EP2197606A2 - Method for producing hollow forged parts and parts thus obtained - Google Patents
Method for producing hollow forged parts and parts thus obtainedInfo
- Publication number
- EP2197606A2 EP2197606A2 EP08840711A EP08840711A EP2197606A2 EP 2197606 A2 EP2197606 A2 EP 2197606A2 EP 08840711 A EP08840711 A EP 08840711A EP 08840711 A EP08840711 A EP 08840711A EP 2197606 A2 EP2197606 A2 EP 2197606A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- core
- blank
- forging
- process according
- positioning
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21K—MAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES, RIVETS, BOLTS OR WHEELS
- B21K21/00—Making hollow articles not covered by a single preceding sub-group
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J5/00—Methods for forging, hammering, or pressing; Special equipment or accessories therefor
- B21J5/002—Hybrid process, e.g. forging following casting
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J5/00—Methods for forging, hammering, or pressing; Special equipment or accessories therefor
- B21J5/02—Die forging; Trimming by making use of special dies ; Punching during forging
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/10—Cores; Manufacture or installation of cores
- B22C9/106—Vented or reinforced cores
Definitions
- the present invention relates to the technical field of the manufacture of metal parts subjected to a forging operation.
- the object of the invention finds particularly advantageous applications for producing metal parts such as aluminum alloy in order to making parts for the field for example of the cycle or the automobile such as connecting rods, wishbones, pivots, transmission parts, motor supports or any other ground connection parts.
- it is known to produce a part by forging techniques. This method consists of making a metal blank and placing it after having possibly heated it between two engravings of a matrix. These two engravings are actuated by a press against each other to exert on the blank a work of deformation while ensuring a good surface condition.
- Such a method makes it possible to obtain parts with a good mechanical resistance (static and dynamic) and a respect of the geometrical tolerances.
- EP 0 850 825 proposes to make a core of lost material to form the hollow part of a bicycle pedal crank.
- This core is extended by a support portion for positioning the support within a casting mold in which a metal is cast. Before a subsequent forging operation, the support portion of the core and the portion of the core defining the receiving bore are removed. Even if such a technique reduces the amount of material used, this technique is unsatisfactory in practice because it does not ensure the good stability of the core during the forging operation. In addition, this technique requires the removal of a portion of the core prior to the forging operation. In addition to the disadvantages of this operation, It can not be ruled out that core debris can be found on forging tools, which can cause surface defects on the part.
- the present invention therefore aims to overcome the disadvantages mentioned above by providing a method to benefit from the advantages of the forging process of a part while allowing to obtain a piece of optimized weight at a reduced cost.
- Another object of the invention is to provide a method for producing a hollow forged part whose dimensional characteristics are perfectly controlled. Another object of the invention is to provide a method for simply and inexpensively producing a hollow forging without surface defects likely to appear during the forging operation.
- the method according to the invention aims at producing a hollow forged part.
- the object of the invention is therefore to provide a method of manufacturing hollow forgings comprising the following steps:
- the method consists in providing the core with at least one gas evacuation duct.
- the method consists in ensuring the positioning of the core in the mold by means of the gas evacuation duct.
- the method consists in sealing the blank by closing off each gas discharge duct.
- the method consists in closing off each gas discharge duct with the aid of a stiffening element filling said duct.
- the method consists in positioning the gas evacuation pipe in the core in a place intended to constitute a housing for the part.
- the method consists in positioning the gas evacuation pipe so that it extends projecting on either side of the core so as to constitute a housing through the room.
- the method consists of preheating the blank before it is forged.
- Another object of the invention is to provide a core of lost material, completely surrounded by a metal envelope in which at least one discharge duct inserted into the core opens.
- the blank comprises a tight sealing and stiffening element placed in each exhaust duct.
- Another object of the invention is to obtain a hollow forging obtained from the blank, after forging and stripping.
- Another object of the invention is to obtain a hollow forging obtained from the process according to the invention.
