ATE461025T1 - Verfahren und vorrichtung zur herstellung einer rohrförmigen verbundstruktur - Google Patents
Verfahren und vorrichtung zur herstellung einer rohrförmigen verbundstrukturInfo
- Publication number
- ATE461025T1 ATE461025T1 AT06019100T AT06019100T ATE461025T1 AT E461025 T1 ATE461025 T1 AT E461025T1 AT 06019100 T AT06019100 T AT 06019100T AT 06019100 T AT06019100 T AT 06019100T AT E461025 T1 ATE461025 T1 AT E461025T1
- Authority
- AT
- Austria
- Prior art keywords
- sectors
- tool
- tubular structure
- radial direction
- base
- Prior art date
Links
- 239000002131 composite material Substances 0.000 title abstract 5
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C33/00—Moulds or cores; Details thereof or accessories therefor
- B29C33/44—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles
- B29C33/48—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles with means for collapsing or disassembling
- B29C33/485—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles with means for collapsing or disassembling cores or mandrels
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
- B29C53/80—Component parts, details or accessories; Auxiliary operations
- B29C53/82—Cores or mandrels
- B29C53/821—Mandrels especially adapted for winding and joining
- B29C53/824—Mandrels especially adapted for winding and joining collapsible, e.g. elastic or inflatable; with removable parts, e.g. for regular shaped, straight tubular articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
- B29C70/446—Moulding structures having an axis of symmetry or at least one channel, e.g. tubular structures, frames
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/045—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for noise suppression
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
- B29L2031/3076—Aircrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0206—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising noise reduction means, e.g. acoustic liners
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/96—Preventing, counteracting or reducing vibration or noise
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/603—Composites; e.g. fibre-reinforced
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
- Y10T29/49885—Assembling or joining with coating before or during assembling
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/4998—Combined manufacture including applying or shaping of fluent material
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/53—Means to assemble or disassemble
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/53—Means to assemble or disassemble
- Y10T29/53039—Means to assemble or disassemble with control means energized in response to activator stimulated by condition sensor
- Y10T29/53061—Responsive to work or work-related machine element
- Y10T29/53078—Responsive to work or work-related machine element with means to fasten by frictional fitting
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Composite Materials (AREA)
- General Engineering & Computer Science (AREA)
- Moulding By Coating Moulds (AREA)
- Shaping Of Tube Ends By Bending Or Straightening (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
- Extrusion Moulding Of Plastics Or The Like (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US11/230,533 US7707708B2 (en) | 2005-09-21 | 2005-09-21 | Apparatus for making a tubular composite structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE461025T1 true ATE461025T1 (de) | 2010-04-15 |
Family
ID=37603101
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT06019100T ATE461025T1 (de) | 2005-09-21 | 2006-09-12 | Verfahren und vorrichtung zur herstellung einer rohrförmigen verbundstruktur |
Country Status (4)
| Country | Link |
|---|---|
| US (2) | US7707708B2 (de) |
| EP (1) | EP1767325B1 (de) |
| AT (1) | ATE461025T1 (de) |
| DE (1) | DE602006012909D1 (de) |
Families Citing this family (34)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2449907B (en) * | 2007-06-07 | 2010-02-10 | Gkn Aerospace Services Ltd | Composite flange and method of making such flange |
| US8245750B2 (en) * | 2008-02-11 | 2012-08-21 | Rohr, Inc. | Segmented mandrel for high temperature bonding of metallic axisymmetric shells having complex curvatures |
| FR2927378B1 (fr) * | 2008-02-13 | 2013-02-08 | Snecma Propulsion Solide | Dispositif de maintien de deux elements dans une position relative precise avec compensation de dilatations differentielles. |
