EP1921005B1 - Gouvernail pour bateaux - Google Patents

Gouvernail pour bateaux Download PDF

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Publication number
EP1921005B1
EP1921005B1 EP07005019A EP07005019A EP1921005B1 EP 1921005 B1 EP1921005 B1 EP 1921005B1 EP 07005019 A EP07005019 A EP 07005019A EP 07005019 A EP07005019 A EP 07005019A EP 1921005 B1 EP1921005 B1 EP 1921005B1
Authority
EP
European Patent Office
Prior art keywords
flow body
rudder
rudder blade
predetermined breaking
propeller
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
Application number
EP07005019A
Other languages
German (de)
English (en)
Other versions
EP1921005A1 (fr
Inventor
Mathias Kluge
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
Application filed by Becker Marine Systems GmbH and Co KG filed Critical Becker Marine Systems GmbH and Co KG
Priority to PL07005019T priority Critical patent/PL1921005T3/pl
Publication of EP1921005A1 publication Critical patent/EP1921005A1/fr
Application granted granted Critical
Publication of EP1921005B1 publication Critical patent/EP1921005B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • B63H25/42—Steering or dynamic anchoring by propulsive elements; Steering or dynamic anchoring by propellers used therefor only; Steering or dynamic anchoring by rudders carrying propellers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B3/00—Hulls characterised by their structure or component parts
    • B63B3/14—Hull parts
    • B63B3/40—Stern posts; Stern frames
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H1/00—Propulsive elements directly acting on water
    • B63H1/02—Propulsive elements directly acting on water of rotary type
    • B63H1/12—Propulsive elements directly acting on water of rotary type with rotation axis substantially in propulsive direction
    • B63H1/14—Propellers
    • B63H1/20—Hubs; Blade connections