- Figure 1 is a cutaway perspective view showing an embodiment of a part obtained by the manufacturing method according to the invention.
- Figure 2 illustrates a partially cut core implemented in a step of the method according to the invention.
- Figure 3 is a cutaway perspective view showing a core provided with gas exhaust ducts.
- Figure 4 illustrates the placement in a mold of a core as illustrated in FIG. 3.
- Figure 5 is a perspective view of a blank obtained after pouring a material into a mold illustrated in FIG. 4.
- Figure 6 illustrates a blank obtained after the molding operation and whose gas exhaust ducts are sealed.
- Figure 7 is a view of a lower forging die in which is positioned the blank shown in FIG. 6.
- Figure 8 illustrates a partly broken perspective view of the part obtained after the forging operation.
- Figure 9 illustrates a partly cutaway perspective view of the part of which part of the core was pierced.
- the object of the invention is to ensure the manufacture of a hollow forged part 1.
- the part 1 is a connecting rod having a body or arm 2 provided at each end with a head 3 of cylindrical shape. Each head 3 is provided with a through bore 4 opening on two opposite lateral faces 5.
- the bores 4 extend along axes parallel to each other and perpendicular to the direction of extension of the arm 2. that is clear from FIG. 1, the body 2 is hollow to the extent that it comprises a recess 7 opening into the bores 4 of the two heads 3.
- the part 1 is obtained according to the manufacturing method according to the invention which aims to ensure a molding operation on a core material lost to obtain a blank then subjected to a forging operation.
- the method according to the invention consists in producing a core 10 made of a lost material whose outer shape corresponds to the inner shape of the part 1 to be obtained, to the deformation undergone during a subsequent forging operation which will be described more precisely in the following description.
- the core 10 is made according to all known methods using lost materials.
- the core 10 is a salt core, a sand core made using a cold or hot box or "croning".
- the core consists of sand and resin.
- the core 10 is full.
- the core is adapted to have sufficient mechanical strength during the subsequent forging operation.
- the core 10 is adapted to withstand the stresses experienced during the forging operation.
- the core 10 is provided with at least one gas discharge duct 11.
- the core 10 is provided with two gas evacuation conduits 11.
- Each gas evacuation duct is made for example by a tube 11 pierced with holes 12 and inserted at least partly inside the core.
- Each duct 11 protrudes from the core 10.
- These ducts 11 are intended to evacuate the gases out of the mold, during the molding operation. These gases can come from the combustion of the resins forming part of the core 10.
- the outer surface of the core 10 can be made impermeable, for example by coating to force the gases to exit through the conduits. 11.
- each gas evacuation duct 11 is positioned in the core 10 in a place intended to constitute the bore 4 for the part.
- each duct 11 is placed so that its axis of symmetry coincides with the axis of the bore 4 in which the duct is placed.
- each gas evacuation duct 11 ensures the positioning of the core 10 in the mold during the molding operation.
- each gas evacuation duct 11 protrudes on either side of the core, that is to say from the lateral faces 5.
- the method consists in providing a molding operation on the core 10 by means of a conventional casting process.
- This foundry operation will not be described in detail because it is part of the technical knowledge of the skilled person and it can be implemented by any known foundry technique.
- the core 10 and as more particularly apparent from Fig.4 is intended to be placed in a mold 15 of which only the lower portion has been illustrated in FIG. 4.
- the gas discharge ducts 11 serve to position the core 10 inside the mold 15.
- the mold is of any type and may be a sand mold, a metal shell or any other molding method for producing a preform to be forged.
- the method thus consists in casting a metal around the core 10 to completely envelop it in order to obtain a blank 18 as illustrated in FIG. 5.
- the core 10 is completely wrapped except the exhaust ducts 11 when they are present.
- the method according to the invention aims to seal the blank 18 so that the core 10 is completely isolated vis-à-vis the external environment.