| US7640961B2 (en) | 2008-03-21 | 2010-01-05 | Rohr, Inc. | Apparatus and method for making a tubular composite barrel |
| GB0810870D0 (en) * | 2008-06-13 | 2008-07-23 | Advanced Composite Components | Tooling |
| US8025499B2 (en) * | 2008-11-03 | 2011-09-27 | Rohr, Inc. | Multi-segment tool and method for composite formation |
| US20100116938A1 (en) * | 2008-11-13 | 2010-05-13 | Kline William T | Method and apparatus for joining composite structural members and structural members made thereby |
| US9669579B2 (en) | 2008-11-13 | 2017-06-06 | The Boeing Company | Aircraft skin attachment system |
| US7798285B2 (en) * | 2008-11-14 | 2010-09-21 | Rohr, Inc. | Acoustic barrel for aircraft engine nacelle including crack and delamination stoppers |
| JP5576650B2 (ja) * | 2009-12-25 | 2014-08-20 | 川崎重工業株式会社 | 複合材料構造物製造用成形型 |
| GB2478312B (en) * | 2010-03-02 | 2012-08-22 | Gkn Aerospace Services Ltd | Seamless acoustic liner |
| US8511359B2 (en) | 2010-09-23 | 2013-08-20 | The Boeing Company | Layup mandrel having changeable shape and method of using the same |
| US9016042B2 (en) | 2011-05-20 | 2015-04-28 | Rohr, Inc. | Reinforcement members for aircraft propulsion system components configured to address delamination of the inner fixed structure |
| GB201116476D0 (en) | 2011-09-26 | 2011-11-09 | Rolls Royce Plc | Mandrel for forming a component |
| RU2482028C1 (ru) * | 2011-12-21 | 2013-05-20 | Открытое акционерное общество "Национальный институт авиационных технологий" (ОАО НИАТ) | Стапель для сборки воздухозаборника двигателя летательного аппарата |
| JP6100461B2 (ja) * | 2011-12-27 | 2017-03-22 | 三菱航空機株式会社 | ベント部材、航空機の主翼 |
| US8685302B2 (en) | 2012-02-20 | 2014-04-01 | Honeywell International Inc. | Monolithic acoustically-treated composite structures and methods for fabricating the same |
| ITTO20120287A1 (it) * | 2012-03-30 | 2013-10-01 | Alenia Aermacchi Spa | Sistema posizionamento settori appartenenti ad un dispositivo per la realizzazione di una sezione di fusoliera di un aereo |
| ITTO20120286A1 (it) * | 2012-03-30 | 2013-10-01 | Alenia Aermacchi Spa | Sistema di vincolo settori appartenenti ad un dispositivo per la realizzazione di una sezione di fusoliera di un aereo |
| FR2990376B1 (fr) * | 2012-05-10 | 2015-01-09 | Aircelle Sa | Procede de fabrication d'une peau en composite formant virole non demoulable |
| FR2991628A1 (fr) * | 2012-06-12 | 2013-12-13 | Aircelle Sa | Ensemble d'outillage pour la fabrication d'une piece composite et procede de fabrication d'une piece composite. |
| FR3007063B1 (fr) * | 2013-06-13 | 2015-07-03 | Composite Ind | Piece de materiau abradable pour la fabrication d'un secteur de joint annulaire abradable pour turbomachine et procede de fabrication d'une telle piece |
| FR3007064B1 (fr) | 2013-06-13 | 2018-06-29 | Composite Industrie | Secteur de joint annulaire abradable pour turbomachine et procede de fabrication d'une telle piece |
| FR3009992B1 (fr) * | 2013-08-28 | 2015-09-11 | Aircelle Sa | Outillage a cles et panneau composite notamment pour nacelle de moteur d’aeronef fabrique a l’aide d’un tel outillage |
| GB201407313D0 (en) * | 2014-04-25 | 2014-06-11 | Rolls Royce Plc | Intake liner |
| CN104691779B (zh) * | 2015-01-13 | 2016-12-07 | 哈尔滨飞机工业集团有限责任公司 | 一种用于复合材料主桨叶包铁更换修理的工艺方法 |
| FR3044253B1 (fr) * | 2015-11-26 | 2018-05-18 | Safran Aircraft Engines | Moule pour la fabrication d'un carter de soufflante de turbine a gaz en materiau composite et procede de fermeture d'un tel moule |
| CN106799798A (zh) * | 2017-02-13 | 2017-06-06 | 中国船舶重工集团公司第七二五研究所 | 一种双曲面回转体复合材料制品的分体成型模具 |
| GB2575295B (en) * | 2018-07-04 | 2022-06-15 | Rolls Royce Plc | An Alignment Tool |
| FR3084445B1 (fr) * | 2018-07-25 | 2021-01-22 | Safran Aircraft Engines | Fabrication d'une chambre de combustion en materiau composite |
| CN112339298B (zh) * | 2021-01-11 | 2021-03-23 | 中国人民解放军国防科技大学 | 一种大尺寸筒体成型方法 |
| CN113247296B (zh) * | 2021-05-31 | 2022-08-26 | 浙江万丰飞机制造有限公司 | 一种飞机薄壁部件的安装工装的制作方法 |
| CN115609954B (zh) * | 2022-09-28 | 2025-08-22 | 北京卫星制造厂有限公司 | 一种尾裙蜂窝夹层结构锥段成型工艺方法 |
| CN116901414B (zh) * | 2023-07-21 | 2025-09-16 | 江西强发科技有限公司 | 一种克拉管连续加工生产设备 |
Family Cites Families (31)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1835986A (en) | 1927-10-12 | 1931-12-08 | Nat Rubber Machinery Co | Collapsible tire building form |
| US2586300A (en) | 1947-08-07 | 1952-02-19 | John F Campbell | Collapsible v-belt mold |
