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EP1578662B1 - Arrangement in a propulsion system - Google Patents

Arrangement in a propulsion system
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Publication number
EP1578662B1
EP1578662B1EP03767842AEP03767842AEP1578662B1EP 1578662 B1EP1578662 B1EP 1578662B1EP 03767842 AEP03767842 AEP 03767842AEP 03767842 AEP03767842 AEP 03767842AEP 1578662 B1EP1578662 B1EP 1578662B1
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EP
European Patent Office
Prior art keywords
propeller
propulsion system
cap
counter rotating
aft
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
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EP03767842A
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German (de)
French (fr)
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EP1578662A1 (en
Inventor
Tomi Veikonheimo
Vladimir Alexandrovich Boushkovskiy
Alexander Vladimirovich Pustoshny
Sergey Viacheslavovich Kaprantzev
Irina Gennadievna Frolova
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ABB Oy
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ABB Oy
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Abstract

In a counter rotating propulsion system (CRP), whereby the aft propeller ( 22 ) and the forward propeller ( 6 ) have opposite directions of rotating and the aft and forward propellers are arranged against each other, the forward propeller is provided with a hubcap ( 30 ), wherein at least two equally distributed flow plates ( 28 ) are arranged on the cap ( 30 ) and the flow plates ( 28 ) are radially projecting from the cap ( 30 ).

