nozzle 176 may be removably coupled to thesecond channel 204, and thesecond channel 204 may be connectable to the one of thebores fuel injection pump 106. Such a feature may enable thecalibration nozzle 176 to be removed from thesecond channel 204 to allow thesecond channel 204 to be directly coupled to thefuel injection pump 106 for calibrating thefuel injection pump 106. - The
calibration nozzle 176 is fluidly coupled to thesecond chamber 188 to control a pressure of air acting on asecond side 189 ofmembrane 184 to calibrate thepressure gauge 200 to a target reading corresponding to a desired pressure differential across themembrane 184. The desired pressure differential and hence the target reading corresponds to a pressure differential that needs to be achieved to calibrate thefuel injection pump 106 for the start of fuel delivery into thecombustion chamber 108 of theengine 100. - Referring to
FIG. 4 amethod 400 for calibrating thefuel injection pump 106 for start of fuel delivery is now explained. Themethod 400 is explained in conjunction withFIGS. 1 ,2 , and3 . Themethod 400 includes astep 402 that includes calibration of thepressure gauge 200 to the target reading. For calibrating thepressure gauge 200, a flow of air from theair supply system 172 to thecalibration nozzle 176 is enabled. To do so, according to an embodiment, thecalibration nozzle 176 is coupled to thesecond channel 204, thereby providing the flow of air from theair source 182 to thecalibration nozzle 176 through thesecond conduit 194 and thesecond channel 204. In an embodiment, the shut-offvalve 208 may be actuated to enable the flow of air to thecalibration nozzle 176 from theair supply system 172. Further, the air from theair source 182 enters thesecond chamber 188 via thesecond conduit 194 and pressurizes thesecond chamber 188. As thesecond chamber 188 is also in fluid communication with thecalibration nozzle 176, the pressure of air inside thesecond chamber 188 may be a function of the air gap of thecalibration nozzle 176. Owing to the air gap of thecalibration nozzle 176, the air in thesecond chamber 188 may be at a first pressure 'P1'. - Further, the air from
air source 182 enters into thefirst chamber 186 via thefirst conduit 192, and pressurize thefirst chamber 186. As thefirst chamber 186 is also in fluid communication with the fixednozzle 174, the pressure of air inside thefirst chamber 186 may be a function of the air gap of the fixednozzle 174. Owing to the air gap of the fixednozzle 174, the air in thefirst chamber 186 may be at a second pressure 'P2'. Due to the pressure differential across themembrane 184, thepressure gauge 200 will show a reading that corresponds to the target reading. In this manner, thepressure gauge 200 is calibrated to the targeted reading. After calibrating thepressure gauge 200 to the target reading, the flow of the air to thecalibration nozzle 176 is disabled/stopped before passing the air flow through theair gap 160 of thefuel injection pump 106. Thus, theair supply system 172 is fluidly decoupled from thecalibration nozzle 176 before establishing a fluid coupling between theair supply system 172 and thefuel injection pump 106. Theair supply system 170 is coupled to thefuel injection pump 106 such that thesecond chamber 188 is in fluid communication with theair gap 160. For fluidly decoupling theair supply system 172 from thecalibration nozzle 176, in an embodiment, thecalibration nozzle 176 may be removed from thesecond channel 204. In such a case, thesecond channel 204 may be directly coupled to thefirst bore 150 to enable a flow or air through theair gap 160 from theair supply system 172. Alternatively, the shut-offvalve 208 may be controlled to stop supply of air from theair supply system 172 to thecalibration nozzle 176. In such a case, for establishing a fluid coupling between theair supply system 172 and thefuel injection pump 106, athird channel 210 of theair supply system 172 may be coupled with thefirst bore 150 to enable a flow or air through theair gap 160 from theair supply system 172. - Now, the
