EP2025593B1 - Ruder für Schiffe - Google Patents

Ruder für Schiffe Download PDF

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Publication number
EP2025593B1
EP2025593B1 EP08015619.3A EP08015619A EP2025593B1 EP 2025593 B1 EP2025593 B1 EP 2025593B1 EP 08015619 A EP08015619 A EP 08015619A EP 2025593 B1 EP2025593 B1 EP 2025593B1
Authority
EP
European Patent Office
Prior art keywords
rudder
cross
sectional
propeller
rudder blade
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.)
Expired - Lifetime
Application number
EP08015619.3A
Other languages
German (de)
English (en)
French (fr)
Other versions
EP2025593A3 (de
EP2025593A2 (de
Inventor
Dirk Lehmann
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Becker Marine Systems GmbH and Co KG
Original Assignee
Becker Marine Systems GmbH and Co KG
Priority date (The priority date 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 date listed.)
Filing date
Publication date
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Application filed by Becker Marine Systems GmbH and Co KG filed Critical Becker Marine Systems GmbH and Co KG
Publication of EP2025593A2 publication Critical patent/EP2025593A2/de
Publication of EP2025593A3 publication Critical patent/EP2025593A3/de
Application granted granted Critical
Publication of EP2025593B1 publication Critical patent/EP2025593B1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H25/00—Steering; Slowing-down otherwise than by use of propulsive elements; Dynamic anchoring, i.e. positioning vessels by means of main or auxiliary propulsive elements
    • B63H25/06—Steering by rudders
    • B63H25/38—Rudders
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H25/00—Steering; Slowing-down otherwise than by use of propulsive elements; Dynamic anchoring, i.e. positioning vessels by means of main or auxiliary propulsive elements
    • B63H25/06—Steering by rudders
    • B63H25/38—Rudders
    • B63H2025/388—Rudders with varying angle of attack over the height of the rudder blade, e.g. twisted rudders