Description

  • This application relates to a counter rotating propulsion system (CRP).
  • The propulsion system is normally located in after part of the marine vessel. The propellers are equipped with hubcap, which is normally covering the propeller fastening bolt. The circulation of water around each forward propeller blade forms a vortex near the hub before they joint to one hub vortex. This hub vortex cavitation is know to be very harmful to the propulsion unit or the rudder behind the main propeller. The hub vortex is itself erosive but it can also induce other harmful forms of cavitation on construction such as propulsion unit or after propeller blade.
  • Especially in the CRP propulsion concept whereby another propeller is arranged close to the main propeller this may cause extensive damages. The steering of the propulsion unit is not fully competent because of erosive hub vortices. This will shorten the maintenance interval of the propulsion system and thereby the overall costs increase.
  • Conventional way to avoid hub vortex cavitation is application of blunt cap after the propeller, which destroy hub vortex due to vast separation after hubcap. But in subject case of counter rotating propeller such way is unacceptable because separation provoke cavitation on the blades of aft propeller especially when aft thruster operates in steering mode so that thruster is turned by some angle, and so fore and aft propellers are not co-axial and blades of aft propeller during its rotation cross the separation zone.
  • PublicationWO 01 54971 A1 (closest prior art) discloses a CRP arrangement where two propellers are propellers are arranged on the same axial line. The aft propeller and the forward propeller have opposite directions of rotating and the aft and forward propellers are arranged opposite to each other. The aft propeller ofWO 01 54971 A1 is installed in the pod that can be turned around a vertical axis to steer the ship.
  • PublicationEP 0255136 A1 discloses a propulsion system where the cap of the propeller has fins in order to decrease the cavitations of a single propeller. The aim ofEP 0255136 is to increase the efficiency of the propulsion arrangement with single propeller.
  • PublicationEP 0758606 A1 discloses another single propeller system having fins on the cap of the propeller. PublicationDE 606119 C discloses a single propeller with a cylinder or a round body whereto fins are attached.
  • Accordingly, it is an object of the present invention to provide a new arrangement, which solves the problems caused by the vortices. This object is achieved in connection of the CRP system by the features as identified in the claim 1. Further advantageous modifications of the invention are characterized by the features of the subclaims.
  • This invention will reduce or eliminate the above mentioned problem in CRP propulsion concept and thus protect the after propeller and entire propulsion unit itself from damage. The invention will increase the capability to steer the propulsion unit behind forward propeller without danger of erosive hub vortex cavitation and without dangerous cavitation on the blades after hub of forward cavitation. This will lead to longer lifetime and reduce repairing costs of the propulsion unit.
  • The invention is based to an idea to break the flow of the vortex caused by the blades of the forward propeller. The hub cab of the propeller, in detail the external appearance of the hubcap is formed so that it consists of at least two, equally distributed flow plates projecting from the outer surface of the hubcap. The number of the flow plates is in practice not higher than eight while four flow plates gives the most efficient result.
  • On the other hand the cap itself should be well-streamlined, with relation of cap diameter and cap length not more than 2. It provides the absence of developed separation after hub cap with plates and so make it possible to eliminate blade cavitation in separation zone after fore hub when thruster is not co-axial with fore propeller.
  • The absence of the hub vortex allows the safe operation of after propeller and steerable propulsion unit. The invention is advantageous to implement, as it requires no other modifications to the structure or to operation of the propulsion system or its peripheral devices. Further as the invention mainly is realized with a special forming of a separate component, the invention is adaptable also to the propulsion devices in use.
  • According to one feature of the invention there is installed a well-streamlined hubcap of the fore propeller between two propellers in order to avoid separation after the fore hub.
  • According to another feature of the invention the hubcap of the fore propeller will have the flow plates which are straight and similar to each other. This gives an optimal effect and a balanced structure.
  • According to another feature of the invention the number of the flow plates is independent of the number of the blades of the forward propeller and the position of the flow plates is independent of the position of the blades of the forward propeller. This feature facilitates the planning and installation of the hubcap, as there is no need to align the flow plates with the blades of the propeller. The same structure of the hubcap can be used in the different propeller configurations.
  • It is another further feature of the invention that the diameter of the tip edges of the plates is in the range of 0,4 -2 times the maximum hub diameter. Within this range the efficiency of the invented appliance is especially advantageous.
  • The flow plates are fastened to the hub cab either by fixed to the cap by welding or by with bolts. The size and shape of the flow plates is easy to change and vary if necessary depending of the respective requirements. If the flow plates are used with the vessels in use, this possibility might be desirable. Alternatively the hubcap is moulded as one piece with flow plates whereby the hubcap can be handled as an integrated piece.
  • According to further advantageous feature the aft propeller is turnable and the aft propeller is used to propel and steer the vessel.
  • The details of one preferred embodiment as well as advantages and further features of the invention will be apparent from the following specification and from the drawings. In the drawings:
    • Figure 1 is a schematic view of a CRP arrangement according to the invention,
    • Figure 2a is side view of a hub cap according to the invention and
    • Figure 2b is front view of a hub cab ofFigure 2a.
  • Figure 1 shows apropulsion arrangement 2 which is realized with counter rotating propellers (CRP), which is placed under thehull 4 of the vessel. The main propulsion propeller, so calledforward propeller 6 is arranged onto themain driving axis 8, which is supported via bearings to thehull 4 of the ship. Theforward propeller 6 is driven e.g. by the drive unit, like a diesel engine, directly or via a electric drive that is supplied by a diesel-generator unit by means of a frequency converter which is well-known in the art. The drive unit and the bearing and other features of the power transmission is utilizing conventional technique well-known in the art and there in no need to explain in detail in order to understand the invention. Theforward propeller 6 comprises ahub 10 arranged to thedriving axis 8 andpropeller blades 12 fixed to thehub 10. The number of blades, the inclination of the blades and the size of the blades will be defined when dimensioning the propulsion system of ship and they may vary case by case. The inclination of the blades may also be adjustable.
  • Thehull 4 of the ship is designed so that the bottom of the hull curves over theforward propeller 8 and the bottom extends at higher level after the forward propeller. Thus thebottom 14 at the rearmost portion of the ship is higher than thebottom 16 of the ship in front of the forward propeller. Under thebottom 14 there is arranged aturnable steering device 18, which consists of an azimuth propeller unit, like an AZIPOD® unit, which steers and propels the vessel. Thesteering device 18 comprises ashaft 20, which is pillowed to be turnable 360 degrees around its vertical axis. Astreamlined casing 21, which covers the driving motor of thesteering propeller 22, is attached under theshaft 20. Thesteering propeller 22 is driven by thedriving axis 24, which is positioned on the same level as theaxis 8 of the forward propeller.
  • According to the CRP concept the well-streamlined hub cap 30 of theforward propeller 6 and thehub cap 26 of thesteering propeller 22 are against each other and theforward propeller 6 and thesteering propeller 22 are rotating in the opposite direction when the ship is moving forwards. When turning the direction of the ship thesteering device 18 is turned around the vertical axis of theshaft 20 in order to effect the desired steering action.
  • The rotating planes of the forward and steering propellers are farther from each other than the double diameter of the forward propeller when the propellers are against each other. Thehub cap 30 of theforward propeller 6 and thehub cap 26 of the steering propeller are thus positioned much closer. The vortex and the stress caused by it effects thus heavily to the hubcap of the forward propeller and also to the steering propeller. According to the teaching of the present invention the hub vortex cavitation and the aft propeller blade cavitation with its harmful effects are minimized by arranging a well-streamlined hub 30 after the forward propeller andflow plates 28 onto thehubcap 30.
  • According to a favourable embodiment of the invention fourflow plates 28 are mounted symmetrically or with equal distance to each flow plate on the outer surface of thehubcap 30 as shown in thefigures 2a and 2b. Thefigure 2a is the side view and thefigure 2b is the front view when seen from the rear of the vessel. The hubcap has length L and diameter D, whereby the ratio D/L is not higher than 2. The flow plates are straight plates that are welded or fixed by bolts to the surface of themain propeller hubcap 2. Theflow plates 2 can also be cast together with the whole propeller hubcap. The flow plate has been installed on the whole length of the cap surface and the flow plates link up to each other outside the cap surface extending a little over the top edge of the cap. In this example the height of the flow plate does not exceed the radial dimensions of the cap. Thus the flow plate does not extend over the diameter of the hubcap. The flow plates are projected in the radial direction from the surface of the hubcap and they are installed in the direction of the propeller axis with no inclination. It has been shown that the tip edges of the flow plates may vary in the range of 0,4 to 2 times the maximum hub diameter D. Accordingly this range corresponds about 0,12 to 0,4 times the diameter of the propeller.
  • The number of the flow plates is not tied to the number of the propeller blades and it may vary from two to eight while four flow plates has been found to be advantageous. Neither the positioning of the flow plates is not bound to the position of the propeller blades but they can coincide or be aside.
  • The invention has been above described using its one modification as an example. The invention may have a lot of different embodiments, the scope of the invention being defined in the claims.