Definitions

  • the invention relates to a rudder for ships according to the preamble of claim 1.
  • the so-called Costa bulb or propulsion bulb serves to form, as an extension of the propeller axis in the region of the rudder blade, a curvature which is pear-shaped or zeppelin-shaped and constitutes a flow body.
  • This flow body has the purpose that the overall profile of the hub is extended so far that only a small turbulence of the outflowing water is formed.
  • Such a Costa pear is for example through the pamphlets DE 198 44 353 A1 .
  • the effect of the Costa bulb is based on its bulbous shape, with which it stands out from the rudder or rudder blade, so that there is a favorable flow guidance.
  • the Costa bulb is thus laterally opposite the rudder blade and is in the event of a shock or impact or pressure in the immediate danger area before the actual rudder blade would be at risk.
  • the object of the invention is to provide a rudder blade for ships, which is less prone to damage or destruction despite favorable flow control against external influences due to shock, impact or pressure and the flow body destroyed by the action of pressure or impact independently.
  • the flow body, the rudder blade viewed in the vertical direction, divides into two areas (A, B), wherein the two areas are identical or not identical in profile.
  • the longitudinal center lines of the areas of the rudder blade do not coincide with the center lines of the flow body and form an angle ⁇ .
  • the flow body has predetermined breaking points, which lead to the destruction of the flow body with increased force, impact, shock or pressure. It is also advantageous if the predetermined breaking points are designed as predetermined breaking lines. It is also expedient if the predetermined breaking lines are oriented in the longitudinal and / or transverse direction of the flow body. But it is also advantageous if the predetermined breaking lines are distributed like a net over the flow body.
  • the predetermined breaking points or predetermined breaking lines are designed as material weakenings, material reductions and / or score lines.
  • the flow body consists of metal or a non-metallic material or a metal-non-metal mixture.
  • the flow body consists of a carbon-fiber composite material.
  • the material comprises embedded carbon fibers, graphite fibers and / or glass fibers.
  • the flow body consists of plastic or plastics.
  • the flow body consists of POM plastic, such as polyoxymethylene, polyformaldehyde or polyacetates.
  • the flow body consists of two individual shell-shaped to the flow body complementary longitudinal bodies in the region of their longitudinal edges on predetermined breaking lines on the outer wall surfaces of the rudder blade are held, wherein the propeller facing edge regions of the two shell-shaped longitudinal body are connected via predetermined breaking lines with a spherical cap-like component which is fixed or detachably connected to the rudder blade.
  • Fig. 1 shows the tail 11 of a ship 10 with a drive propeller 12 and a rudder 13, the rudder blade 15 is provided with a pear-shaped or zeppelin-shaped flow body 20, which is preferably designed as a hollow body and which may be integrated into the rudder blade 15 as well as two or a plurality of components 21, 22 may be, which are attached to the outer wall surfaces 15 a, 15 b of the rudder blade 15.
  • the flow body 20 may also be formed as a solid body.
  • a curvature is formed in the region of the rudder blade 1, which forms the flow body 20, also called propulsion bulb or Costa bulb.
  • the flow body 20 is designed so that it is itself destructive to pressure, impact or impact.
  • the wall 25 of the flow body 20 consists of individual wall sections 30, which are connected to one another via predetermined breaking lines 40 in the form of material weakenings or score lines ( Fig. 6 ).
  • the predetermined breaking lines are formed running in the longitudinal direction and / or transversely to the longitudinal direction of the flow body 20 in the wall 25 of the flow body 20, wherein the Rupture lines 40 may also be irregular.
  • the predetermined breaking lines 40 can also be distributed in a network over the flow body 20.
  • frangible lines 40 are formed and mounted so that in the outer wall surface of the flow body 20 no bumps, depressions, grooves o. The like. Emerge and so the smooth outer wall surface is maintained.
  • the flow body 20 itself is destroyed or self-dissolves in the event of impact, impact or pressure. Thus, no excessive force is transmitted to the rudder blade itself, so that leading to a significant damage or destruction impairment of the rudder blade can be avoided.
  • the Fig. 2 shows the view of a rudder blade 15 with a flow body 20, which is composed of three separate parts 50, 51, 55.
  • the parts 50, 51 form the sides of the flow body 20 on the sides of the rudder blade 15 and the part 55 forms the front, ie the propeller 12 facing substantially substantially hemispherical conclusion.
  • the arrows X, X1, X2 indicate that the parts 50, 51, 55 are disassembled from the rudder blade 15 in these directions.