Definitions

  • the invention relates to a rudder arrangement for fast ships with highly loaded propellers.
  • Ship rudders such as full-floating rudder or balance rudder, with or without hinged fin, are known in various embodiments.
  • the DE 44 26 953 A1 discloses a rudder or rudder nozzle for marine craft having a pivoting main rudder or swivel rudder nozzle and a fin articulated to the main rudder or rudder nozzle, the main rudder or rudder nozzle being located at a location in the floor structure of the ship's stern arranged known Ruderkokers, flat hollow-plate bearing is rotatably mounted and wherein in the hollow-column bearing a Flossenruderschaft is rotatably mounted, which is brought via a lever-pin slide-fork connection with the fin in operative connection.
  • the GB 332 082 A describes a ship's rudder of the rowing types "balanced” or "semibalanced".
  • the side surfaces of the rudder converge asymmetrically from either side of the rudder axis to a leading edge offset above the axis of the bolt to one side and below said axis to the other side, the leading edge being opposed to the water of the screw stream during normal forward travel of the vessel. Further, the side surfaces converge symmetrically from both sides of the rudder axis to a trailing edge located in the median plane of the rudder.
  • a rudder is described in which in a cross-sectional view, the nose strip is formed in a symmetrical wing shape, wherein the end bar of the upper part above the propeller shaft and the lower part are rotated below the propeller shaft to each other, so that they correspond to flow vectors. Furthermore, cross-sections of another rudder are disclosed in which a cross-section is offset from the other cross-section in the region of the leading edge.
  • the DE-U-87 08 276 discloses a rudder, in particular a balance profiled rudder for watercraft, with a fin articulated on the rudder blade and with a rudder rod bearing which is provided as a cantilever with a central longitudinal inner bore for receiving the rudder shank for the rudder blade, to the rudder blade connected to the rudder end is formed in sufficient extent, in its inner bore has a bearing for supporting the rudder stock, and on its outer wall surface approximately at the same height to the bearing in the inner longitudinal bore of the rudder rod bearing another bearing for receiving and supporting the rudder blade has, the rudder stock with his in the rudder blade lying end up in the range of the propeller shaft center or to above the propeller shaft center is guided.
  • the KR 2001-0009112 describes a ship's rudder, in which the front end at the level of the propeller axis in the upper and lower part separated and these are twisted in the opposite direction with each other. At the adjacent area of the upper and lower part of a streamlined bulb is provided according to the asymmetric property of the complex rotational flows.
  • the rudder assembly for fast ships an oar consisting of a rudder blade and a rudder associated, arranged on a drivable propeller propeller, on.
  • the rudder blade consists of only two superimposed rudder blade sections, the propeller facing, a rounded profile having front nose strips are offset from each other such that the one nose bar to port or starboard and the other nose bar are offset to starboard or port side, the two side panels of the rudder blade converge in an end bar facing away from the propeller.
  • the rudder assembly on a fin, which is articulated to the rudder blade in the region of the end bar.
  • the nose strips of the two rudder blade sections are offset from each other, so that the nose strip of the upper rudder blade section to port and the nose strip of the lower rudder blade section to starboard or the nose strip of the upper rudder blade section to starboard and the nose strip of the lower rudder blade section are offset to port, respectively obtained two mutually mirror-inverted cross-sectional profiles of the two rudder blade sections.
  • the rudder trunk bearing is designed as a cantilever beam with a central inner longitudinal bore for receiving the rudder stock for the rudder blade and extending into the rudder end connected to the rudder blade, wherein for storage of the rudder stock a single bearing is arranged in the inner longitudinal bore of the rudder trunk bearing, with its free End in a recess, collection o. The like.
  • the rudder stock is led out in its end with a portion of the rudder trunk bearing and releasably connected to the, free, lower end of this section with the rudder blade, with no storage between the rudder blade and the rudder trunk bearing is provided and the connection of the rudder stock with the rudder blade is above the propeller shaft center, the inner bearing is arranged for the storage of the rudder stock in the rudder trunk in the end of the rudder trunk bearing.
  • the upper rudder blade portion of the rudder blade has a cross-sectional profile extending from a front of the leading edge bead extending to the rear end strip and up to a maximum profile thickness conically expanding front cross-sectional area and adjoining the front cross-sectional area and is formed to the rear end bar conically tapered rear cross-sectional area, wherein the two formed by a running in the longitudinal direction of the rudder blade center line
  • Cross-sectional area portion have different sizes, of which the larger cross-sectional area portion is located on the port side and the smaller cross-sectional area is starboard side lying, wherein the two formed by the center line in the rear region of the cross-sectional profile cross-sectional area portion are the same, and that the lower rudder blade portion of the rudder blade has a cross-sectional profile, the from a front cross-sectional area extending from the leading leading edge and extending to a maximum profile thickness, and being formed adjacent to the anterior cross-sectional area and forming a rearward cross-sectional area, the two extending from a centerline extending longitudinally of the rudder leaf formed front cross-sectional area portion have different sizes, of which the larger Querterrorismsf lying on the starboard side and the smaller cross-sectional area portion is located on the port side, wherein the two of the center line in the rear region of the cross-sectional profile formed cross-sectional area are the same, so that the propeller associated with the nose of the upper rudder blade section
  • the two propeller-side cross-sectional surface portions of the cross-sectional profile of the upper rudder blade portion have edge regions with a flat arc and a highly curved arc, the two facing away from the propeller cross-sectional surface portions of the cross-sectional profile of the upper rudder blade portion tangentially extending edge region, wherein the cross-sectional surface portion with the edge region with a highly curved arc curve starboard side lying down.
  • the two propeller-side cross-sectional surface portions of the cross-sectional profile of the lower rudder blade portion have edge region with a flat arc and a highly curved arc, the two facing away from the propeller cross-sectional surface portions of the cross-sectional profile of lower rudder blade portion have tangentially extending edge regions, wherein the cross-sectional surface portion is lying on the port side with the edge region with strongly arched bow course.
  • a rudder box bearing 100 a rudder blade and 140 denotes a rudder stock.
  • the rudder blade 100 is assigned a propeller 220 arranged on a drivable propeller shaft 225.
  • the rudder blade 100 according to Fig. 2A . 2 B and 3 has two superimposed rudder sections 10, 20, the propeller 220 facing front nose strips 11, 31 are offset such that the one nose strip 11 are offset to port BB and the other nose strip 21 to starboard SB.
  • the two side wall surfaces 100a, 100b of the rudder blade 100 merge into an end bar 30 facing away from the propeller 220.
