EP3601778B1 - A fuel pump for supplying fuel to an internal combustion piston engine - Google Patents
A fuel pump for supplying fuel to an internal combustion piston engine Download PDFInfo
- Publication number
- EP3601778B1 EP3601778B1 EP17717208.7A EP17717208A EP3601778B1 EP 3601778 B1 EP3601778 B1 EP 3601778B1 EP 17717208 A EP17717208 A EP 17717208A EP 3601778 B1 EP3601778 B1 EP 3601778B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- space
- space section
- pump
- piston member
- fuel
- 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.)
- Active
Links
- 239000000446 fuel Substances 0.000 title claims description 66
- 238000002485 combustion reaction Methods 0.000 title claims description 8
- 238000007789 sealing Methods 0.000 claims description 26
- 238000005461 lubrication Methods 0.000 claims description 24
- 239000000463 material Substances 0.000 claims description 10
- 230000033001 locomotion Effects 0.000 claims description 9
- 238000005086 pumping Methods 0.000 claims description 7
- 239000003921 oil Substances 0.000 description 19
- 239000000314 lubricant Substances 0.000 description 7
- 239000007789 gas Substances 0.000 description 6
- 230000000694 effects Effects 0.000 description 4
- 230000005540 biological transmission Effects 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 230000004323 axial length Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 230000005489 elastic deformation Effects 0.000 description 1
- 238000007373 indentation Methods 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 239000012528 membrane Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000010705 motor oil Substances 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
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
- 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
- F02M59/44—Details, components parts, or accessories not provided for in, or of interest apart from, the apparatus of groups F02M59/02 - F02M59/42; Pumps having transducers, e.g. to measure displacement of pump rack or piston
-
- 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
- F02M55/00—Fuel-injection apparatus characterised by their fuel conduits or their venting means; Arrangements of conduits between fuel tank and pump F02M37/00
- F02M55/007—Venting means
-
- 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
- F02M59/02—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps of reciprocating-piston or reciprocating-cylinder type
- F02M59/10—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps of reciprocating-piston or reciprocating-cylinder type characterised by the piston-drive
- F02M59/102—Mechanical drive, e.g. tappets or cams
-
- 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
- F02M63/00—Other fuel-injection apparatus having pertinent characteristics not provided for in groups F02M39/00 - F02M57/00 or F02M67/00; Details, component parts, or accessories of fuel-injection apparatus, not provided for in, or of interest apart from, the apparatus of groups F02M39/00 - F02M61/00 or F02M67/00; Combination of fuel pump with other devices, e.g. lubricating oil pump
- F02M63/0001—Fuel-injection apparatus with specially arranged lubricating system, e.g. by fuel oil
-
- 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
- F04B1/00—Multi-cylinder machines or pumps characterised by number or arrangement of cylinders
- F04B1/04—Multi-cylinder machines or pumps characterised by number or arrangement of cylinders having cylinders in star- or fan-arrangement
- F04B1/0404—Details or component parts
-
- 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
- F04B1/00—Multi-cylinder machines or pumps characterised by number or arrangement of cylinders
- F04B1/04—Multi-cylinder machines or pumps characterised by number or arrangement of cylinders having cylinders in star- or fan-arrangement
- F04B1/0404—Details or component parts
- F04B1/0443—Draining of the housing; Arrangements for handling leaked fluids
-
- 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
- F04B39/00—Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00
- F04B39/02—Lubrication
-
- 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
- F04B53/00—Component parts, details or accessories not provided for in, or of interest apart from, groups F04B1/00 - F04B23/00 or F04B39/00 - F04B47/00
- F04B53/18—Lubricating
-
- 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
- F02M59/44—Details, components parts, or accessories not provided for in, or of interest apart from, the apparatus of groups F02M59/02 - F02M59/42; Pumps having transducers, e.g. to measure displacement of pump rack or piston
- F02M59/442—Details, components parts, or accessories not provided for in, or of interest apart from, the apparatus of groups F02M59/02 - F02M59/42; Pumps having transducers, e.g. to measure displacement of pump rack or piston means preventing fuel leakage around pump plunger, e.g. fluid barriers
Definitions
- the invention relates to a fuel pump according to the preamble of claim 1.
- Internal combustion piston engines need to be provided with one or more fuel pumps.
- the fuel injection in so called common rail systems into the combustion chambers of the engine requires capability of pumping the fuel into high pressure of even above 250 MPa.
- the pumps are typically lubricated by the lubrication oil of the engine the presence of both the fuel and the lubrication oil in the pump may call for special attention particularly relating to preventing or minimizing the mixing of the fuel and the lubricant in the pump.
- Document EP 1 184 568 A2 discloses a fuel pump according to the preamble of claim 1.
- Document EP 0976926 B1 discloses an integrated pump and tappet unit for supplying fuel to an internal combustion engine, such as a large diesel engine, the unit comprising a body part enclosing a tappet member, whose axial movement is governed by movement of a cam surface provided on a cam shaft or the like, and a piston member operationally connected to the tappet member and which is arranged to pump fuel under high pressure from a fuel chamber disposed within the body part.
- the body part is a single member housing both said tappet member and said fuel chamber and the tappet member and the piston member are connected to each other by means of a tappet arm, which is sealed to a flange member fixed to the body part, so that fuel from the fuel chamber is prevented from coming into contact with the tappet member.
- Document DE 102015002304 A1 discloses a high pressure fuel pump. Document is silent about the possible leakage of the fuel into the lubrication oil but shows a lubrication system of the pump.
- the pump comprises a pump housing having an inner space, a pump plunger with a guide surface, which is guided in the interior space on the pump housing, wherein the interior space and the pump plunger limits a spring chamber of the high-pressure fuel pump, a lubricant line which opens into the interior space against the guide surface of the plunger, a vent pipe, by means of which the lubricant can be discharged from the spring chamber.
- Document DE102008042067 A1 discloses a pump which has a drive shaft provided with an eccentric cam, and a piston accommodated in a cylinder.
- the document discloses circular membrane seals used for separating the fuel and lubrication systems from each other.
- Document DE102006059333 A1 discloses a fuel pump comprising at least one wiper element integrated in the pump piston for removing leakage fuel collecting between the pump cylinder and the pump piston from the cylinder wall.
- the wiper element is a scraper ring that removes leakage fuel accumulating on the wall of the pump cylinder and guides it into at least one leakage groove.
- US7308849 defines a work chamber and driven at least indirectly by a drive shaft in a reciprocating motion, counter to the force of a restoring spring.
- the pump piston is braced on the drive shaft at least indirectly via a sleeve like tappet, and the restoring spring engages at least the pump piston.
