EP3094853B1 - Bobbin with venting conduit - Google Patents
Bobbin with venting conduit Download PDFInfo
- Publication number
- EP3094853B1 EP3094853B1 EP14806214.4A EP14806214A EP3094853B1 EP 3094853 B1 EP3094853 B1 EP 3094853B1 EP 14806214 A EP14806214 A EP 14806214A EP 3094853 B1 EP3094853 B1 EP 3094853B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- bobbin assembly
- venting conduit
- bobbin
- over
- process manufacturing
- 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
- 238000013022 venting Methods 0.000 title claims description 29
- 238000000034 method Methods 0.000 claims description 18
- 238000000465 moulding Methods 0.000 claims description 14
- 238000004519 manufacturing process Methods 0.000 claims description 11
- 238000004804 winding Methods 0.000 claims description 6
- 238000005553 drilling Methods 0.000 claims description 5
- 238000009434 installation Methods 0.000 claims description 3
- 238000003466 welding Methods 0.000 claims description 3
- 239000000446 fuel Substances 0.000 description 27
- 239000012530 fluid Substances 0.000 description 7
- 238000002347 injection Methods 0.000 description 5
- 239000007924 injection Substances 0.000 description 5
- 238000002485 combustion reaction Methods 0.000 description 3
- 238000003754 machining Methods 0.000 description 2
- 238000006073 displacement reaction Methods 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
- F02M47/00—Fuel-injection apparatus operated cyclically with fuel-injection valves actuated by fluid pressure
- F02M47/02—Fuel-injection apparatus operated cyclically with fuel-injection valves actuated by fluid pressure of accumulator-injector type, i.e. having fuel pressure of accumulator tending to open, and fuel pressure in other chamber tending to close, injection valves and having means for periodically releasing that closing pressure
- F02M47/027—Electrically actuated valves draining the chamber to release the closing pressure
-
- 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
- F02M55/002—Arrangement of leakage or drain conduits in or from injectors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- 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
- F02M63/0012—Valves
- F02M63/0014—Valves characterised by the valve actuating means
- F02M63/0015—Valves characterised by the valve actuating means electrical, e.g. using solenoid
- F02M63/0017—Valves characterised by the valve actuating means electrical, e.g. using solenoid using electromagnetic operating 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
- F02M2200/00—Details of fuel-injection apparatus, not otherwise provided for
- F02M2200/50—Arrangements of springs for valves used in fuel injectors or fuel injection pumps
Definitions
- the present invention relates to a method for process manufacturing of a bobbin assembly and has particular but not exclusive application to fuel injectors for use in delivering fuel under pressure to a combustion space of an internal combustion engine.
- a known fuel injector for use in such a fuel system is illustrated in fig 1 and includes a nozzle needle 10 slidable within a bore.
- the needle 10 is slipping within a bore formed in a nozzle body 17 and engageable with a seating to control fuel delivery through one or more outlet openings. Movement of the nozzle needle 10 occurs rapidly, in use, the periods during which fuel injection occurs being of short duration.
- a similar fuel injector is disclosed in EP2320066A1 .
- the movement of the needle is controlled using two chambers, a high pressure control chamber 12 and a low pressure chamber 16, which communicates with low pressure drain reservoir 22.
- an actuator 30 is energized (opening phase), which urges an armature 29 and a valve member 25 in contact therewith, identified as a control valve 15, located in the chamber to move upwards against the action of a bobbin spring 33 of the actuator 30.
- the length of the spring 33 is reduced and then the pressure within the bobbin spring area 43 increases, thus there is a movement of the fluid in the spring area 43 which perturbs the displacement of the armature 29 secured to the valve member 25 .
- a bobbin assembly of an electromagnetic actuator is adapted to be in a fuel injector.
- the bobbin assembly comprises a core extending along a main axis, a wire coil arranged around the core.