method 400 moves to astep 404 that includes passing the air from theair supply system 172, through theair gap 160 of thefuel injection pump 106. In an embodiment, before passing the air through theair gap 160, thefuel cam 130 may be moved/turned to thebase circle 134 such that thecam follower 138 abuts/contacts thebase circle 134 of thefuel cam 130. To enable the flow of the air through theair gap 160, theair supply system 172 is coupled to thefuel injection pump 106 such that theair gap 160 is in fluid communication with thesecond chamber 188 and theair source 182 though thefirst bore 150. In an embodiment, theair supply system 172 may be coupled to thefuel injection pump 106 by coupling thesecond channel 204 to thefirst bore 150 after removing thecalibration nozzle 176 from theair supply system 172. In another embodiment, thethird channel 210 may be coupled to thefirst bore 150 to enable a flow of air provided by theair source 182 and theair supply system 172 through theair gap 160. In such a case, the flow of air to thecalibration nozzle 176 may be disabled by controlling the shut-offvalve 208. In an embodiment, avalve 212 may be disposed on thethird channel 210 to control a flow of air from theair source 182 through theair supply system 172 to theair gap 160. Upon enabling the flow of air through the air gap 160 a reading of thepressure gauge 200 is monitored. - Thereafter, the
method 400 moves to step 406. In thestep 406, theplunger 140 of thefuel injection pump 106 is moved to, at least partially, close theair gap 160 to attain the target reading on thepressure gauge 200. Theplunger 140 of thefuel injection pump 106 may be moved by rotating thecrankshaft 114 and subsequently thecamshaft 116 in a direction that corresponds to a rotation ofcrankshaft 114 when theengine 100 produces power. In an embodiment, a control rod of thefuel injection pump 106 may be brought a full load position before moving thecrankshaft 114 andcamshaft 116. Upon movement of thefuel cam 130 due to the rotation of thecamshaft 116, thecam follower 138 may come in contact with thelobe portion 132, and may follow the profile of thelobe portion 132 upon further rotation of thecamshaft 116. The movement of thecam follower 138 may cause theplunger 140 to move in the upward direction, causing reduction of theair gap 160 of thefuel injection pump 106. The reduction in theair gap 160 may result in an increase in the pressure into thesecond chamber 188 of theair supply system 172. In so doing, a reading on thepressure gauge 200 changes and moves towards the target reading. Theplunger 140 is moved in the upward direction by rotating thecamshaft 116 till the reading on thepressure gauge 200 reaches the target reading. Further movement of theplunger 140 is stopped as thepressure gauge 200 attains the target reading. The position of theplunger 140 upon attaining the targeted reading corresponds to the start of fuel delivery from thefuel injection pump 106. In this manner, thefuel injection pump 106 is calibrated for the start of the fuel delivery when the target reading is attained. - In certain implementations, a graduated disc (not shown) may be mounted on the
crankshaft 114 to indicate a position of thepiston 104 before a top dead center (TDC) of thecylinder 102. In an implementation, the position of thepiston 104 indicated by the graduated disc, upon attainment of the target reading, may differ from a designed fuel injection timing. The designed fuel injection timing may correspond to a specified position of thepiston 104 before the TDC. In an exemplary embodiment, the designed fuel injection timing may correspond to a position of thepiston 104 which is 10 degrees before the TDC. - When the position of the
piston 104 differs from the specified position, thepiston 104 may be moved to the specified position to enable a start of fuel delivery into thecombustion chamber 108 at the designed fuel injection timing. For so doing, thecamshaft 116 is decoupled from thecrankshaft 114 so as to prevent a transfer of a motion of thepiston 104/crankshaft 114 to thecamshaft 116, and subsequently to theplunger 140. In certain implementations, the decoupling of thecamshaft 116 from thecrankshaft 114 may be achieved by decoupling thecam gearwheel 124 from thecamshaft 116. In an embodiment, decoupling of thecam gearwheel 124 from thecamshaft 116 is performed by hydraulically expanding thecam gearwheel 124 attached to thecamshaft 116. After decoupling thecrankshaft 114 from thecamshaft 116, thecrankshaft 114 may be moved to move thepiston 104 to the specified position before TDC. The specified position may correspond to the position of thepiston 104 at the designed fuel injector timing, and therefore the start of the fuel delivery into thecombustion chamber 108 of theengine 100. The specified position of thepiston 104 may be indicated by the graduated disc. Upon moving and positioning thepiston 104 at the specified position, thecrankshaft 114 is again coupled to thecamshaft 116. In this manner, thefuel injection pump 106 is calibrated for start of fuel delivery into thecombustion chamber 108 of theengine 100 at the designed fuel injection timing. - In an optional embodiment, to check an accurate start of fuel delivery at the designed fuel injection timing, the