- a support element in the tappet braces the pump piston toward the drive shaft and is braced at least indirectly on the drive shaft.
- the restoring spring via a spring plate, engages the pump piston and the tappet.
- the spring plate is elastically deformable in the direction of motion of the pump piston in such a way that as a result of its elastic deformation, deviations in the position of its contact faces on the pump piston and on the tappet are compensated for.
- WO2011160908 A1 discloses a pump which comprises at least one pump element which has a pump piston that is at least indirectly driven in a stroke movement by a drive shaft.
- a plunger having a plunger body is arranged between the drive shaft and the pump piston and is movably guided in a receiving device in the direction of the stroke movement of the pump piston and is supported on the drive shaft by means of a support element.
- Lubricant is supplied to the receiving device via a supply line and lubricant is conducted out of the receiving device via a discharge line into the plunger body to the support element.
- An annular gap filter is provided between the plunger body and the receiving device and is arranged between the supply line for supplying lubricant to the receiving device and the discharge line for discharging lubricant into the plunger body.
- An object of the invention is to provide a fuel pump for supplying fuel to an internal combustion piston engine in which the performance is considerably improved compared to the prior art solutions.
- a fuel pump according to claim 1 is provided.
- the vent flow path is provided with a one-way valve allowing flow towards the second space section.
- the discharge flow path is provided with a one-way valve allowing flow away from the second space section.
- the annular gap in the second space section circumscribes the first space section at least partially such that the annular gap and the first space section are overlapping with each other in the direction of the central axis of the cylindrical space.
- the cylindrical extension is a bushing removably attached to the body of the pump.
- the present invention is suitable for use as a high pressure pump in a common rail fuel system.
- FIG. 1 depicts schematically a fuel pump 10 configured to supply fuel to an internal combustion piston engine. More particularly the pump is a high pressure pump configured to deliver fuel at a pressure of above 200 MPa.
- the pump 10 is provided with a supply rail 12 and a high pressure rail 14 which are both in connection with a first pump chamber 16 arranged to a body 18 of the pump 10.
- the body 18 comprising the pump chamber 16 may also be referred to as a barrel of the pump 10.
- the supply rail 12 is connected to the pump chamber 16 via an intake conduit 20.
- the high pressure rail is connected to the pump chamber 16 via an outlet conduit 22.
- the intake conduit 20 is provided with a one-way valve 24 configured to allow fuel to flow only from the supply rail 12 to the pump chamber 16.
- the outlet conduit 22 is provided with a one-way valve 26 configure to allow fuel to flow only from the pump chamber 16 to the high pressure rail 14.
- the supply rail 12 and the high pressure rail 14 are integrated into the body 18 but it is conceivable that the rails are external to the body 18.
- the pump 10 is also provided with a piston member 28 which is arranged into a cylindrical space 30 arranged into the body 18.
- the cylindrical space 30 has a central axis 32 and it is substantially rotationally symmetrical in respect to the central axis 32. Therefore the piston member 28 is also rotationally symmetrical in respect to the central axis 32.
- the outer form of the body may be designed according to the needs.
- the piston member 28 is arranged into the space in re-ciprocatable manner.
- the piston member 28 has a first end 28' which borders the cylindrical space 30 at an end thereof forming the first pumping chamber 16.
- the piston has also a second end 28" opposite to the first end 28'.
- the piston member 28 is configured to reciprocate in the space 30 provided for the piston member 28 and pump the fuel.
- the piston member 28 is advantageously an assembly of several parts, which is here illustrated so that the first end 28' and the second end 28" are separate parts removably connected to each other.
- the cylindrical space 30 comprises a first space section 30' which has a first diameter D1.
- the wall of the space section and the wall of the piston member 28 are arranged against each other providing a first sealing gap 34 between the walls, which also guides the piston member 28 in the body 18. Additionally the wall of the first space section guides the piston member in the body 18 while it reciprocates in the space.
- the piston member 28 comprises a first portion which is arranged into the first space section 30' and has a diameter substantially same as the first diameter such that a desired guidance and sealing is provided.
- the cylindrical space 30 comprises also a second space section 30" which has a second diameter D2, being greater than the first diameter D1.
- the second space section 30" is on same central axis as the first space section 30'.
- the piston member 28 comprises a second portion which is arranged in the second space section 30" such that a desired guidance and sealing is provided.
- the wall of the second space section and the wall of the piston member 28 are arranged against each other providing a second sealing gap 35 between the walls, respectively. Additionally the wall of the second space section guides the piston member at its second portion in the body 18 while the piston member reciprocates in the space.
- the second pump chamber 16' is arranged to a body 18 of the pump 10.
- the second pump chamber 16' is arranged in connection with the second space section 30" such that second pump chamber 16' is configured to use empty space of the second space section 30" as the pump chamber.
- the piston member 28 is arranged to border both the first and the second pump chamber 16, 16'.
- the piston member 28 and the first and the second pump chambers are configured in the pump shown in the figure 1 such that volumes of the first and the second pump chambers are changing same way i.e. either increasing or decreasing, during the piston member is moving to one direction.
- the wall of the space section and the wall of the piston member 28 are arranged against each other providing the first sealing gap 34 between the walls.
- the first sealing gap 34 separates the first pump chamber 16 and the second pump chamber 16' and it is of annular form. Since the first pump chamber 16 operates as a high pressure pump configured to deliver fuel at a pressure at above 200 MPa the fuel in the first pump chamber tends to flow into the first sealing gap 34 and further to flow through the sealing gap 34. Even if not shown here the first sealing gap 34 between the pump chambers 16, 16' may be provided with means to collect fuel material flown from the first pump chamber 16 into the first sealing gap 34. Such a means may comprise a groove arranged to the wall of the first space section provided with a conduit to lead the fuel material to further processing. Since the second pump chamber 16' is within the second space section 30" there may be commonly referred to in the following.
- the pump 10 is provided with means for transferring fuel material away from the second pump chamber 16'. Therefore firstly the pump 10 is provided with a vent flow path 36.
- the vent flow path 36 runs through the body 18 of the pump and connects the second pump chamber 16 which is formed into the second space section 30" to outside of the body 18.
- the vent flow path 36 is configured to allow gas admission into the second space section 30", driven by the reciprocating movement of the piston member.
- the pump 10 is further provided with a discharge flow path 38 connecting the second pump chamber 16' to outside of the body 18 configured to transfer fuel material entered into the second pump chamber 16' or the second space section 30" via the sealing gap 34 away from the second space section 30" i.e. the second pump chamber 16'.
- the vent flow path 36 is provided with a one-way valve 40 which allows gas flow in the vent flow path 36 in the direction towards the second space section 30" and prevent back flow of the fluid.