- the coil is over-moulded so that it has a cylindrical external surface extending axially from a first surface to a second surface and an axial blind bore extending axially and inwardly inside the bobbin assembly from the first surface to the distal end.
- the blind bore is adapted to accommodate a spring for biasing a magnetic armature.
- the bobbin assembly is provided with a venting conduit extending through the over-moulding from the blind axial bore to the external cylindrical surface.
- venting conduit is arranged proximal to the distal end. Moreover the venting conduit is proximal to the first face of the bobbin and comprises at least one groove in the first radial surface. Besides the venting conduit makes an angle with the main axis between 80 degrees and 120 degrees. Additionally the angle can be preferably 90 degrees.
- the actuator of the fuel injector comprises the bobbin assembly and the fuel injector comprises the actuator .
- a method for process manufacturing of the bobbin assembly comprises the following steps:
- a known fuel injector for use in such a fuel system in illustrated in fig 1 and includes a valve needle 10 slidable within a bore 11.
- the bore 11 takes the form of a blind bore formed in a nozzle body 17; the bore 11 is supplied with fuel under high pressure.
- the needle 10 includes a surface exposed to the fuel pressure within a control chamber 12.
- the control chamber 12 is supplied with fuel under high pressure from a supply passage 13 dimensioned such that fuel is only permitted to flow to the control chamber 12 at a restricted rate.
- a spring 20 is located within the control chamber 12, the spring acting to apply a biasing force to the needle 10 urging the needle 10 into engagement with the seating.
- a high pressure control chamber 12 which communicates with low pressure drain reservoir 22.
- an actuator 30, which comprises a bobbin assembly 44 and a control valve 15, is energized (opening phase), which urges an armature 29 and a valve member 25 in contact therewith, identified as a control valve 15, located in the chamber 16 to move upwards against the action of a bobbin spring 33 of the actuator 30, lifting the valve member 25 away for its seating.
- EMBODIEMENT FIGURES 2, 3, 4, 5, 6 and 7.
- control chamber 12 is supplied with fuel from an INO orifice 52, conduit which supplied fuel from the common rail (not shown), through a hemispheric part 50, dimensioned such that fuel is only permitted to flow to the control chamber 12 at a restricted rate.
- the spring 20 is within the control chamber 12, the spring 20 acting to apply a biasing force to the needle 10, urging the needle 10 into engagement with its seating.
- fuel is able to escape from the control chamber 12 to the chamber 16 ( fig 3 ) which is at a low pressure, through an hemispheric part 51 and then through a spill canal SPO 54 ( figure 3 ), and then the fuel escape from the chamber 16 to a return passage 27 ( figure 3 ).
- control chamber 12 there are 2 orifices; one is the INO orifice 52 ( fig 2 ) which fills in the chamber 12 with fuel and the SPO orifice 54 ( fig 3 ) which empty the chamber of its fluid. Then the ratio INO/SPO is calculated in order to empty quicker than to fill-in.
- the actuator spring 33 When the actuator 30 is energized, the actuator spring 33 is compressed by the pressure urged by the armature 29, thus the pressure in an axial blind bore 43 increases.
- the length of the spring 33 is reduced so the volume of the axial bore 43 is reduced so the pressure increases.
- the overpressure within the axial bore 43 is suppressed by a venting conduit 42 which is fluidically connected to the axial bore 43 by one end and by the other end to a low pressure area 41, which communicates to a return circuit 40.
- the venting conduit 42 is within an over-moulded coil 96, from the axial bore (43), which is the area of the spring 33, to the external cylindrical surface (108)
- venting conduit 42 is at the proximal portion of upper part of the axial bore 43. Moreover the venting conduit 42 make an angle of 90 degree to the main axis of the injector 5 and the shape of the venting conduit 42 is round or square or conical.
- the venting conduit 42 is made by machining, drilling or with the use of an insert during the over moulding 96 of the bobbin assembly 44. In a further embodiment, the venting conduit 42, makes an angle, for instance between 80 degrees and 120 degrees from the main axis (vertical) of the injector 5 and the shape of the venting conduit 42 is round or square or conical.