  • the parts 50, 51, 55 of the flow body 20 are designed shell-shaped and preferably do not form solid bodies, but in the assembled state only a hollow body which is attached to the rudder blade 15.
  • the flow body 20 consists of two individual shell-shaped, complementary to the flow body longitudinal bodies 50, 51 which are held in the region of their longitudinal edges 50a, 51a via predetermined breaking lines 40 on the outer wall surfaces 15a, 15b of the rudder blade 15, wherein the propeller 12 facing edge portions 50a , 51 b of the two bowl-shaped Longitudinal body 50, 51 are connected via predetermined breaking lines 40 with a spherical cap-like component which is fixedly or detachably connected to the rudder blade 15 ( Fig. 2 and 3 ).
  • the rudder blade 15 is not a homogeneous component, but is formed from an upper portion A and a lower portion B.
  • the upper portion A has at least on its front side a curvature or orientation which is more bent or oriented to the left and the lower part B has at least one curvature or orientation which is more bent or oriented to the right.
  • this difference can be recognized by the fact that the two front areas are formed like tongues which do not coincide with each other, but are approximately Y-shaped apart.
  • the longitudinal center lines LM1 of the two areas A and B are not congruent and parallel, but have an angle ⁇ between each other. Also, the longitudinal center lines LM1 of the regions A and B are not located on the center line ML of the flow body 20.
  • the Fig. 3 shows a view of the rudder blade 15 with flow body 20 with the parts 50, 51 and 55.
  • the areas A and B may be different, so that the longitudinal center lines LM1 pierce the leading edge at LM1 and thus outside the Center line ML of the flow body 20 are.
  • the upper region A may be identical to the lower region B, so that either the deviation of the longitudinal center line LM1 to the center line ML of the flow body 20 is equal and at an angle of zero or equal to zero can.
  • FIGS. 8 and 9 each show a view of the rudder blade 15 from below or from above. Clearly visible is the angle ⁇ between each the longitudinal center line LM1 of the rudder blade 15 and the center line ML of the flow body 20.
  • Fig. 4 shows a rudder blade 15 with a flow body 20 in a side view from the left rear.
  • the areas A and B can be seen here. In the rear area, the areas A and B are identical, whereas they are designed differently in the front area (see also Fig. 2 ).
  • Fig. 5 shows the rudder blade 15 in a view from behind and the Fig. 7 a view from the front. In each case, the flow body 20 can be clearly seen.
  • Fig. 6 shows the rudder blade 15 according to the invention with the flow body 20, wherein the flow body for better own destruction in a force, shock or pressure has predetermined breaking points.
  • the predetermined breaking points are advantageously provided as predetermined breaking lines 40, which are distributed over the surface of the flow body. These are advantageously oriented in the longitudinal and / or transverse direction of the flow body 20. It is particularly advantageous if the predetermined breaking points are formed by material reduction or by notching, ie by score lines.
  • the predetermined breaking lines 40 are distributed like a net over the surface of the flow body 20.
  • the rudder blade 15 has a cross-sectional area 16, the longitudinal center line LM1 is offset at an angle ⁇ to the center line ML of the flow body 20, so that the nose bar 70 of the rudder blade 15 facing the drive propeller 12 comes to lie outside the center line ML of the flow body 20.
  • the flow body 20 is advantageously made of metal. In another embodiment, however, it may also be formed from a non-metallic material, such as a carbon-fiber composite, preferably with embedded carbon fibers, graphite fibers and / or glass fibers. Also, a metal-non-metal mixture may be predetermined.
  • a non-metallic material such as a carbon-fiber composite, preferably with embedded carbon fibers, graphite fibers and / or glass fibers.
  • a metal-non-metal mixture may be predetermined.
  • the flow body 20 may also be made of plastic or plastics.
  • POM plastics can be used, such as polyoxymethylene, polyformaldehyde or polyacetates. These substances typically have a high lubricity, which is advantageous for the friction in the water.
  • the rudder blade 15 according to the invention is used with the flow body 20 in Vollschweberudern.
  • the flow body 20 is integrated in the rudder blade 15 or the flow body 20 is attached, for example, in half on both sides of the rudder blade 15.
  • the propeller 12 facing nose strips 70, 71 of the two superimposed rudder blade areas A and B offset from each other such that the nose strip 70 of the upper rudder blade area A to port BB and the nose bar 71 are offset to starboard SB, wherein the reverse offset is possible.
  • the outer wall surfaces 15a, 15b of the rudder blade 15 are merged in an end bar 75 facing away from the propeller 12 (twisted rudder).
  • the nose strip 70, 71 of the two rudder blade portions A and B are offset from each other, so that the leading edge of the 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 Port are offset, two each to each other obtained mirror-inverted cross-sectional profiles of the two rudder blade areas.