- the vent flow path 36 has an inlet which opens into the surroundings of the pump 10.
- the discharge flow path 38 is provided with a one-way valve 42 configured to allow flow away from the second space section 30" via the discharge flow path 38.
- the piston member 28 is at its first extreme position where the first pump chamber 16 has its smallest volume.
- the piston member 28 is movable by an external force, depicted by an arrow 44, which may be provided directly by the operation of the engine.
- the piston member 28 is provided with a sleeve member 46 which connects to the second end 28" of the piston member 28 and which has a closed end i.e. a bottom 58.
- the bottom 58 of the sleeve member 46 extends radially to the piston member 28.
- the sleeve member 46 may be integral to or separate part from the second end 28" of the piston member 28 and/or the sleeve member 46.
- the bottom 58 of the sleeve member 46 is therefore common with the piston member 28 and it serves for receiving the force needed for reciprocate the piston member 28 in the pump 10.
- the sleeve member is arranged such that an annular space is provided between the sleeve member 46 and the piston member 28, which now forms the second pump space 16'.
- the sleeve member 46 opens towards the first end 28' of the piston member 28.
- the sleeve member is arranged into the second space section 30" such that the radially inner wall of the second space section 30" and the radially outer wall of the sleeve member 46 are against each other providing a second sealing gap 35.
- the wall of the second space section 30" guides the sleeve member 46 of the piston member 28 in the body 18 when the piston member 28 and sleeve member are moving along the central axis 32.
- the body 18 of the pump 10 is provided with a cylindrical extension 48 towards the second end of the piston member 28 which extension is coaxial to the first space section 30'.
- the cylindrical extension 48 has an axial length in the direction of the central axis 32 and an outer diameter smaller than the second diameter D2.
- the cylindrical extension 48 extends axially into the second space section 30". This way the cylindrical extension 48 forms an annular gap 47 radially between the cylindrical extension 48 of the body and the inner wall of the body.
- the annular gap 47 circumscribes the first space section at least partially such that the annular gap of the second space section 30" and the first space 30' section are overlapping with each other in the direction of the central axis 32 of the cylindrical space.
- the sleeve member 46 is arranged to extend into said annular gap 47.
- the end face of the cylindrical extension 48 borders the second pump chamber 16' together with the piston member 28 and the sleeve member 46.
- the fitting of the sleeve member 46 extending into the annular gap between the cylindrical extension 48 and the second space section 30" is such that the radially inner wall of the annular gap i.e. the cylindrical outer wall of the extension 48 and the radially inner wall of the sleeve member 46 are against each other providing a third sealing gap 37.
- third space section 60 arranged into the annular gap radially between the cylindrical extension 48 and the inner wall of the body and the sleeve member 49 which borders the third space section.
- the third space section serves for purposes of lubrication the pump 10.
- the pump 10 is provided with lubrication oil supply channel 62 and a lubrication oil discharge channel 64.
- the minimum volume of the third space section 60 and the locations and/dimensions of the lubrication oil supply channel 62 and the lubrication oil discharge channel 64 are configured to allow a formation of a pond of lubrication oil in the third space section but preventing a total filling of the third space section with the lubrication oil.
- the lubrication oil supply channel 62 and the lubrication oil discharge channel 64 are dimensioned so that the flow rate of the lubrication oil out from the third space section 60 is at least in the long run greater than the flow rate of the lubrication oil in to the third space section 60.
- the vent flow path 36 extends through the body 18 to the inner wall of the second space section 30" where its outlet 50 is arranged.
- the vent flow path 36 continues in the sleeve member 46 and it opens into the second pump chamber 16' via an outlet 52 of the vent flow path.
- the transition area between the vent flow path 36 in the body 18 and in the sleeve member 46 is provided with an oblong space 54 extending in the direction of the center axis 32 into which space the vent flow path opens. This way the flow path is open at all operational positions of the piston member 28 and the sleeve member 46.
- the vent flow path and the discharge flow path may be realized by providing suitable bores, grooves or otherwise provided channels into the material of the pump 10.
- the oblong space 54 is provided as an indentation, into the outer wall of the sleeve member 46, but it is conceivable to arrange that also to the inner wall of the body 18.
- the discharge flow path 38 is provided with similar oblong space 54 for bring about a flow connection between discharge flow path 38 in the piston member 28 and in the body 18.
- the external force 44 is advantageously brought about by a power system of the engine. Therefore the piston member 28 is in mechanical force transmission connection, typically indirectly, with the crankshaft of the engine. In practise this mean that mechanical force transmission is lubricated by the engine lubricant.
- the pump 10 is provided with means for transferring fuel material away from the second pump chamber 16' any fuel material which escapes through the sealing gap 34 will not find its way into the lubrication oil of the engine.
- vent flow path 36 and discharge flow path 38 inlets and outlets into the piston member and the body.
- the oblong spaces 54 are located so that situated that the vent flow path 36 is open when the piston part is in a suction stroke which makes is possible to balance the created underpressure in the second pump chamber 16'.
- the vent flow path 36 and discharge flow path 38 inlets and outlets are so arranged that when the piston member moves towards it first end 28' the vent flow path is closed and the pressure is increasing in the second pump chamber 16'. At a certain position of the piston member 28 the discharge flow path 38 opens and the second pump chamber is discharged.
- FIG 3 which shows an example which is not a part of the claimed invention
- a pump unit 10 where the structure of the second pump chamber 16' is different to that shown in the figures 1 and 2 .
- the piston member 28 extends from its first end through a guide flange 56 to a cam drive system (not shown) of the pump 10.
- the piston member 28 is provided with a bottom 58 as a radial extension part, which borders the second pump chamber 16'.
- the radial distal end of the bottom 58 is adequately sealed against the inner wall of the second space section 30" such that pumping effect can be obtained by the second pump space 16'..
- a feature that is common to all of the figures 1 - 3 is that the discharge flow path 38 opens into a part which borders the second pump chamber 16' farthest from the first end of the piston member.
- the discharge flow path 38 opens into lowest position in the second pump chamber 16'.
- the center axis 32 need not be exactly vertical but the pump may be tilted as long as the discharge flow path is arranged to substantially lowest position into the second pump chamber 16'.
- FIG 4 there is shown an embodiment of the invention where the pump 10 is configured to be installed such that the first end 28' of the piston member 28 is horizontally below the second end 28" of the piston member 28.
- the basic configuration of the pump 10 is similar to that shown in the figure 1 being though such features, which are effected by the departing orientation, designed differently.