piston 104 may be moved away from the specified position by rotating thecrankshaft 114 in a direction opposite to the direction of a rotation of thecrankshaft 114 in which thecrankshaft 114 rotates when theengine 100 generates power. This results into a change in the reading of thepressure gauge 200. Thereafter, thepiston 104 may be moved at the specified position by rotating thecrankshaft 114 in the direction of rotation of thecrankshaft 114 that results into generation of power. As thepiston 104 reaches the specified positon, the reading indicated by thepressure gauge 200 reaches the target reading and therefore confirms an accurate calibration of thefuel injection pump 106 for the start of the fuel delivery at the designed fuel injection timing. By using thecalibration system 170 and themethod 400 as explained above, the calibration of thefuel injection pump 106 for start of fuel delivery into thecombustion chamber 108 of theengine 100 can be performed on an assembly line. Further,calibration system 170 and themethod 400 as explained above reduces the overall time required for calibration offuel injection pump 106 for start of fuel delivery into thecombustion chamber 108 of theengine 100. - In certain implementations, an engine may include multiple cylinders. In such a case, the start of the fuel delivery from a fuel injection pump for a first cylinder is calibrated in a manner explained above. For calibrating a start of fuel delivery for the other cylinders from the corresponding fuel injection pumps, the
steps - It should be understood that the above description is intended for illustrative purposes only and is not intended to limit the scope of the present disclosure. Thus, one skilled in the art will appreciate that other aspects of the disclosure may be obtained from a study of the drawings, the disclosure, and the appended claim.
Claims (10)
- A method (400) for calibrating a fuel injection pump (106) for a start of a fuel delivery, the method (400) comprising:calibrating a pressure gauge (200) of an air supply system (172) to a target reading by providing an air flow from the air supply system (172) to a calibration nozzle (176), the pressure gauge (200) is configured to monitor a pressure differential across a membrane (184) of the air supply system (172);passing the air flow from the air supply system (172) through an air gap (160) defined by one or more bores (150,152) of the fuel injection pump (106), and monitoring a reading of the pressure gauge (200); andmoving a plunger (140) of the fuel injection pump (106) to close, at least partly, the air gap (160) to attain the target reading on the pressure gauge (200), wherein the fuel injection pump (106) is calibrated for the start of the fuel delivery when the target reading is attained.
- The method (400) of claim 1, further comprising stopping the air flow to the calibration nozzle (176) before passing the air flow through the air gap (160) of the fuel injection pump (106).
- The method (400) of claim 1, wherein the fuel injection pump (106) is configured to deliver fuel into a combustion chamber (108) of an engine (100), wherein moving the plunger (140) includes rotating a camshaft (116) of the engine (100).
- The method (400) of claim 1, wherein the fuel injection pump (106) is configured to deliver fuel into a combustion chamber (108) of an engine (100), the method (400) further including turning a fuel cam (130) of the engine (100) to a base circle (134) of the fuel cam (130) before passing the air flow through the air gap (160).
- The method (400) of claim 1, wherein the fuel injection pump (106) is configured to deliver fuel into a combustion chamber (108) of an engine (100), the method (400) further including decoupling a camshaft (116) of the engine (100) from a crankshaft (114) of the engine (100) and moving a piston (104) of the engine (100) to a specified position before a top dead center (TDC) by rotating the crankshaft (114), wherein the specified position corresponds to the start of the fuel delivery.
- The method (400) of claim 5, wherein decoupling is performed by hydraulically expanding a cam gearwheel (124) attached to the camshaft (116).