- the venting hole is made by machining, drilling or with the use of an insert during the over-moulding 96 of the bobbin assembly 44.
- the manufacturing process is now described.
- the bobbin assembly 44 includes the sub assembly 90 which includes a coil 92, two terminals 94, an over moulding 96 and a jacket 98.
- the bobbin assembly 44 starts with the following steps:
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Fluid Mechanics (AREA)
- Fuel-Injection Apparatus (AREA)
Description
- The present invention relates to a method for process manufacturing of a bobbin assembly and has particular but not exclusive application to fuel injectors for use in delivering fuel under pressure to a combustion space of an internal combustion engine.
- A known fuel injector for use in such a fuel system is illustrated in
fig 1 and includes anozzle needle 10 slidable within a bore. Theneedle 10 is slipping within a bore formed in anozzle body 17 and engageable with a seating to control fuel delivery through one or more outlet openings. Movement of thenozzle needle 10 occurs rapidly, in use, the periods during which fuel injection occurs being of short duration. A similar fuel injector is disclosed inEP2320066A1 . - The movement of the needle is controlled using two chambers, a high
pressure control chamber 12 and alow pressure chamber 16, which communicates with lowpressure drain reservoir 22. When injection starts, anactuator 30 is energized (opening phase), which urges anarmature 29 and avalve member 25 in contact therewith, identified as acontrol valve 15, located in the chamber to move upwards against the action of abobbin spring 33 of theactuator 30. At this stage, the length of thespring 33 is reduced and then the pressure within thebobbin spring area 43 increases, thus there is a movement of the fluid in thespring area 43 which perturbs the displacement of thearmature 29 secured to thevalve member 25 . This problem will be solved by the present invention, which will further be described. - A bobbin assembly of an electromagnetic actuator is adapted to be in a fuel injector. The bobbin assembly comprises a core extending along a main axis, a wire coil arranged around the core. The coil is over-moulded so that it has a cylindrical external surface extending axially from a first surface to a second surface and an axial blind bore extending axially and inwardly inside the bobbin assembly from the first surface to the distal end. Moreover the blind bore is adapted to accommodate a spring for biasing a magnetic armature. Furthermore the bobbin assembly is provided with a venting conduit extending through the over-moulding from the blind axial bore to the external cylindrical surface.
- In addition the venting conduit is arranged proximal to the distal end. Moreover the venting conduit is proximal to the first face of the bobbin and comprises at least one groove in the first radial surface. Besides the venting conduit makes an angle with the main axis between 80 degrees and 120 degrees. Additionally the angle can be preferably 90 degrees. In addition the actuator of the fuel injector comprises the bobbin assembly and the fuel injector comprises the actuator . A method for process manufacturing of the bobbin assembly comprises the following steps:
- winding of the wire on the sub assembly, wrapping of the wire on one end of the terminals, an installation of the covers on the wrapping , welding of the covers , fit of a jacket on the area of the wire winding, then over-moulding and grinding of the bobbin assembly and providing the venting conduit in the over-moulding of the bobbin assembly. Moreover the venting conduit is made by drilling the venting conduit in the over-moulding.
-
-
Fig 1 is a sectional view of the overall assembly of a known injector -
Fig 2 and Fig 3 are the sectional views of a fuel injector with the venting conduit in different phases (opening). -
Figure 4 is a sectional view of the bobbin assembly area and the venting conduit. -
Fig 5 is a sectional view of a inclined venting conduit -
Fig 6 and Fig 7 are the sectional views of the manufacturing the bobbin assembly. - In the following description, similar parts will be described by the same references. To be concise and for clarity of the description, the upper and lower orientation will be used as the orientation of the figures with no limitation for the scope of the protection, in particular in regard to the different embodiments. Words like "upper, lower, top bottom... "will be used without limitative intent.