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  • Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Ocean & Marine Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Toys (AREA)
  • Physical Or Chemical Processes And Apparatus (AREA)
  • Wind Motors (AREA)
  • Earth Drilling (AREA)
  • Steroid Compounds (AREA)
  • Laminated Bodies (AREA)
  • Medicines Containing Material From Animals Or Micro-Organisms (AREA)
  • Farming Of Fish And Shellfish (AREA)
  • Revetment (AREA)
  • Ladders (AREA)

Claims (12)

  1. Gouvernail pour navires qui comprend une pale de gouvernail (15) à laquelle correspond une hélice (12) placée sur un axe d'hélice qui peut être commandé, un corps d'écoulement (20) étant placé sur la pale de gouvernail (15), corps qui est configuré piriforme ou en forme de Zeppelin et qui est placé dans la prolongation de l'axe d'hélice dans la zone de la pale de gouvernail (15),
    caractérisé en ce
    que le corps d'écoulement (20) est configuré auto-destructible ou auto-dissolvable pour une action accrue de force, de coup, de choc ou de pression.
  2. Gouvernail selon la revendication 1,
    caractérisé en ce
    que le corps d'écoulement (20) sépare la pale de gouvernail (15) en deux zones (A et B), ceci étant considéré dans le sens de la hauteur, les deux zones (A et B) étant de profil identique ou non identique.
  3. Gouvernail selon la revendication 1 ou 2,
    caractérisé en ce
    que les lignes centrales longitudinales (LM1) des zones (A et B) de la pale de gouvernail (15) ne coïncident pas avec les lignes centrales (ML) du corps d'écoulement (20) ou divergent l'une de l'autre et forment un angle α.
  4. Gouvernail selon la revendication 3,
    caractérisé en ce
    que l'angle α entre la ligne centrale longitudinale (LM1) d'une zone (A, B) de la pale de gouvernail (15) et la ligne centrale (ML) du corps d'écoulement (20) pour les deux zones (A, B) est différent pour les deux zones (A, B).
  5. Gouvernail selon l'une des revendications 1 à 4,
    caractérisé en
    ce que la paroi (25) du corps d'écoulement (20) présente, en configurant différentes sections de paroi (30), des lignes destinées à la rupture ou des points destinés à la rupture (40) qui provoquent, pour une action accrue de force, de coup, de choc ou de pression, la destruction du corps d'écoulement (20) et qui sont configurées comme des affaiblissements de matière, des réductions de matière, des lignes entaillées ou des perforations.
  6. Gouvernail selon l'une des revendications 1 à 5,
    caractérisé en ce
    que les lignes destinées à la rupture (40) sont configurées dans le sens longitudinal et/ou transversalement par rapport au sens longitudinal du corps d'écoulement (20) dans la paroi du corps d'écoulement (20), les lignes destinées à la rupture (40) pouvant également être irrégulières.
  7. Gouvernail selon l'une des revendications 1 à 6,
    caractérisé en ce
    que les lignes destinées à la rupture (40) sont distribuées à la manière d'un filet sur le corps d'écoulement (20).
  8. Gouvernail selon l'une des revendications 1 à 7,
    caractérisé en ce
    que le corps d'écoulement (20) est constitué par deux différents corps longitudinaux (50, 51) en forme de coque, qui se complètent en un corps d'écoulement, qui sont maintenus sur les surfaces de paroi extérieure (15a, 15b) de la pale de gouvernail (15) dans la zone de leurs bords longitudinaux (50a, 51 a) par des lignes destinées à la rupture (40), les zones marginales (50b, 51 b) tournées vers l'hélice (12) des deux corps longitudinaux en forme de coque (50, 51) étant reliées par des lignes destinées à la rupture (40) à un composant de type calotte sphérique (55) qui est relié de manière fixe ou amovible à la pale de gouvernail (15).
  9. Gouvernail selon l'une des revendications 1 à 8,
    caractérisé en ce
    que la pale du gouvernail (15) présente une surface de section (16) dont la ligne centrale longitudinale (LM1) est décalée dans un angle α par rapport à la ligne centrale (ML) du corps d'écoulement (20) si bien que le bord d'attaque (70 ; 71) de la pale de gouvernail (15) qui est tourné vers l'hélice de commande (12) vient se poser en dehors de la ligne centrale (ML) du corps d'écoulement (20).
  10. Gouvernail selon l'une des revendications 1 à 9,
    caractérisé en ce
    que le corps d'écoulement (20) et ses composants (50, 51) sont constitués en matériaux métalliques ou non métalliques comme les matériaux composites en fibres de carbone ou les matériaux composites en fibres avec des fibres de graphite ou des fibres de verre incorporées, en un mélange de métal et de non métal, en une matière synthétique.
  11. Gouvernail selon l'une des revendications 1 à 10,
    caractérisé en ce
    que le corps d'écoulement (20) est en matière POM comme le polyoxyméthylène, le polyformaldéhyde ou les polyacétates.
  12. Gouvernail selon l'une des revendications 1 à 11,
    caractérisé en ce
    que les bords d'attaque (70, 71) tournés vers l'hélice (12) des deux zones de pale de gouvernail (A et B) superposées sont décalés l'un par rapport à l'autre de telle manière que le bord d'attaque (70) de la zone supérieure de pale de gouvernail (A) est décalé vers bâbord (BB) et le bord d'attaque (71) vers tribord (SB) ou même vice-versa, les surfaces de paroi extérieure (15a, 15b) de la pale de gouvernail (15) étant réunies en un bord d'attaque (75) opposé à l'hélice (12).
EP07005019A 2006-11-13 2007-03-12 Gouvernail pour bateaux Active EP1921005B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL07005019T PL1921005T3 (pl) 2006-11-13 2007-03-12 Ster do statków