- The method (400) of claim 5 further including coupling the camshaft (116) with the crankshaft (114) after moving the piston (104) to the specified position before TDC.
- The method (400) of claim 1, wherein a fixed nozzle (174) is coupled to the air supply system (172), the fixed nozzle (174) being configured to control a pressure of air acting on a first side (187) of the membrane (184).
- The method (400) of claim 1, wherein the calibration nozzle (176) is coupled to the air supply system (172), the calibration nozzle (176) being configured to control a pressure of air acting on a second side (189) of the membrane (184).
- A calibration system (170) for calibrating a fuel injection pump (106) for a start of a fuel delivery into a combustion chamber (108) of an engine (100), the fuel injection pump (106) includes a cylinder (142), a plunger (140), and an air gap (160) defined by one or more bores (150,152) in the cylinder (142) and the plunger (140), the calibration system (170) comprising:
an air supply system (172) including:a housing (180);a membrane (184) disposed within the housing (180) and defining a first chamber (186) and a second chamber (188) within the housing (180), the first chamber (186) and the second chamber (188) configured to receive air from an air source (182); anda pressure gauge (200) configured to monitor a pressure differential across the membrane (184), the pressure gauge (200) configured to be calibrated to a target reading,wherein the air supply system (172) is configured to be coupled to the fuel injection pump (106) to provide an air flow through the air gap (160) such that the second chamber (188) is in fluid communication with the air gap (160), andwherein the fuel injection pump (106) is calibrated for the start of the fuel delivery when the target reading of the pressure gauge (200) is attained upon a movement of the plunger (140) of the fuel injection pump (106).
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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GB1710058.7A GB2563663A (en) | 2017-06-23 | 2017-06-23 | Method to calibrate a fuel injection pump |
Publications (3)
Publication Number | Publication Date |
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EP3418551A2 EP3418551A2 (en) | 2018-12-26 |
EP3418551A3 EP3418551A3 (en) | 2019-01-02 |
EP3418551B1 true EP3418551B1 (en) | 2020-07-29 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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EP18176648.6A Active EP3418551B1 (en) | 2017-06-23 | 2018-06-07 | Method to calibrate a fuel injection pump |
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EP (1) | EP3418551B1 (en) |
GB (1) | GB2563663A (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
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GB2554731B (en) * | 2016-10-07 | 2019-04-03 | Caterpillar Motoren Gmbh & Co | Piston pump having push rod assembly and stopping assembly |
CN112628047B (en) * | 2020-12-14 | 2022-09-13 | 中国船舶重工集团公司第七一一研究所 | High-pressure common rail system test bed oil injection flow measuring system and calibration method |
CN114263555B (en) * | 2021-09-09 | 2023-09-12 | 翟泉来 | Verification device for fuel spray nozzle of engine of miniature ship |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB736781A (en) * | 1952-01-11 | 1955-09-14 | Fuel Injection & Engineering S | Improvements in or relating to the testing and calibration of fuel-injection pumps |
US3354874A (en) * | 1965-02-09 | 1967-11-28 | Publicite Francaise | Device for regulating a fuel injection pump for an internal combustion engine as a function of the depression prevailing in the induction pipe |
GB1296284A (en) * | 1969-11-14 | 1972-11-15 | ||
GB1439932A (en) * | 1972-04-10 | 1976-06-16 | Hartridge Ltd Leslie | Apparatus for testing fuel injector pumps |
SU1106918A1 (en) * | 1983-01-14 | 1984-08-07 | Чувашский сельскохозяйственный институт | Device for diagnosis of injection pump plunger pair |
-
2017
- 2017-06-23 GB GB1710058.7A patent/GB2563663A/en not_active Withdrawn
-
2018
- 2018-06-07 EP EP18176648.6A patent/EP3418551B1/en active Active
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None * |
Also Published As
Publication number | Publication date |
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GB201710058D0 (en) | 2017-08-09 |
EP3418551A2 (en) | 2018-12-26 |
GB2563663A (en) | 2018-12-26 |
EP3418551A3 (en) | 2019-01-02 |
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