| DE1262570B (de) | 1964-06-18 | 1968-03-07 | Mueller Ernst Kg | Hohldorn zum Herstellen von aus schraubenlinienfoermig gewickelten Kunststoffstreifen bestehenden Rohren oder Behaeltermaenteln beliebiger Laenge |
| DE1504597B2 (de) | 1965-11-06 | 1971-04-01 | Muller geb Schneider, Hedwig Ida, 5905 Freudenberg | Hohldorn zum herstellen von aus schrabenlinienfoermig ge wickelten kunststoffstreifen bestehenden rohren oder behaeltermaentel beliebiger laenge |
| US3768954A (en) | 1969-06-03 | 1973-10-30 | R Marsh | Device for forming and handling concrete pipe |
| US3785894A (en) * | 1971-10-12 | 1974-01-15 | Goodyear Tire & Rubber | Tire building drum |
| DE2259690A1 (de) | 1972-12-06 | 1974-06-12 | Bautenberg Gmbh | Hohler wickeldorn |
| DE2352373A1 (de) | 1973-10-18 | 1975-04-24 | Hermann Sarres | Wickeldorn zur herstellung von zylindrischen koerpern aus wickel- oder spritzfaehigen kunststoffen |
| GB1522558A (en) | 1976-04-05 | 1978-08-23 | Rolls Royce | Duct linings |
| DE2652862C2 (de) * | 1976-11-20 | 1979-01-04 | Basf Ag, 6700 Ludwigshafen | Formkern zum Herstellen von aus faserverstärktem Kunstharz bestehenden Hohlkörpern |
| US4288277A (en) | 1979-07-17 | 1981-09-08 | Lembit Siilats | Molding system with retracting mold |
| US4278490A (en) | 1979-12-21 | 1981-07-14 | Owens-Corning Fiberglas Corporation | Sleeve for changing diameter of collapsible mandrel |
| US4436574A (en) | 1982-12-13 | 1984-03-13 | Eagle-Picher Industries, Inc. | Radial mandrel |
| US4462787A (en) | 1983-02-01 | 1984-07-31 | Bogardus Jr Carl R | Cantilevered mandrel assembly |
| EP0154038B1 (de) | 1984-02-08 | 1989-03-15 | Georg Prinzing GmbH & Co. KG Betonformen- und Maschinenfabrik | Formkern mit verstellbaren Teilen |
| IT1177395B (it) | 1984-12-12 | 1987-08-26 | Dino Piccoli | Apparecchiatura per la produzione in discontinuo di strutture tubolari |
| DE3666180D1 (en) | 1986-08-23 | 1989-11-16 | Vv System Ag | Dilatable ring for sealing an envelope to the beads of a tyre to be retreaded |
| US5022845A (en) | 1989-04-25 | 1991-06-11 | Hercules Incorporated | Segmented mandrel for forming composite articles |
| AU9108391A (en) | 1991-02-19 | 1992-09-15 | John W. Boyd | Method and apparatus for producing a filament wound tank shell |
| US5228374A (en) | 1991-08-09 | 1993-07-20 | Santeramo Sr Joseph J | Table saw fence assembly |
| US5266137A (en) | 1992-11-10 | 1993-11-30 | Hollingsworth Ritch D | Rigid segmented mandrel with inflatable support |
| DE4340951A1 (de) | 1992-12-04 | 1994-06-09 | Grumman Aerospace Corp | Einstückiges Triebwerkeinlaß-Schallrohr |
| FR2767560B1 (fr) | 1997-08-19 | 1999-11-12 | Aerospatiale | Ensemble reducteur de bruit pour turboreacteur d'aeronef |
| US6004250A (en) * | 1997-09-30 | 1999-12-21 | Wyko, Inc. | System and method for releaseably attaching outer segments to a drum useful in the manufacture of vehicle tires |
| US6458309B1 (en) | 1998-06-01 | 2002-10-01 | Rohr, Inc. | Method for fabricating an advanced composite aerostructure article having an integral co-cured fly away hollow mandrel |
| DE10010917A1 (de) | 2000-03-06 | 2001-09-13 | Baumgaertner Maschf Gmbh | Formmantel |
| FR2821788B1 (fr) | 2001-03-09 | 2004-04-02 | Eads Airbus Sa | Procede de fabrication d'un panneau a couche resistive acoustique adaptee et panneau acoustique ainsi obtenu |
| FR2841494B1 (fr) | 2002-06-27 | 2005-11-25 | Airbus France | Outillage de moulage a clef notamment pour la realisation d'entree d'air sans eclisse |
| US7497679B2 (en) | 2004-06-21 | 2009-03-03 | Mamada Sangyo | Injection mold having a switching valve |
| US7571527B2 (en) | 2005-03-29 | 2009-08-11 | The Boeing Company | Mandrel for fabrication of a monolithic composite nacelle panel |
| US7640961B2 (en) * | 2008-03-21 | 2010-01-05 | Rohr, Inc. | Apparatus and method for making a tubular composite barrel |
-
2005
- 2005-09-21 US US11/230,533 patent/US7707708B2/en active Active
-
2006
- 2006-09-12 AT AT06019100T patent/ATE461025T1/de not_active IP Right Cessation
- 2006-09-12 EP EP06019100A patent/EP1767325B1/de active Active
- 2006-09-12 DE DE602006012909T patent/DE602006012909D1/de active Active
-
2010
- 2010-03-19 US US12/727,922 patent/US7861394B2/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| EP1767325B1 (de) | 2010-03-17 |
| US20100170633A1 (en) | 2010-07-08 |
| US7861394B2 (en) | 2011-01-04 |
| EP1767325A2 (de) | 2007-03-28 |
| EP1767325A3 (de) | 2007-05-02 |
| DE602006012909D1 (de) | 2010-04-29 |
| US20070062022A1 (en) | 2007-03-22 |
| US7707708B2 (en) | 2010-05-04 |
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