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE202006017370U DE202006017370U1 (de) 2006-11-13 2006-11-13 Ruder für Schiffe

Publications (2)

Publication Number Publication Date
EP1921005A1 EP1921005A1 (fr) 2008-05-14
EP1921005B1 true EP1921005B1 (fr) 2008-11-12

Family

ID=39154974

Family Applications (1)

Application Number Title Priority Date Filing Date
EP07005019A Active EP1921005B1 (fr) 2006-11-13 2007-03-12 Gouvernail pour bateaux

Country Status (16)

Country Link
US (1) US20080110386A1 (fr)
EP (1) EP1921005B1 (fr)
JP (1) JP4571658B2 (fr)
KR (1) KR100895379B1 (fr)
CN (1) CN101181930B (fr)
AT (1) ATE414012T1 (fr)
DE (2) DE202006017370U1 (fr)
DK (1) DK1921005T3 (fr)
ES (1) ES2313690T3 (fr)
HK (1) HK1120475A1 (fr)
HR (1) HRP20080636T3 (fr)
NO (1) NO337821B1 (fr)
PL (1) PL1921005T3 (fr)
PT (1) PT1921005E (fr)
SG (1) SG143109A1 (fr)
TW (1) TWI331975B (fr)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
ATE523423T1 (de) * 2008-09-12 2011-09-15 Waertsilae Netherlands B V Antriebs- und steueranordnung
ES2548060T3 (es) * 2008-09-12 2015-10-13 Wärtsilä Netherlands B.V. Disposición de propulsión y dirección
KR100901391B1 (ko) * 2009-03-04 2009-06-05 대우조선해양 주식회사 전연 비대칭 유선형 단면과 볼록한 띠형 덮개를 갖는 선박용 방향타
DE102009033163A1 (de) * 2009-04-22 2010-11-04 Becker Marine Systems Gmbh & Co. Kg Ruderflosse
JP2012111422A (ja) * 2010-11-26 2012-06-14 Mitsubishi Heavy Ind Ltd アジマス推進器およびこれを備えた船舶
JP5689328B2 (ja) * 2011-02-03 2015-03-25 住友重機械マリンエンジニアリング株式会社 ラダーバルブ付き舵、船舶、及びラダーバルブ、並びにラダーバルブ付き舵の製造方法
KR101346167B1 (ko) * 2011-04-14 2013-12-31 삼성중공업 주식회사 선박용 벌브 러더
KR101291119B1 (ko) * 2011-05-26 2013-08-01 삼성중공업 주식회사 선박 추진장치 및 이를 갖춘 선박
JP2013107522A (ja) * 2011-11-22 2013-06-06 Nippon Yusen Kk ラダーバルブおよび船舶用舵
KR101323797B1 (ko) * 2011-12-27 2013-10-31 삼성중공업 주식회사 선박
EP2626290B1 (fr) * 2012-02-09 2015-09-23 ABB Oy Agencement de propulsion pour navire
US9776693B2 (en) * 2013-03-15 2017-10-03 Hadal, Inc. Systems and methods for improving buoyancy in underwater vehicles
JP5950971B2 (ja) * 2014-01-06 2016-07-13 ジャパン・ハムワージ株式会社 船舶用舵
EP3489128A1 (fr) * 2017-11-28 2019-05-29 Becker Marine Systems GmbH Safran de gouvernail à construction modulaire, segment pour un safran de gouvernail ou pour un dispositif d'amélioration de la propulsion et procédé de fabrication d'un safran de gouvernail
KR102054384B1 (ko) * 2018-11-08 2019-12-10 재단법인한국조선해양기자재연구원 러더벌브의 탈부착이 가능한 선박 러더
CN110588927B (zh) * 2019-10-23 2021-02-19 中国科学院沈阳自动化研究所 一种轻质舵板系统
CN114954872B (zh) * 2022-06-29 2024-06-11 中国人民解放军海军工程大学 一种用于水下航行体降噪增效的扭曲舵及其设计方法