- the sealing of the blank 18 is ensured by sealing each gas evacuation duct 11 with a closure element 20 of all types (FIG 6).
- This closure member 20 can be made in any suitable manner by a metal plug, resin, plastic or ceramic. In this way, the core 10 is not in contact with the air.
- the method consists in closing off each gas evacuation duct 11 with the aid of a stiffening element 20 filling the duct.
- this element 20 may be a rod or a metal shaft completely filling each gas discharge duct 11. This element makes it possible to stiffen and quench each gas discharge duct 11.
- the method according to the invention consists of then forging the forging of the blank 18 to obtain the piece to the desired shape.
- This forging operation is performed either cold or hot.
- the blank 18 is preheated before being placed as illustrated in FIG. 7, in a die 22 of a forging press.
- the blank 18 is thus positioned between the two dies of a forging press of all known types.
- the core 10 still present in the blank 18, makes it possible to ensure against-pressure avoiding a collapse of the part at the recess 7, during the striking operation.
- the core 10 thus ensures a level of compression adapted to obtain good mechanical strength characteristics. It should be noted that the presence of the metal pins 20 inside the core 10 also contributes to the strength of the core.
- the piece 1 is removed from the dies as shown in Fig. 8. If the piece 1 has a burr 22 due to the forging operation, then this burr 22 is removed.
- the method according to the invention then consists in ensuring the breaking of the core 10 of the part 1 to obtain the hollow forging.
- This stripping operation may be performed by any appropriate means such as drilling, vibration and / or heat treatment to remove the entire core 10.
- it may be envisaged to drill at the heads 3 in order to obtain bores 4 (Fig. 9) and a heat treatment to remove the core located in the arm 2 to obtain the recess 7.
- the hollow part 1 is obtained (Fig. 1).
- the method according to the invention makes it possible to obtain a hollow forged part.
- the part 1 is a connecting rod. It is clear that the object of the invention can be implemented for different pieces with various shapes with one or more opening recesses.
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0757922A FR2921574B1 (en) | 2007-09-28 | 2007-09-28 | METHOD FOR MANUFACTURING HOLLOW FORGED PARTS AND PARTS THUS OBTAINED |
PCT/FR2008/051720 WO2009050382A2 (en) | 2007-09-28 | 2008-09-26 | Method for producing hollow forged parts and parts thus obtained |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2197606A2 true EP2197606A2 (en) | 2010-06-23 |
EP2197606B1 EP2197606B1 (en) | 2011-09-21 |
Family
ID=39321470
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP08840711A Not-in-force EP2197606B1 (en) | 2007-09-28 | 2008-09-26 | Method for producing hollow forged parts |
Country Status (5)
Country | Link |
---|---|
EP (1) | EP2197606B1 (en) |
CN (1) | CN101808762B (en) |
AT (1) | ATE525151T1 (en) |
FR (1) | FR2921574B1 (en) |
WO (1) | WO2009050382A2 (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2958193B1 (en) | 2010-04-06 | 2012-06-29 | Saint Jean Ind | PROCESS FOR MANUFACTURING LIGHT ALLOY FORGED PARTS INCORPORATING FULL OR DRAWN THICKNESS SECTIONS |
FR2969516B1 (en) | 2010-12-23 | 2013-08-16 | Saint Jean Ind | PROCESS FOR THE PRODUCTION OF SALT CORE BY ISOSTATIC COMPACTION UILIZABLE IN FOUNDRY OR FOUNDRY-FORGING |
CN106925720A (en) * | 2017-04-17 | 2017-07-07 | 大连旅桑实业有限公司 | A kind of sand mold mould for casting arm type casting long |
CN111842749A (en) * | 2020-07-13 | 2020-10-30 | 中国船舶工业集团公司第七0八研究所 | Manufacturing method of universal marine steel structure |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1938526A1 (en) * | 1969-07-29 | 1971-02-18 | Ideal Standard | Sand core with ventilation channels |
JPS5554259A (en) * | 1978-10-18 | 1980-04-21 | Hitachi Metals Ltd | Mold casting method |
JPS56114554A (en) * | 1980-02-13 | 1981-09-09 | Hitachi Metals Ltd | Mold |
JPS6076249A (en) * | 1983-09-30 | 1985-04-30 | Toyota Motor Corp | Sand core |
JPH05146841A (en) * | 1991-11-27 | 1993-06-15 | Toyota Motor Corp | Forging method |
JP3248676B2 (en) * | 1996-12-27 | 2002-01-21 | 株式会社シマノ | Bicycle crank and manufacturing method thereof |
JP3149374B2 (en) * | 1996-12-27 | 2001-03-26 | 株式会社シマノ | Bicycle hollow crank and manufacturing method thereof |
CN1057716C (en) * | 1997-02-18 | 2000-10-25 | 曾绍谦 | Mould core device capable of simple taking out mandrel for cold forging and use method thereof |
-
2007