- the first sealing gap 34 is provided with a fuel scraper ring 68 in an annular space arranged to minimize the flow of fuel into the second space section 30".
- annular space 67 closer to the first pump chamber 16 from which a fuel discharge channel 66 is extending to outside the body 18.
- similar fuel scraper ring 68 and fuel discharge channel 66 may be arranged to the pumps shown in the figures 1 to 3 . This arrangement decreases the amount of fuel flow through the first sealing gap 34 to the second pump space 16', but the fuel directed to the fuel discharge channel 66 is still at considerably high pressure.
- the second space section 30" is provided with a bushing 70.
- the bushing is generally cylindrical part having an outwardly extending shoulder at its first end. It is at its first end attached to the inner surface of the second space section 30" and it is provided with a section having a smaller diameter than the second space section 30" such that an annular space 60 is provided between the bushing 70 and the inner surface of the section space section 30".
- the bushing 70 is attached at its first end, on the side of the first end 28' of the piston member 28, to the body 18.
- the piston member 28 comprises a sleeve member 46 which is arranged in the second space section 30" such that a desired guidance and sealing is provided corresponding to the figures 1 and 2 .
- the inner wall of the second space section 30" and the wall of the sleeve member 46 are arranged against each other providing a second sealing gap 35 between the walls, respectively.
- the sleeve member 46 is arranged to extend into said annular gap 60 formed by the bushing 70 and the wall of the second space section 30". This way the bushing 70 borders the second pump chamber 16' together with sleeve member 46 and the piston member 28.
- the fitting of the sleeve member 46 to extend into the annular gap between the bushing 70 and wall of the second space section 30" is such that the radially inner wall of the annular gap i.e. the radially outer wall of the bushing 70 and the radially inner wall of the sleeve member 46 are against each other providing a third sealing gap 37.
- FIG 4 there is a third space section 60 arranged into the annular gap radially between the bushing 70 and the inner wall of the body and the sleeve member 49 which borders the third space section 60.
- the third space section 60 serves for purposes of lubrication the pump 10.
- the pump 10 is provided with lubrication oil supply channel 62 and a lubrication oil discharge channel 64.
- the lubrication oil supply channel 62 is arranged to a position so as to supply oil to the second sealing gap 35.
- the lubrication oil discharge channel 64 is positioned to open in to the third space section 60.
- the pump 10 is provided with means for transferring fuel material away from the second pump chamber 16'. Therefore firstly the pump 10 is provided with a vent flow path 36.
- the vent flow path 36 runs through the body 18 of the pump and connects the second pump chamber 16' which is formed into the second space section 30" to outside of the body 18.
- the vent flow path 36 is configured to allow gas admission into the second space section 30", driven by the reciprocating movement of the piston member 28.
- the pump 10 is further provided with a discharge flow path 38 connecting the second pump chamber 16' to outside of the body 18 configured to transfer fuel material entered into the second pump chamber 16' or the second space section 30" via the sealing gap 34 away from the second space section 30" i.e. the second pump chamber 16'.
- the vent flow path 36 is provided with a one-way valve 40 which allows gas flow in the vet flow path 36 in the direction towards the second space section 30" and prevent back flow of the fluid.
- the vent flow path 36 has an inlet which opens into the surroundings of the pump 10.
- the discharge flow path 38 is provided with a one-way valve 42 configured to allow flow away from the second space section 30" via the discharge flow path 38.
- the sealing effect of the sealing gaps above may be based on qualities of the surface and/or dimension tolerances of parts and/or separate sealing elements, such as an o-ring or a lip seal.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Details Of Reciprocating Pumps (AREA)
- Fuel-Injection Apparatus (AREA)
Description
- The invention relates to a fuel pump according to the preamble of claim 1.
- Internal combustion piston engines need to be provided with one or more fuel pumps. Particularly the fuel injection in so called common rail systems into the combustion chambers of the engine requires capability of pumping the fuel into high pressure of even above 250 MPa. Since the pumps are typically lubricated by the lubrication oil of the engine the presence of both the fuel and the lubrication oil in the pump may call for special attention particularly relating to preventing or minimizing the mixing of the fuel and the lubricant in the pump.
- Document
EP 1 184 568 A2 discloses a fuel pump according to the preamble of claim 1. - Document
EP 0976926 B1 discloses an integrated pump and tappet unit for supplying fuel to an internal combustion engine, such as a large diesel engine, the unit comprising a body part enclosing a tappet member, whose axial movement is governed by movement of a cam surface provided on a cam shaft or the like, and a piston member operationally connected to the tappet member and which is arranged to pump fuel under high pressure from a fuel chamber disposed within the body part. The body part is a single member housing both said tappet member and said fuel chamber and the tappet member and the piston member are connected to each other by means of a tappet arm, which is sealed to a flange member fixed to the body part, so that fuel from the fuel chamber is prevented from coming into contact with the tappet member. - Document
DE 102015002304 A1 discloses a high pressure fuel pump. Document is silent about the possible leakage of the fuel into the lubrication oil but shows a lubrication system of the pump. The pump comprises a pump housing having an inner space, a pump plunger with a guide surface, which is guided in the interior space on the pump housing, wherein the interior space and the pump plunger limits a spring chamber of the high-pressure fuel pump, a lubricant line which opens into the interior space against the guide surface of the plunger, a vent pipe, by means of which the lubricant can be discharged from the spring chamber. - Document
DE102008042067 A1 discloses a pump which has a drive shaft provided with an eccentric cam, and a piston accommodated in a cylinder. The document discloses circular membrane seals used for separating the fuel and lubrication systems from each other. - Document
DE102006059333 A1 discloses a fuel pump comprising at least one wiper element integrated in the pump piston for removing leakage fuel collecting between the pump cylinder and the pump piston from the cylinder wall. The wiper element is a scraper ring that removes leakage fuel accumulating on the wall of the pump cylinder and guides it into at least one leakage groove. -
US7308849 defines a work chamber and driven at least indirectly by a drive shaft in a reciprocating motion, counter to the force of a restoring spring. The pump piston is braced on the drive shaft at least indirectly via a sleeve like tappet, and the restoring spring engages at least the pump piston. A support element in the tappet braces the pump piston toward the drive shaft and is braced at least indirectly on the drive shaft. The restoring spring, via a spring plate, engages the pump piston and the tappet. The spring plate is elastically deformable in the direction of motion of the pump piston in such a way that as a result of its elastic deformation, deviations in the position of its contact faces on the pump piston and on the tappet are compensated for. -
WO2011160908 A1 discloses a pump which comprises at least one pump element which has a pump piston that is at least indirectly driven in a stroke movement by a drive shaft. A plunger having a plunger body is arranged between the drive shaft and the pump piston and is movably guided in a receiving device in the direction of the stroke movement of the pump piston and is supported on the drive shaft by means of a support element. Lubricant is supplied to the receiving device via a supply line and lubricant is conducted out of the receiving device via a discharge line into the plunger body to the support element. An annular gap filter is provided between the plunger body and the receiving device and is arranged between the supply line for supplying lubricant to the receiving device and the discharge line for discharging lubricant into the plunger body. - An object of the invention is to provide a fuel pump for supplying fuel to an internal combustion piston engine in which the performance is considerably improved compared to the prior art solutions.