- According to a known fuel injector for use in such a fuel system in illustrated in
fig 1 and includes avalve needle 10 slidable within abore 11. Thebore 11 takes the form of a blind bore formed in anozzle body 17; thebore 11 is supplied with fuel under high pressure. Theneedle 10 includes a surface exposed to the fuel pressure within acontrol chamber 12. Thecontrol chamber 12 is supplied with fuel under high pressure from asupply passage 13 dimensioned such that fuel is only permitted to flow to thecontrol chamber 12 at a restricted rate. - A
spring 20 is located within thecontrol chamber 12, the spring acting to apply a biasing force to theneedle 10 urging theneedle 10 into engagement with the seating. - The movement of the needle is controlled using two chambers, a high
pressure control chamber 12 and alow pressure chamber 16, which communicates with lowpressure drain reservoir 22. When injection starts, anactuator 30, which comprises abobbin assembly 44 and acontrol valve 15, is energized (opening phase), which urges anarmature 29 and avalve member 25 in contact therewith, identified as acontrol valve 15, located in thechamber 16 to move upwards against the action of abobbin spring 33 of theactuator 30, lifting thevalve member 25 away for its seating. As a result, fuel is able to escape from thecontrol chamber 12 to thechamber 16 which is at a low pressure, due to its connection with the low pressure reservoir by a return passage 27 (not shown in figures) .As a result, the fuel pressure in thecontrol chamber 12 falls, and as a result, the force applied to theneedle 10 urging theneedle 10 to is seating also falls. A point will be reached beyond which the fuel pressure acting upon athrust surface 10a is sufficient to lift theneedle 10 away from its seating, and permitting fuel from thebore 11 to flow past the seating to the outlet openings and into the combustion space with which the injector is associated. - As illustrated in
figure 2 , when theelectromagnetic control valve 15 is not energized, thevalve member 25 engages itsseating 46, and then thebore 11 and thecontrol chamber 12 will contain fluid under high pressure. The action of the high pressure in thecontrol chamber 12 and the action of thespring 20 is sufficient to ensure that theneedle 10 remains in engagement in its seating and theinjector 5 is closed with no injection of fluid. - As illustrated in
figure 2 , thecontrol chamber 12 is supplied with fuel from an INOorifice 52, conduit which supplied fuel from the common rail (not shown), through ahemispheric part 50, dimensioned such that fuel is only permitted to flow to thecontrol chamber 12 at a restricted rate. Thespring 20 is within thecontrol chamber 12, thespring 20 acting to apply a biasing force to theneedle 10, urging theneedle 10 into engagement with its seating. - As illustrated in
figure 3 , when the injection is to start, anactuator 30, which includes thecontrol valve 15 and abobbin assembly 44 which includes asub assembly 90, is energized, urging thearmature 29 andvalve member 25 to move upwards against the action of thespring 33, lifting thevalve member 25 away for its seating. As a result, fuel is able to escape from thecontrol chamber 12 to the chamber 16 (fig 3 ) which is at a low pressure, through anhemispheric part 51 and then through a spill canal SPO 54 (figure 3 ), and then the fuel escape from thechamber 16 to a return passage 27 (figure 3 ). - In the
control chamber 12, there are 2 orifices; one is the INO orifice 52 (fig 2 ) which fills in thechamber 12 with fuel and the SPO orifice 54 (fig 3 ) which empty the chamber of its fluid. Then the ratio INO/SPO is calculated in order to empty quicker than to fill-in. - A first embodiment is now described in reference to
figure 4 . - When the
actuator 30 is energized, theactuator spring 33 is compressed by the pressure urged by thearmature 29, thus the pressure in an axialblind bore 43 increases. During the opening phase of thecontrol valve 15, the length of thespring 33 is reduced so the volume of theaxial bore 43 is reduced so the pressure increases. Thearmature 29, moving upwards, urges the fluid in theaxial bore 43, which is a blind bore and the fluid wave moves back downwards to thearmature 29 and the fluid wave perturbs thecontrol valve 15. The overpressure within theaxial bore 43 is suppressed by aventing conduit 42 which is fluidically connected to theaxial bore 43 by one end and by the other end to alow pressure area 41, which communicates to areturn circuit 40. Theventing conduit 42 is within an over-mouldedcoil 96, from the axial bore (43), which is the area of thespring 33, to the external cylindrical surface (108) - Furthermore the