- 2007-09-28 FR FR0757922A patent/FR2921574B1/en not_active Expired - Fee Related
-
2008
- 2008-09-26 WO PCT/FR2008/051720 patent/WO2009050382A2/en active Application Filing
- 2008-09-26 EP EP08840711A patent/EP2197606B1/en not_active Not-in-force
- 2008-09-26 AT AT08840711T patent/ATE525151T1/en not_active IP Right Cessation
- 2008-09-26 CN CN200880107675.9A patent/CN101808762B/en not_active Expired - Fee Related
Non-Patent Citations (1)
Title |
---|
See references of WO2009050382A3 * |
Also Published As
Publication number | Publication date |
---|---|
ATE525151T1 (en) | 2011-10-15 |
EP2197606B1 (en) | 2011-09-21 |
CN101808762B (en) | 2013-02-20 |
FR2921574B1 (en) | 2010-04-16 |
WO2009050382A2 (en) | 2009-04-23 |
FR2921574A1 (en) | 2009-04-03 |
CN101808762A (en) | 2010-08-18 |
WO2009050382A3 (en) | 2009-06-11 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP2585721B1 (en) | Process of manufacturing the metallic shield of a turbomachine blade | |
EP2197606B1 (en) | Method for producing hollow forged parts | |
FR2572394A1 (en) | METHOD FOR MANUFACTURING A CERAMIC TURBINE RING INTEGRATED WITH AN ANNULAR METAL SUPPORT | |
EP2555886B1 (en) | Method for the manufacture of forged light alloy workpieces with full and hollow cross-sections | |
CA2954024C (en) | Method for manufacturing a two-component blade for a gas turbine engine and blade obtained by such a method | |
EP1693127B1 (en) | Method of upsetting a metallic billet and jacket - top set for carrying out said method | |
WO2017060600A1 (en) | Method for additive manufacturing comprising a step of hot isostatic pressing | |
WO2009112725A1 (en) | Method for making metal plates, alone or in the form of a homogenous alloy, by centrifuging | |
CH622857A5 (en) | ||
JPH07102917A (en) | Sodium-enclosed hollow engine valve manufacturing method | |
EP0598664A1 (en) | Connecting-rod in two parts which are assembled on each other | |
FR2888288A3 (en) | IC engine cylinder head with partitioned inlet duct has partition made from same material as head during casting process | |
FR2828122A1 (en) | METHOD AND APPARATUS FOR MANUFACTURING A BOOSTER COMPRESSOR ROTOR | |
EP0586314B1 (en) | Method of making pieces of casting alloys with reinforced parts | |
FR2474908A1 (en) | CLOSED CHAMBER EXTRUSION METHOD AND DEVICE FOR CONFIGURING A METAL ROD IN A TULIP-SHAPED WORKPIECE | |
EP1470889A1 (en) | Method of manufacturing a piston, tool for carrying out said method and piston thus obtained | |
FR2748677A1 (en) | Method of cold forging motor vehicle clutch components | |
BE499042A (en) | ||
FR3036048A1 (en) | FOUNDRY METHOD WITH PERMANENT MOLD | |
FR2662471A1 (en) | Method for making spark plug wells in a cylinder head of an internal combustion engine, and set of elements intended to form at least one such spark plug well | |
FR2492291A1 (en) | Container for hot extrusion of metal powder - with flow-modifying profiling element(s) to improve prod. yield | |
EP3017164B1 (en) | Metal part produced by moulding comprising inner recesses, method for producing same and internal combustion engine comprising such a part | |
FR2905615A1 (en) | Producing block-engine oil circuit of internal combustion engine of automobile vehicle, comprises assembling tubular/curved elements to form tubular network, arranging tubular network in mold, and molding block-engine material in mold | |
FR2965596A1 (en) | Method for forging connecting rod in internal combustion engine, involves forming blank of rod during stamping process, and carrying-out hot calibration of head and foot of rod after heating pieces in atmosphere to compress core of rod | |
WO2010146293A1 (en) | Method for making a metal part including a fibrous annular reinforcement |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
17P | Request for examination filed |
Effective date: 20100316 |
|
AK | Designated contracting states |
Kind code of ref document: A2 Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MT NL NO PL PT RO SE SI SK TR |
|
AX | Request for extension of the european patent |
Extension state: AL BA MK RS |
|
17Q | First examination report despatched |
Effective date: 20101102 |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
RTI1 | Title (correction) |
Free format text: METHOD FOR PRODUCING HOLLOW FORGED PARTS |
|
DAX | Request for extension of the european patent (deleted) | ||