- The objects of the invention can be met substantially as is disclosed in the independent claim 1. Dependent claims 2-5 describe preferred embodiments of the invention.
- According to the invention a fuel pump according to claim 1 is provided.
- According to an embodiment of the invention the vent flow path is provided with a one-way valve allowing flow towards the second space section.
- According to an embodiment of the invention the discharge flow path is provided with a one-way valve allowing flow away from the second space section.
- According to an embodiment of the invention the annular gap in the second space section circumscribes the first space section at least partially such that the annular gap and the first space section are overlapping with each other in the direction of the central axis of the cylindrical space.
- According to an embodiment of the invention the cylindrical extension is a bushing removably attached to the body of the pump.
- The present invention is suitable for use as a high pressure pump in a common rail fuel system.
- The exemplary embodiments of the invention presented in this patent application are not to be interpreted as limiting. The scope of the invention is solely defined by the appended claims.
- In the following, the invention will be described with reference to the accompanying exemplary, schematic drawings, in which
-
Figure 1 illustrates a fuel pump according to an embodiment of the invention, -
Figure 2 illustrates a fuel pump according to another embodiment of the invention, -
Figure 3 illustrates a fuel pump according to an example which is not a part of the claimed invention, and -
Figure 4 illustrates a fuel pump according to still another embodiment of the invention. -
Figure 1 depicts schematically afuel pump 10 configured to supply fuel to an internal combustion piston engine. More particularly the pump is a high pressure pump configured to deliver fuel at a pressure of above 200 MPa. Thepump 10 is provided with asupply rail 12 and ahigh pressure rail 14 which are both in connection with afirst pump chamber 16 arranged to abody 18 of thepump 10. Thebody 18 comprising thepump chamber 16 may also be referred to as a barrel of thepump 10. Thesupply rail 12 is connected to thepump chamber 16 via anintake conduit 20. The high pressure rail is connected to thepump chamber 16 via anoutlet conduit 22. Theintake conduit 20 is provided with a one-way valve 24 configured to allow fuel to flow only from thesupply rail 12 to thepump chamber 16. Respectively, theoutlet conduit 22 is provided with a one-way valve 26 configure to allow fuel to flow only from thepump chamber 16 to thehigh pressure rail 14. In the embodiment shown in thefigure 1 thesupply rail 12 and thehigh pressure rail 14 are integrated into thebody 18 but it is conceivable that the rails are external to thebody 18. - The
pump 10 is also provided with apiston member 28 which is arranged into acylindrical space 30 arranged into thebody 18. Thecylindrical space 30 has acentral axis 32 and it is substantially rotationally symmetrical in respect to thecentral axis 32. Therefore thepiston member 28 is also rotationally symmetrical in respect to the central axis 32.The outer form of the body may be designed according to the needs. Thepiston member 28 is arranged into the space in re-ciprocatable manner. Thepiston member 28 has a first end 28' which borders thecylindrical space 30 at an end thereof forming thefirst pumping chamber 16. The piston has also asecond end 28" opposite to the first end 28'. Thepiston member 28 is configured to reciprocate in thespace 30 provided for thepiston member 28 and pump the fuel. This way the reciprocating piston member together with the one-way valves piston member 28 is advantageously an assembly of several parts, which is here illustrated so that the first end 28' and thesecond end 28" are separate parts removably connected to each other. - The
cylindrical space 30 comprises a first space section 30' which has a first diameter D1. In the first space section 30' the wall of the space section and the wall of thepiston member 28 are arranged against each other providing afirst sealing gap 34 between the walls, which also guides thepiston member 28 in thebody 18. Additionally the wall of the first space section guides the piston member in thebody 18 while it reciprocates in the space. Thepiston member 28 comprises a first portion which is arranged into the first space section 30' and has a diameter substantially same as the first diameter such that a desired guidance and sealing is provided. - The
cylindrical space 30 comprises also asecond space section 30" which has a second diameter D2, being greater than the first diameter D1. Thesecond space section 30" is on same central axis as the first space section 30'. Thepiston member 28 comprises a second portion which is arranged in thesecond space section 30" such that a desired guidance and sealing is provided. In thesecond space section 30" the wall of the second space section and the wall of thepiston member 28 are arranged against each other providing asecond sealing gap 35 between the walls, respectively. Additionally the wall of the second space section guides the piston member at its second portion in thebody 18 while the piston member reciprocates in the space. - There is a second pump chamber 16' arranged to a
body 18 of thepump 10. The second pump chamber 16' is arranged in connection with thesecond space section 30" such that second pump chamber 16' is configured to use empty space of thesecond space section 30" as the pump chamber. Thepiston member 28 is arranged to border both the first and thesecond pump chamber 16, 16'. - The
piston member 28 and the first and the second pump chambers are configured in the pump shown in thefigure 1 such that volumes of the first and the second pump chambers are changing same way i.e. either increasing or decreasing, during the piston member is moving to one direction. - As mentioned above, in the first space section 30' the wall of the space section and the wall of the
piston member 28 are arranged against each other providing thefirst sealing gap 34 between the walls. Thefirst sealing gap 34 separates thefirst pump chamber 16 and the second pump chamber 16' and it is of annular form. Since thefirst pump chamber 16 operates as a high pressure pump configured to deliver fuel at a pressure at above 200 MPa the fuel in the first pump chamber tends to flow into thefirst sealing gap 34 and further to flow through the sealinggap 34. Even if not shown here thefirst sealing gap 34 between thepump chambers 16, 16' may be provided with means to collect fuel material flown from thefirst pump chamber 16 into thefirst sealing gap 34. Such a means may comprise a groove arranged to the wall of the first space section provided with a conduit to lead the fuel material to further processing. Since the second pump chamber 16' is within thesecond space section 30" there may be commonly referred to in the following. - The