venting conduit 42 is at the proximal portion of upper part of theaxial bore 43. Moreover theventing conduit 42 make an angle of 90 degree to the main axis of theinjector 5 and the shape of theventing conduit 42 is round or square or conical. Theventing conduit 42 is made by machining, drilling or with the use of an insert during the over moulding 96 of thebobbin assembly 44. In a further embodiment, theventing conduit 42, makes an angle, for instance between 80 degrees and 120 degrees from the main axis (vertical) of theinjector 5 and the shape of theventing conduit 42 is round or square or conical. The venting hole is made by machining, drilling or with the use of an insert during the over-moulding 96 of thebobbin assembly 44. - In another aspect of the invention, the manufacturing process is now described. As shown in the
figure 6 and 7 , thebobbin assembly 44 includes thesub assembly 90 which includes acoil 92, twoterminals 94, an overmoulding 96 and ajacket 98. Thebobbin assembly 44 starts with the following steps: - winding of the
wire 92 on thesub assembly 90 and then; - wrapping of the
wire 92 ends on the low end of theterminals 94 and then; - installation of the
covers 95 down on the lower ends of theterminals 94 and then; - welding of the
cover 95 on the lower ends of theterminals 94 then; - fit of a
jacket 98 on the area of the wire winding (92) and then; - over-moulding and grinding of the bobbin assembly (44) ;
- Providing the venting conduit (42) by the use of insert in the over moulding phase of the bobbin assembly (44) or by drilling after the over-moulding of the bobbin assembly.
- Insert of the
washer 100 and the joint 102 in the terminal end side of the bobbin assembly (44);
Claims (6)
- Method for process manufacturing of a bobbin assembly (44) comprising a core (93) extending along a main axis,
a coil (92) arranged around the core (93), the coil being over-moulded so that it has a cylindrical external surface (108) extending axially from a first surface (104) to a second surface and an axial blind bore (43) extending axially and inwardly inside the bobbin assembly (44) from the first surface (104) to a distal end (106), the blind bore (43) adapted to accommodate a spring (33) for biasing a magnetic armature; the bobbin assembly (44) further provided with a venting conduit (42) extending through the over-moulding (96) from the blind axial bore (43) to the external cylindrical surface (108), the method for process manufacturing of a bobbin assembly (44) comprising the following steps:- winding of a coil (92) on a sub assembly (90) comprising terminals (94),- wrapping of the coil (92) on one end of the terminals (94) and then;- installation of a cover (95) on the wrapping and welding of the cover (95) then;- fit of a jacket (98) on the area of a wire winding and then;- over-moulding and grinding of the bobbin assembly (44) and then;- providing a venting conduit (42) in the over-moulding (96) of the bobbin assembly (44); the venting conduit (42) made by drilling the venting conduit (42) in the over-moulding (96), and wherein the venting conduit (42) makes an angle with the main axis between 80 degrees and 120 degrees. - Method for process manufacturing of a bobbin assembly (44) as set in claim 1, wherein the venting conduit (42) is arranged proximal to the distal end (106)
- Method for process manufacturing of a bobbin assembly (44) as set in claim 1, wherein the venting conduit (42) is proximal to the first face (104) of the bobbin (44).
- Method for process manufacturing of a bobbin assembly (44) as set in claim 1, wherein the venting conduit 42 makes an angle of 90 degree to the main axis .
- Method for process manufacturing of a bobbin assembly (44) as set in any one of claims 1 to 4, wherein an actuator (30) comprises the bobbin assembly (44).