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MT NL NO PL PT RO SE SI SK TR |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D Free format text: NOT ENGLISH |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: EP |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D Free format text: LANGUAGE OF EP DOCUMENT: FRENCH |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 602008010049 Country of ref document: DE Effective date: 20111201 |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: VDEP Effective date: 20110921 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: HR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20110921 Ref country code: SE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20110921 Ref country code: NO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20111221 Ref country code: LT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20110921 Ref country code: FI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20110921 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: NV Representative=s name: BOVARD AG |
|
LTIE | Lt: invalidation of european patent or patent extension |
Effective date: 20110921 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20110921 Ref country code: LV Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20110921 Ref country code: CY Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20110921 Ref country code: GR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20111222 Ref country code: AT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20110921 |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: MK05 Ref document number: 525151 Country of ref document: AT Kind code of ref document: T Effective date: 20110921 |
|
BERE | Be: lapsed |
Owner name: C2FT Effective date: 20110930 |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FD4D |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MC Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20110930 Ref country code: SK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20110921 Ref country code: IE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20110921 Ref country code: CZ Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20110921 Ref country code: IS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20120121 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: EE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20110921 Ref country code: NL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20110921 Ref country code: PL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20110921 Ref country code: RO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20110921 Ref country code: PT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20120123 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20110930 |
|
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20110921 |
|
26N | No opposition filed |
Effective date: 20120622 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 602008010049 Country of ref document: DE Effective date: 20120622 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20110921 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: ES Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20120101 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20110926 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BG Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20111221 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: TR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20110921 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: HU Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20110921 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 9 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 10 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 11 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: IT Payment date: 20210910 Year of fee payment: 14 Ref country code: CH Payment date: 20210920 Year of fee payment: 14 Ref country code: FR Payment date: 20210930 Year of fee payment: 14 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20210928 Year of fee payment: 14 Ref country code: DE Payment date: 20210908 Year of fee payment: 14 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R082 Ref document number: 602008010049 Country of ref document: DE Representative=s name: CBDL PATENTANWAELTE GBR, DE |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R119 Ref document number: 602008010049 Country of ref document: DE |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20220926 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20220930 Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20220930 Ref country code: DE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20230401 Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20220930 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20220926 Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20220926 |