  • the upper and lower rudder blade sections 10, 20 of the rudder blade 100 are formed as follows:
  • the upper rudder blade section 10 has according to Fig. 4 a cross-sectional profile 12, which is formed by a front of the leading edge 11 to the end bar 30 to a maximum profile thickness 13 conically widening front cross-sectional area 14. Adjoining this front cross-sectional area 14 is a rear cross-sectional area 15, which extends to the end bar 30 and tapers to the end bar 30.
  • the front cross-sectional area 14 is subdivided by a center line M1 extending in the longitudinal direction of the rudder blade 100 into two cross-sectional area sections 14a, 14b which have different sizes.
  • the larger cross-sectional area section 14a lies on the port side and the smaller cross-sectional area section 14b faces the starboard side.
  • the rear cross-sectional area 15 is also divided from the center line M1 into two cross-sectional area portions 15a, 15b.
  • the two cross-sectional surface portions 15a, 15b are the same size and have the same shapes.
  • the two propeller-side cross-sectional surface sections 14a, 14b of the cross-sectional profile 12 of the upper rudder blade section 10 have edge regions 16, 16a with a flat curved path 16'a, wherein the two cross-sectional surface sections 15a, 15b of the cross-sectional profile 12 of the upper rudder blade section 10 facing away from the propeller 220 have tangentially extending edge regions 17 17a.
  • the cross-sectional area section 14b with the edge region 16a with a strongly arched curve 16'a is located on the starboard side.
  • the lower rudder blade section 20 has according to Fig. 5 a mirrored cross-sectional profile 22.
  • This cross-sectional profile 20 extends from a cross-sectional area conically widening from the front leading edge 21 to the end strip 30 and up to a maximum profile thickness 23.
  • Adjoining this front cross-sectional area 24 is a cross-sectional area 25 extending to the end bar 30, which tapers to the end bar 30.
  • the front cross-sectional area 24 is subdivided by a center line M2 extending in the longitudinal direction of the rudder blade 100 into two cross-sectional area sections 24a, 24b which have different sizes.
  • the larger cross-sectional area section 24b is located on the starboard side and the small cross-sectional area section 24a faces the port side.
  • the rear cross-sectional area 25 is also divided from the center line M2 into two cross-sectional area portions 25a, 25b.
  • the two cross-sectional surface portions 25a, 25b are the same size and have the same
  • the two propeller-side cross-sectional surface sections 24a, 24b of the cross-sectional profile 22 of the upper rudder blade section 20 have edge regions 26, 26a with a flat arc 26 'and a curved arc 26'a, the two facing away from the propeller 220 cross-sectional surfaces 25a, 25b of the cross-sectional profile 22 of the lower Ruderblattabiteses 20 tangentially extending edge regions 27, 27a have.
  • the cross-sectional surface portion 24b with the edge region 26'a with a strongly arched arc curve 26'a is located on the port side.
  • the design and arrangement of the two rudder blade sections 10, 20 provides that the propeller 220 associated nose strip 11 of the upper rudder blade section 10 port side to the center line M1 and the nose strip 21 of the lower rudder blade section 20 starboard side lying to the center line M2, wherein the two rudder blade sections 10, 20th in the rear region of the rudder blade 100 are brought together in an end strip 30.
  • Fig. 2A . 2 B . 3, 4 and 5 are the two rudder blade sections 10, 20 of the rudder blade 100 with their cross-sectional profiles 12, 22 arranged to each other such that the side wall portions of the rudder blade, which are in the region of the highly curved arc curves 16'a and 26'a the cross-sectional surface portions 14b and 24b starboard side and port side, then the cross-sectional surface portion 14b of the cross-sectional profile 12 of the starboard side and the cross-sectional surface portion 24b of the cross-sectional profile 22 of the port side are facing, so that the nose strips 11, 21 of the two rudder blade sections 10, 20 are port side and starboard side.
  • the invention also includes an embodiment of the rudder, according to which the two rudder blade sections 10, 20 of the rudder blade 100 are arranged with their cross-sectional profiles 12, 22 to each other such that the side wall portions of the rudder blade, in the region of the highly curved arc curves 16'a and 26'a of the cross-sectional surface portions 14b and 24b are port side and starboard side, in which case the cross-sectional surface portion 14b of the port side cross-sectional profile 12 and the cross-sectional surface portion 24b of the starboard cross-sectional profile 22 are facing, so that the nose strips 11, 21 of the two rudder blade sections 10, 20 are starboard side and port side.
  • a hull 120 a rudder box bearing, 100 a rudder blade and 140 denotes a rudder stock.
  • a fin 135 is hinged.
  • the rudder blade 100 has a preferably cylindrical recess 155 for receiving the free end of the rudder trunk bearing 120.
  • the rudder trunk bearing 120 is provided as a cantilever with a central inner longitudinal bore 125 for receiving the rudder stock 140 for the rudder blade 100.
  • the rudder trunk bearing 120 is sufficiently formed to the rudder blade 100 connected to the rudder end.
  • the rudder trunk bearing 120 In its inner bore 125, the rudder trunk bearing 120 has a bearing 150 for supporting the rudder stock 140, wherein preferably this bearing 150 is arranged in the lower end region 120b of the rudder trunk bearing 120.
  • the rudder stock 140 is led out with its end 140b with a section 145 from the rudder trunk bearing 120.
  • this extended portion 145 of the rudder stock 140 is fixedly connected to the rudder blade 100 at 170, but here too a connection is provided which allows a release of the rudder blade 100 of the rudder stock 140 when the propeller shaft is to be replaced.
  • the connection of the rudder stock 140 in the area 170 with the rudder blade 100 is above the propeller shaft center 200, so that only the rudder blade 100 must be removed from the rudder stock 140 for the expansion of the propeller shaft, while pulling out the rudder stock 140 from the rudder trunk 120 not is necessary, since both the free lower end 120b of the rudder trunk bearing 120 and the free lower end of the rudder stock 140 are above the propeller shaft center.
  • both the free lower end 120b of the rudder trunk bearing 120 and the free lower end of the rudder stock 140 are above the propeller shaft center.
  • a single inner bearing 150 is provided for the storage of the rudder stock 140 in the rudder trunk bearing 120; a further bearing for the rudder blade 100 on the outer wall of the rudder trunk bearing 120 is omitted.
  • the rudder blade 100 is provided with a recess or recess indicated at 160.
  • the rudder trunk bearing 120 is provided as a cantilever with a central inner longitudinal bore 125 for receiving the rudder stock 140 for the rudder blade 100. Furthermore, the rudder trunk bearing 120 is formed reaching into the rudder blade 100 connected in the rudder end and has in its inner bore 125 a bearing 150 for supporting the rudder stock 140 in the rudder trunk bearing 120. With its free end 120 b, the rudder trunk bearing 120 extends into a recess 160 in the rudder blade 100, the rudder stock 140 being led out of the rudder trunk bearing 120 in its end region 140 b with a section 145.
  • this extended portion 145 of the rudder stock 140 is connected to the rudder blade 100, wherein the connection of the rudder stock 140 with the rudder blade 100 above the propeller shaft center 200 is lying.
  • the inner bearing 150 is preferably provided in the end region 120b of the rudder trunk bearing 120.