- Method for process manufacturing of a bobbin assembly (44) as set in claim 5, wherein an injector (5) comprises the actuator (30).
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GBGB1400650.6A GB201400650D0 (en) | 2014-01-15 | 2014-01-15 | Bobbin with venting conduit |
PCT/EP2014/075492 WO2015106866A1 (en) | 2014-01-15 | 2014-11-25 | Bobbin with venting conduit |
Publications (2)
Publication Number | Publication Date |
---|---|
EP3094853A1 EP3094853A1 (en) | 2016-11-23 |
EP3094853B1 true EP3094853B1 (en) | 2020-09-02 |
Family
ID=50238982
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP14806214.4A Active EP3094853B1 (en) | 2014-01-15 | 2014-11-25 | Bobbin with venting conduit |
Country Status (5)
Country | Link |
---|---|
EP (1) | EP3094853B1 (en) |
KR (1) | KR102204703B1 (en) |
CN (1) | CN106133305B (en) |
GB (1) | GB201400650D0 (en) |
WO (1) | WO2015106866A1 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB201513309D0 (en) | 2015-07-29 | 2015-09-09 | Delphi Int Operations Lux Srl | Fuel injector |
FR3055370B1 (en) * | 2016-09-01 | 2020-05-01 | Delphi Technologies Ip Limited | COIL ASSEMBLY |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2336628A (en) * | 1998-04-24 | 1999-10-27 | Lucas Ind Plc | A fuel injector, for an I.C. engine, having a three way two position needle control valve |
DE10031582A1 (en) * | 2000-06-29 | 2002-01-17 | Bosch Gmbh Robert | Pressure controlled injector with controlled nozzle needle |
JP3790711B2 (en) * | 2002-03-15 | 2006-06-28 | ボッシュ株式会社 | Fuel injector |
JP2007040242A (en) * | 2005-08-04 | 2007-02-15 | Denso Corp | Solenoid valve and fuel injection device using the same, and solenoid valve manufacturing method |
DE102006049050A1 (en) * | 2006-10-18 | 2008-04-30 | Robert Bosch Gmbh | Injector for injecting fuel |
DE102007011789A1 (en) * | 2007-03-12 | 2008-09-18 | Robert Bosch Gmbh | fuel injector |
US20100096473A1 (en) * | 2008-10-20 | 2010-04-22 | Caterpillar Inc. | Variable flow rate valve for mechnically actuated fuel injector |
EP2320066A1 (en) * | 2009-11-06 | 2011-05-11 | Delphi Technologies Holding S.à.r.l. | Electromagnetic actuator |
EP2444650B1 (en) * | 2010-10-20 | 2015-12-23 | Delphi International Operations Luxembourg S.à r.l. | Improved fuel injector |
DE102012110240A1 (en) * | 2012-10-26 | 2014-04-30 | L'orange Gmbh | Fuel injection injector for internal combustion engines |
-
2014
- 2014-01-15 GB GBGB1400650.6A patent/GB201400650D0/en not_active Ceased
- 2014-11-25 CN CN201480077185.4A patent/CN106133305B/en active Active
- 2014-11-25 WO PCT/EP2014/075492 patent/WO2015106866A1/en active Application Filing
- 2014-11-25 KR KR1020167021886A patent/KR102204703B1/en active IP Right Grant
- 2014-11-25 EP EP14806214.4A patent/EP3094853B1/en active Active
Non-Patent Citations (1)
Title |
---|
None * |
Also Published As
Publication number | Publication date |
---|---|
CN106133305A (en) | 2016-11-16 |
GB201400650D0 (en) | 2014-03-05 |
EP3094853A1 (en) | 2016-11-23 |
KR102204703B1 (en) | 2021-01-20 |
KR20160107287A (en) | 2016-09-13 |
WO2015106866A1 (en) | 2015-07-23 |
CN106133305B (en) | 2018-11-20 |
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