pump 10 is provided with means for transferring fuel material away from the second pump chamber 16'. Therefore firstly thepump 10 is provided with avent flow path 36. Thevent flow path 36 runs through thebody 18 of the pump and connects thesecond pump chamber 16 which is formed into thesecond space section 30" to outside of thebody 18. Thevent flow path 36 is configured to allow gas admission into thesecond space section 30", driven by the reciprocating movement of the piston member. Thepump 10 is further provided with adischarge flow path 38 connecting the second pump chamber 16' to outside of thebody 18 configured to transfer fuel material entered into the second pump chamber 16' or thesecond space section 30" via the sealinggap 34 away from thesecond space section 30" i.e. the second pump chamber 16'. - The
vent flow path 36 is provided with a one-way valve 40 which allows gas flow in thevent flow path 36 in the direction towards thesecond space section 30" and prevent back flow of the fluid. Thevent flow path 36 has an inlet which opens into the surroundings of thepump 10. Respectively, thedischarge flow path 38 is provided with a one-way valve 42 configured to allow flow away from thesecond space section 30" via thedischarge flow path 38. During compression stroke of the volume of the second pump chamber 16' is reduced and due to that it is pressurized. Gases and liquids within the second pump chamber 16' are forced out from the second pump chamber 16' via the discharge one-way valve 42. During suction stroke of the pump also the second pump chamber 16' expands causing suction through the vent one-way valve 40. - In the
figure 1 thepiston member 28 is at its first extreme position where thefirst pump chamber 16 has its smallest volume. Thepiston member 28 is movable by an external force, depicted by anarrow 44, which may be provided directly by the operation of the engine. - The
piston member 28 is provided with asleeve member 46 which connects to thesecond end 28" of thepiston member 28 and which has a closed end i.e. a bottom 58. The bottom 58 of thesleeve member 46 extends radially to thepiston member 28. Thesleeve member 46 may be integral to or separate part from thesecond end 28" of thepiston member 28 and/or thesleeve member 46. The bottom 58 of thesleeve member 46 is therefore common with thepiston member 28 and it serves for receiving the force needed for reciprocate thepiston member 28 in thepump 10. The sleeve member is arranged such that an annular space is provided between thesleeve member 46 and thepiston member 28, which now forms the second pump space 16'. Thesleeve member 46 opens towards the first end 28' of thepiston member 28. The sleeve member is arranged into thesecond space section 30" such that the radially inner wall of thesecond space section 30" and the radially outer wall of thesleeve member 46 are against each other providing asecond sealing gap 35. The wall of thesecond space section 30" guides thesleeve member 46 of thepiston member 28 in thebody 18 when thepiston member 28 and sleeve member are moving along thecentral axis 32. - The
body 18 of thepump 10 is provided with acylindrical extension 48 towards the second end of thepiston member 28 which extension is coaxial to the first space section 30'. Thecylindrical extension 48 has an axial length in the direction of thecentral axis 32 and an outer diameter smaller than the second diameter D2. Thecylindrical extension 48 extends axially into thesecond space section 30". This way thecylindrical extension 48 forms anannular gap 47 radially between thecylindrical extension 48 of the body and the inner wall of the body. Theannular gap 47 circumscribes the first space section at least partially such that the annular gap of thesecond space section 30" and the first space 30' section are overlapping with each other in the direction of thecentral axis 32 of the cylindrical space. Thesleeve member 46 is arranged to extend into saidannular gap 47. The end face of thecylindrical extension 48 borders the second pump chamber 16' together with thepiston member 28 and thesleeve member 46. The fitting of thesleeve member 46 extending into the annular gap between thecylindrical extension 48 and thesecond space section 30" is such that the radially inner wall of the annular gap i.e. the cylindrical outer wall of theextension 48 and the radially inner wall of thesleeve member 46 are against each other providing athird sealing gap 37. - There is
third space section 60 arranged into the annular gap radially between thecylindrical extension 48 and the inner wall of the body and the sleeve member 49 which borders the third space section. The third space section serves for purposes of lubrication thepump 10. Thepump 10 is provided with lubricationoil supply channel 62 and a lubricationoil discharge channel 64. The minimum volume of thethird space section 60 and the locations and/dimensions of the lubricationoil supply channel 62 and the lubricationoil discharge channel 64 are configured to allow a formation of a pond of lubrication oil in the third space section but preventing a total filling of the third space section with the lubrication oil. Particularly the lubricationoil supply channel 62 and the lubricationoil discharge channel 64 are dimensioned so that the flow rate of the lubrication oil out from thethird space section 60 is at least in the long run greater than the flow rate of the lubrication oil in to thethird space section 60. - The
vent flow path 36 extends through thebody 18 to the inner wall of thesecond space section 30" where itsoutlet 50 is arranged. Thevent flow path 36 continues in thesleeve member 46 and it opens into the second pump chamber 16' via anoutlet 52 of the vent flow path. The transition area between thevent flow path 36 in thebody 18 and in thesleeve member 46 is provided with anoblong space 54 extending in the direction of thecenter axis 32 into which space the vent flow path opens. This way the flow path is open at all operational positions of thepiston member 28 and thesleeve member 46. The vent flow path and the discharge flow path may be realized by providing suitable bores, grooves or otherwise provided channels into the material of thepump 10. In the embodiment of thefigure 1 theoblong space 54 is provided as an indentation, into the outer wall of thesleeve member 46, but it is conceivable to arrange that also to the inner wall of thebody 18. Thedischarge flow path 38 is provided with similaroblong space 54 for bring about a flow connection betweendischarge flow path 38 in thepiston member 28 and in thebody 18. - Now, when installed to an internal combustion engine, the
external force 44 is advantageously brought about by a power system of the engine. Therefore thepiston member 28 is in mechanical force transmission connection, typically indirectly, with the crankshaft of the engine. In practise this mean that mechanical force transmission is lubricated by the engine lubricant. Thepump 10 is provided with means for transferring fuel material away from the second pump chamber 16' any fuel material which escapes through the sealinggap 34 will not find its way into the lubrication oil of the engine. - In the