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE496398A (fr) *
FR1020502A (fr) * 1950-06-19 1953-02-06 Forges Chantiers Mediterranee Dispositif pour améliorer le rendement de propulsion d'hélices, en particulier pour bateaux
FR1159201A (fr) * 1955-08-13 1958-06-25 Corps directeur en forme de bulbe pour navires
GB800917A (en) * 1956-05-25 1958-09-03 Leo Costa Improvements in propelling and steering ships
CN87209395U (zh) * 1987-06-20 1988-02-17 武汉水运工程学院 装有整流构件的舵
JPH06305487A (ja) * 1993-04-21 1994-11-01 Hitachi Zosen Corp 舵
JPH08164887A (ja) * 1994-12-14 1996-06-25 Mitsubishi Heavy Ind Ltd 衝突エネルギー吸収型バルバス・バウ構造
GB2303832B (en) * 1995-04-11 1998-02-11 Mitsui Shipbuilding Eng Ship
DE19844353A1 (de) * 1998-09-28 2000-03-30 Herbert Schneekluth Steuerruder für Schiffe
JP2000168680A (ja) * 1998-12-01 2000-06-20 Shibata Ind Co Ltd 浮体用緩衝材
JP3899406B2 (ja) * 2003-04-17 2007-03-28 独立行政法人海上技術安全研究所 横曲げ緩衝型船首を有する船舶
DE102004041593B4 (de) * 2004-08-26 2007-02-15 Lindenau Gmbh Schiffswerft Und Maschinenfabrik Doppelhüllenschiff
CN100348459C (zh) * 2005-11-17 2007-11-14 上海交通大学 十字型抗纵摇舵

Also Published As

Publication number Publication date
NO337821B1 (no) 2016-06-27
CN101181930A (zh) 2008-05-21
US20080110386A1 (en) 2008-05-15
SG143109A1 (en) 2008-06-27
KR100895379B1 (ko) 2009-04-29
TW200821219A (en) 2008-05-16
JP4571658B2 (ja) 2010-10-27
TWI331975B (en) 2010-10-21
ES2313690T3 (es) 2009-03-01
DK1921005T3 (da) 2009-02-02
DE202006017370U1 (de) 2008-03-20
DE502007000234D1 (de) 2008-12-24
CN101181930B (zh) 2011-05-25
JP2008120370A (ja) 2008-05-29
EP1921005A1 (fr) 2008-05-14
PL1921005T3 (pl) 2009-04-30
HRP20080636T3 (en) 2009-01-31
HK1120475A1 (en) 2009-04-03
ATE414012T1 (de) 2008-11-15
KR20080043200A (ko) 2008-05-16
PT1921005E (pt) 2008-11-26
NO20071886L (no) 2008-05-14

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