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  • Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Ocean & Marine Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Toys (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Physical Or Chemical Processes And Apparatus (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
  • Wind Motors (AREA)
  • Soil Working Implements (AREA)
  • Steroid Compounds (AREA)
  • Specific Sealing Or Ventilating Devices For Doors And Windows (AREA)
EP08015619.3A 2004-04-23 2004-06-22 Ruder für Schiffe Expired - Lifetime EP2025593B1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE202004006453U DE202004006453U1 (de) 2004-04-23 2004-04-23 Ruder für Schiffe
EP04740144A EP1626897B1 (de) 2004-04-23 2004-06-22 Ruder für schiffe

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
EP04740144A Division EP1626897B1 (de) 2004-04-23 2004-06-22 Ruder für schiffe

Publications (3)

Publication Number Publication Date
EP2025593A2 EP2025593A2 (de) 2009-02-18
EP2025593A3 EP2025593A3 (de) 2009-04-01
EP2025593B1 true EP2025593B1 (de) 2016-08-17

Family

ID=33441997

Family Applications (3)

Application Number Title Priority Date Filing Date
EP07013643.7A Expired - Lifetime EP1857358B1 (de) 2004-04-23 2004-06-22 Ruder für Schiffe
EP08015619.3A Expired - Lifetime EP2025593B1 (de) 2004-04-23 2004-06-22 Ruder für Schiffe
EP04740144A Revoked EP1626897B1 (de) 2004-04-23 2004-06-22 Ruder für schiffe

Family Applications Before (1)