figure 2 there is shown an embodiment of the invention where the pumping effect in the second pump chamber 16' is accomplished without one-way valves by suitably locatedvent flow path 36 anddischarge flow path 38 inlets and outlets into the piston member and the body. Theoblong spaces 54 are located so that situated that thevent flow path 36 is open when the piston part is in a suction stroke which makes is possible to balance the created underpressure in the second pump chamber 16'. Thevent flow path 36 anddischarge flow path 38 inlets and outlets are so arranged that when the piston member moves towards it first end 28' the vent flow path is closed and the pressure is increasing in the second pump chamber 16'. At a certain position of thepiston member 28 thedischarge flow path 38 opens and the second pump chamber is discharged. - In the
figure 3 , which shows an example which is not a part of the claimed invention, there is shown apump unit 10 where the structure of the second pump chamber 16' is different to that shown in thefigures 1 and2 . Here thepiston member 28 extends from its first end through aguide flange 56 to a cam drive system (not shown) of thepump 10. Thepiston member 28 is provided with a bottom 58 as a radial extension part, which borders the second pump chamber 16'. In this case there is not asleeve member 46 provided in connection with the bottom 58.The radial distal end of the bottom 58 is adequately sealed against the inner wall of thesecond space section 30" such that pumping effect can be obtained by the second pump space 16'.. A feature that is common to all of thefigures 1 - 3 is that thedischarge flow path 38 opens into a part which borders the second pump chamber 16' farthest from the first end of the piston member. When the pump is at the position as is shown in thefigures 1-2 (center axis 32 is vertically positioned and the first end 28' of the piston member is upwards oriented) thedischarge flow path 38 opens into lowest position in the second pump chamber 16'. In practise thecenter axis 32 need not be exactly vertical but the pump may be tilted as long as the discharge flow path is arranged to substantially lowest position into the second pump chamber 16'. - In the
figure 4 there is shown an embodiment of the invention where thepump 10 is configured to be installed such that the first end 28' of thepiston member 28 is horizontally below thesecond end 28" of thepiston member 28. The basic configuration of thepump 10 is similar to that shown in thefigure 1 being though such features, which are effected by the departing orientation, designed differently. In thefigure 4 there is shown that thefirst sealing gap 34 is provided with afuel scraper ring 68 in an annular space arranged to minimize the flow of fuel into thesecond space section 30". There is also another annular space 67 closer to thefirst pump chamber 16 from which a fuel discharge channel 66 is extending to outside thebody 18. Even if not shown, similarfuel scraper ring 68 and fuel discharge channel 66 may be arranged to the pumps shown in thefigures 1 to 3 . This arrangement decreases the amount of fuel flow through thefirst sealing gap 34 to the second pump space 16', but the fuel directed to the fuel discharge channel 66 is still at considerably high pressure. - In the
pump 10 shown in thefigure 4 thesecond space section 30" is provided with abushing 70. The bushing is generally cylindrical part having an outwardly extending shoulder at its first end. It is at its first end attached to the inner surface of thesecond space section 30" and it is provided with a section having a smaller diameter than thesecond space section 30" such that anannular space 60 is provided between thebushing 70 and the inner surface of thesection space section 30". Thebushing 70 is attached at its first end, on the side of the first end 28' of thepiston member 28, to thebody 18. Thepiston member 28 comprises asleeve member 46 which is arranged in thesecond space section 30" such that a desired guidance and sealing is provided corresponding to thefigures 1 and2 . In thesecond space section 30" the inner wall of thesecond space section 30" and the wall of thesleeve member 46 are arranged against each other providing asecond sealing gap 35 between the walls, respectively. Thesleeve member 46 is arranged to extend into saidannular gap 60 formed by thebushing 70 and the wall of thesecond space section 30". This way thebushing 70 borders the second pump chamber 16' together withsleeve member 46 and thepiston member 28. The fitting of thesleeve member 46 to extend into the annular gap between thebushing 70 and wall of thesecond space section 30" is such that the radially inner wall of the annular gap i.e. the radially outer wall of thebushing 70 and the radially inner wall of thesleeve member 46 are against each other providing athird sealing gap 37. - In the
figure 4 there is athird space section 60 arranged into the annular gap radially between thebushing 70 and the inner wall of the body and the sleeve member 49 which borders thethird space section 60. Thethird space section 60 serves for purposes of lubrication thepump 10. Thepump 10 is provided with lubricationoil supply channel 62 and a lubricationoil discharge channel 64. The lubricationoil supply channel 62 is arranged to a position so as to supply oil to thesecond sealing gap 35. The lubricationoil discharge channel 64 is positioned to open in to thethird space section 60. - The
pump 10 is provided with means for transferring fuel material away from the second pump chamber 16'. Therefore firstly thepump 10 is provided with avent flow path 36. Thevent flow path 36 runs through thebody 18 of the pump and connects the second pump chamber 16' which is formed into thesecond space section 30" to outside of thebody 18. Thevent flow path 36 is configured to allow gas admission into thesecond space section 30", driven by the reciprocating movement of thepiston member 28. Thepump 10 is further provided with adischarge flow path 38 connecting the second pump chamber 16' to outside of thebody 18 configured to transfer fuel material entered into the second pump chamber 16' or thesecond space section 30" via the sealinggap 34 away from thesecond space section 30" i.e. the second pump chamber 16'. - The
vent flow path 36 is provided with a one-way valve 40 which allows gas flow in thevet flow path 36 in the direction towards thesecond space section 30" and prevent back flow of the fluid. Thevent flow path 36 has an inlet which opens into the surroundings of thepump 10. Respectively, thedischarge flow path 38 is provided with a one-way valve 42 configured to allow flow away from thesecond space section 30" via thedischarge flow path 38. During compression stroke of the volume of the second pump chamber 16' is reduced and due to that it is pressurized. Gases and liquids within the second pump chamber 16' are forced out from the second pump chamber 16' via the discharge one-way valve 42. During suction stroke of the pump also the second pump chamber 16' expands causing suction through the vent one-way valve 40. - The sealing effect of the sealing gaps above may be based on qualities of the surface and/or dimension tolerances of parts and/or separate sealing elements, such as an o-ring or a lip seal.
- While the invention has been described herein by way of examples in connection with what are, at present, considered to be the most preferred embodiments, it is to be understood that the invention is not limited to the disclosed embodiments, but is intended to cover various modifications as long as these are included within the scope of the invention, as defined in the appended claims.
Claims (5)
- A fuel pump (10) for supplying fuel to an internal combustion piston engine, comprising:a body (18) and a cylindrical space (30) arranged in the body having a central axis (32),a piston member (28) arranged to reciprocate in the cylindrical space (30),where the cylindrical space (30) comprises a first space section (30') having a first diameter (D1) in which the wall of the space and the wall of the piston member (28) are arranged against each other providing a first sealing gap (34) such that the wall of the space (30) guides the piston member (28) in the body (18), andwhere the first space section (30') is bordered by a first end (28') of the piston member (28) forming a first pumping chamber (16) of the fuel pump (10) configured to pump the fuel as the piston member (28) reciprocates in the space, and where the cylindrical space (30) further comprises a second space section (30") on the central axis (32) having a second diameter (D2) greater than the first diameter (D1),and where the piston member is provided with a sleeve member (46) extending towards the first end (28') of the piston member (28) such that an annular space is provided between the sleeve member (46) and the piston member (28), which annular space opens towards the first end (28') of the piston member (28), and where an inner wall of the second space section (30") and a radially outer wall of the sleeve member (46) are arranged against each other providing a second sealing gap (35) such that the inner wall of the second space section (30') guides the sleeve member (46) in the second space section (30"), andwherein the pump body (18) is provided with a cylindrical extension (48) which is coaxial to the first space section (30') forming an annular gap circumscribing the piston member (28), wherein the sleeve member (48) is arranged to extend into the annular gap between the cylindrical extension (48) and inner wall of the second space section (30"), wherein an annular third space section (60) is arranged into fuel pump (10) which third space section (60) is partially bordered by the inner wall of the second space section (30"), the outer wall of the cylindrical extension (48) and the sleeve member (46) which is arranged to extend into the annular third space section (60), characterised inthat the second space section (30") is provided with a second pumping chamber (16') of the pump configured to pump fuel from the second space section (30"), as the piston member (28) reciprocates in the space (30), and the pump (10) is provided with a vent flow path (36) connecting the second space section (30") to outside of the body for allowing gas admission into the second space section (30"), driven by the reciprocating movement of the piston member, and a discharge flow path (38) connecting the second space section (30") to outside of the body for transferring fuel material away from the second space section (30"),and in that a lubrication oil supply channel (62) and a lubrication oil discharge channel (64) are connected to the third space section (60).
- A fuel pump according to claim 1, characterized in that the vent flow path (36) is provided with a one-way valve (40) allowing flow towards the second space section (30").
- A fuel pump according to claim 1 characterized in that the discharge flow path is provided with a one-way valve (42) allowing flow away from the second space section (30").
- A fuel pump according to claim 1, characterized in that the annular gap in the second space section (30") circumscribes the first space section at least partially such that the annular gap and the first space section (30') are overlapping with each other in the direction of the central axis (32) of the cylindrical space.
- A fuel pump (10) according to claim 1, characterized in that the cylindrical extension (48) is a bushing (70) removably attached to the body (18) of the pump (10).
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/FI2017/050218 WO2018178502A1 (en) | 2017-03-29 | 2017-03-29 | A fuel pump for supplying fuel to an internal combustion piston engine |
Publications (2)
Publication Number | Publication Date |
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EP3601778A1 EP3601778A1 (en) | 2020-02-05 |
EP3601778B1 true EP3601778B1 (en) | 2024-10-09 |
Family
ID=58544982
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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EP17717208.7A Active EP3601778B1 (en) | 2017-03-29 | 2017-03-29 | A fuel pump for supplying fuel to an internal combustion piston engine |
Country Status (4)
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EP (1) | EP3601778B1 (en) |
KR (1) | KR102216495B1 (en) |
CN (1) | CN110709598B (en) |
WO (1) | WO2018178502A1 (en) |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1184568A2 (en) * | 2000-08-31 | 2002-03-06 | Delphi Technologies, Inc. | Fuel pump |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4030951B4 (en) * | 1990-09-29 | 2004-03-18 | Robert Bosch Gmbh | Heavy oil fuel injector for injection internal combustion engines |
DE19507295B4 (en) * | 1995-03-02 | 2004-09-02 | Siemens Ag | Radial piston pump, in particular fuel pump for an internal combustion engine |
FI108071B (en) | 1998-07-03 | 2001-11-15 | Waertsilae Tech Oy Ab | Integrated pump and lift unit in the fuel supply system |
JP2003206824A (en) * | 2001-11-09 | 2003-07-25 | Bosch Automotive Systems Corp | Injection pump, dme fuel supply device of diesel engine having it |
JP3788373B2 (en) * | 2002-03-11 | 2006-06-21 | 日産自動車株式会社 | High pressure fuel pump refueling device |
DE10355027A1 (en) | 2003-11-25 | 2005-06-23 | Robert Bosch Gmbh | High-pressure pump, in particular for a fuel injection device of an internal combustion engine |
JP4386030B2 (en) * | 2005-12-02 | 2009-12-16 | トヨタ自動車株式会社 | High pressure pump |
JP2007177704A (en) * | 2005-12-28 | 2007-07-12 | Toyota Motor Corp | High pressure pump |
DE102006059333B4 (en) | 2006-12-15 | 2018-07-12 | Man Diesel & Turbo Se | Fuel pump |
JP5642925B2 (en) * | 2008-08-20 | 2014-12-17 | 日産自動車株式会社 | High pressure fuel pump |
DE102008042067A1 (en) | 2008-09-12 | 2010-03-18 | Robert Bosch Gmbh | High-pressure pump for supplying pressurized fuel into combustion chamber of internal-combustion engine, has circular chambers sealed by circular membranes with respect to chambers contaminated by fuel and lubricant |
DE102009037407A1 (en) * | 2009-08-13 | 2011-04-21 | Continental Automotive Gmbh | High-pressure pump for conveying fuel into injector of injection system utilized for injecting fuel into diesel internal-combustion engine of motor vehicle, has flow control valve arranged in flushing pipe that flushes recess and bearing |
DE102010030498A1 (en) | 2010-06-24 | 2011-12-29 | Robert Bosch Gmbh | Pump, in particular high-pressure fuel pump |
EP2530315A1 (en) * | 2011-06-02 | 2012-12-05 | Delphi Technologies Holding S.à.r.l. | Fuel pump lubrication |
DE102011089399A1 (en) * | 2011-12-21 | 2013-06-27 | Robert Bosch Gmbh | Pump, in particular high-pressure fuel pump for a fuel injection device |
DE102012204264A1 (en) * | 2012-03-19 | 2013-09-19 | Robert Bosch Gmbh | high pressure pump |
DE102015002304A1 (en) | 2015-02-24 | 2016-03-31 | Mtu Friedrichshafen Gmbh | High-pressure fuel pump |
-
2017
- 2017-03-29 CN CN201780091343.5A patent/CN110709598B/en active Active
- 2017-03-29 EP EP17717208.7A patent/EP3601778B1/en active Active
- 2017-03-29 KR KR1020197031752A patent/KR102216495B1/en active IP Right Grant
- 2017-03-29 WO PCT/FI2017/050218 patent/WO2018178502A1/en unknown
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1184568A2 (en) * | 2000-08-31 | 2002-03-06 | Delphi Technologies, Inc. | Fuel pump |
Also Published As
Publication number | Publication date |
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KR20190124811A (en) | 2019-11-05 |
CN110709598B (en) | 2021-08-06 |
CN110709598A (en) | 2020-01-17 |
KR102216495B1 (en) | 2021-02-16 |
WO2018178502A1 (en) | 2018-10-04 |
EP3601778A1 (en) | 2020-02-05 |
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