Application Number Title Priority Date Filing Date
EP07013643.7A Expired - Lifetime EP1857358B1 (de) 2004-04-23 2004-06-22 Ruder für Schiffe

Family Applications After (1)

Application Number Title Priority Date Filing Date
EP04740144A Revoked EP1626897B1 (de) 2004-04-23 2004-06-22 Ruder für schiffe

Country Status (14)

Country Link
EP (3) EP1857358B1 (zh)
JP (2) JP4410656B2 (zh)
KR (2) KR20050103137A (zh)
CN (2) CN101016082B (zh)
AT (1) ATE431285T1 (zh)
DE (8) DE202004006453U1 (zh)
DK (2) DK1857358T3 (zh)
ES (3) ES2323784T3 (zh)
HK (1) HK1083813A1 (zh)
PL (2) PL1857358T3 (zh)
PT (1) PT1626897E (zh)
SI (1) SI1626897T1 (zh)
TW (2) TWI302894B (zh)
WO (1) WO2005113332A1 (zh)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100735724B1 (ko) * 2006-06-15 2007-07-06 김효철 이중차단 틈새 유동차단기가 고정부와 가동부 사이에설치된 선박용 타 장치
DE102006047755A1 (de) * 2006-10-06 2008-04-10 Wobben, Aloys Seitliches Schiffsruder
KR100899737B1 (ko) * 2007-10-29 2009-05-27 대우조선해양 주식회사 러더벌브를 구비한 선박의 비대칭 전가동러더
DE202007015941U1 (de) * 2007-11-13 2008-01-17 Becker Marine Systems Gmbh & Co. Kg Ruder für Schiffe
ATE458670T1 (de) * 2007-11-13 2010-03-15 Becker Marine Sys Gmbh & Co Kg Ruderanordnung für schiffe mit höheren geschwindigkeiten mit einem kavitationsreduzierenden, twistierten, insbesondere vollschweberuder
DE202007016164U1 (de) * 2007-11-16 2008-01-24 Becker Marine Systems Gmbh & Co. Kg Hochleistungsruder für Schiffe
KR101010850B1 (ko) * 2007-11-27 2011-01-26 삼성중공업 주식회사 캐비테이션 저감용 비대칭 단면 타
CN101186233B (zh) * 2007-12-19 2011-05-11 沪东中华造船(集团)有限公司 减少船舶尾部半平衡悬挂舵舵叶表面空化现象的方法
ES2385822T3 (es) * 2008-08-13 2012-08-01 Becker Marine Systems Gmbh & Co. Kg Dispositivo de timón para embarcaciones de gran velocidad, con un timón reductor de la cavitación, torsionado, en especial completamente suspendido
CA2639804C (en) * 2008-08-13 2011-02-01 Becker Marine Systems Gmbh & Co. Kg Rudder arrangement for ships having higher speeds comprising a cavitation-reducing twisted, in particular balanced rudder
KR100903066B1 (ko) * 2009-04-15 2009-06-18 대우조선해양 주식회사 러더벌브를 구비한 선박의 비대칭 전가동러더
KR100958075B1 (ko) * 2009-04-15 2010-05-14 대우조선해양 주식회사 러더벌브를 구비한 선박의 비대칭 전가동러더
KR100903067B1 (ko) * 2009-04-16 2009-06-18 대우조선해양 주식회사 러더벌브를 구비한 선박의 비대칭 전가동러더
KR100901393B1 (ko) * 2009-04-17 2009-06-05 대우조선해양 주식회사 러더벌브를 구비한 선박의 비대칭 전가동러더
ATE555981T1 (de) 2009-06-17 2012-05-15 Daewoo Shipbuilding & Marine Schiffsruder
KR200447816Y1 (ko) * 2009-07-10 2010-02-23 대우조선해양 주식회사 선박용 방향타
DE102009047244A1 (de) * 2009-11-27 2011-06-01 Van Der Velden Barkemeyer Gmbh Verfahren und Verbindungsvorrichtung zur Verbindung eines Ruder- oder Propellerschafts mit einer antreibenden oder anzutreibenden Baugruppe eines Schiffes
NO336848B1 (no) * 2013-03-08 2015-11-16 Rolls Royce Marine As Rudders Roranordning
NO336378B1 (no) * 2013-06-20 2015-08-10 Rolls Royce Marine As Rudders Roranordning
CN105416554B (zh) * 2015-12-24 2017-09-29 九成投资集团有限公司 带有曲向导边的舵叶
CN105438430A (zh) * 2015-12-24 2016-03-30 大连船舶重工集团舵轴有限公司 曲向导流悬挂舵
JP6582296B2 (ja) * 2016-03-31 2019-10-02 三井Ｅ＆Ｓ造船株式会社 船舶用舵及び船舶
CN109436278A (zh) * 2017-03-17 2019-03-08 合肥智慧龙图腾知识产权股份有限公司 一种组合式船舶用舵叶
JP7148329B2 (ja) * 2018-09-03 2022-10-05 住友重機械マリンエンジニアリング株式会社 舵板、及び船舶
CN110723263B (zh) * 2019-09-17 2020-07-14 广州文冲船舶修造有限公司 一种船舶舵叶改装工艺
CN111746749A (zh) * 2020-06-22 2020-10-09 沪东中华造船(集团)有限公司 一种舵桨匹配系统

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DE8708276U1 (de) * 1987-06-12 1987-08-27 Willi Becker Ingenieurbüro GmbH, 2000 Hamburg Ruder, insbesondere Balance-Profilruder für Wasserfahrzeuge

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DE2834015C2 (de) * 1978-08-03 1980-07-03 Howaldtswerke-Deutsche Werft Ag Hamburg Und Kiel, 2300 Kiel Ruderausbildung für Schiffe
DE8016289U1 (de) * 1980-06-20 1980-10-02 Mti Manoevriertechnisches Institut Gmbh, 2000 Hamburg Ruder fuer wasserfahrzeuge und schwimmendes geraet
JPS5816996A (ja) * 1981-07-22 1983-01-31 Ishikawajima Harima Heavy Ind Co Ltd 舵
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DE29609745U1 (de) * 1996-06-04 1996-08-29 Willi Becker Ingenieurbüro GmbH, 20099 Hamburg Ruder für Seeschiffe
KR100346512B1 (ko) 1999-07-07 2002-08-01 삼성중공업 주식회사 선박의 방향타
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Patent Citations (1)

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Publication number Priority date Publication date Assignee Title
DE8708276U1 (de) * 1987-06-12 1987-08-27 Willi Becker Ingenieurbüro GmbH, 2000 Hamburg Ruder, insbesondere Balance-Profilruder für Wasserfahrzeuge

Also Published As

Publication number Publication date
JP2007131298A (ja) 2007-05-31
TWI302894B (en) 2008-11-11
ES2604756T3 (es) 2017-03-09
EP1857358A2 (de) 2007-11-21
EP1857358A3 (de) 2007-12-05
DE202004021474U1 (de) 2008-04-10
EP2025593A3 (de) 2009-04-01
DK1857358T3 (da) 2017-01-02
DE202004021218U1 (de) 2007-04-19
TWI295982B (en) 2008-04-21
ES2323784T3 (es) 2009-07-24
PL1857358T3 (pl) 2017-02-28
EP1626897B1 (de) 2009-05-13
KR20090029249A (ko) 2009-03-20
CN100351143C (zh) 2007-11-28
DE202004021223U1 (de) 2007-04-19
ES2602562T3 (es) 2017-02-21
ATE431285T1 (de) 2009-05-15
KR20050103137A (ko) 2005-10-27
PT1626897E (pt) 2009-06-16
EP1626897A1 (de) 2006-02-22
CN101016082B (zh) 2010-12-08
TW200734244A (en) 2007-09-16
JP4597146B2 (ja) 2010-12-15
SI1626897T1 (sl) 2009-08-31
DE502004009484D1 (de) 2009-06-25
DE202004021495U1 (de) 2008-06-05
WO2005113332A1 (de) 2005-12-01
EP1857358B1 (de) 2016-09-07
HK1083813A1 (en) 2006-07-14
CN101016082A (zh) 2007-08-15
EP2025593A2 (de) 2009-02-18
TW200535049A (en) 2005-11-01
CN1689912A (zh) 2005-11-02
JP4410656B2 (ja) 2010-02-03
DE202004021222U1 (de) 2007-04-26
DE202004006453U1 (de) 2004-11-11
JP2005306355A (ja) 2005-11-04
DK1626897T3 (da) 2009-07-13
PL1626897T3 (pl) 2009-10-30
DE202004021604U1 (de) 2009-05-28

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