Claims (9)

  1. A counter rotating propulsion system (CRP), which propulsion system comprises an aft propeller (22) installed on a rotatable thruster (18) and a forward propeller (6) installed on a shaft (8) or on a thruster, which propellers are arranged on the essentially same axial line, whereby the aft propeller (22) and the forward propeller (6) have opposite directions of rotating and the aft and forward propellers are arranged against each other, the propellers having a hub with a cap,characterized in that at least two flow plates (28) are arranged on the cap (30) of the forward propeller (6) radially projecting from the cap (30) and that the flow plates (28) are equally distributed on the cap (30).
  2. A counter rotating propulsion system according to claim 1,characterized in that the forward hubcap (30) have diameter to length ratio not higher than 2.
  3. A counter rotating propulsion system according to claim 1 or 2,characterized in that the flow plates (28) are straight and similar to each other.
  4. A counter rotating propulsion system according to any of the claims 1 to 3,characterized in that the number of the flow plates (28) is independent of the number of the blades (12) of the forward propeller (6) and the position of the flow plates (28) is independent of the position of the blades of the forward propeller.
  5. A counter rotating propulsion system according to any of the claims 1 to 4,characterized in that the diameter of the tip edges of the plates (28) are in the range of 0,4 -2 times the maximum hub diameter.
  6. A counter rotating propulsion system according to any of the claims 1 to 5,characterized in that the plates (28) are integrated to the cap (30).
  7. A counter rotating propulsion system according to any of the claims 1 to 6,characterized in that the plates (28) are fixed to the cap (30) by welding or by bolts.
  8. A counter rotating propulsion system according to any of the claims 1 to 7,characterized in that the aft propeller (22) is turnable and the aft propeller (22) is used to propel and to steer the vessel.
  9. A counter rotating propulsion system according to any of the claims 1 to 8,characterized in that the aft propeller (22) being after the forward propeller (6) has a streamlined cap (26).
EP03767842A2002-12-202003-12-19Arrangement in a propulsion systemExpired - LifetimeEP1578662B1 (en)

Applications Claiming Priority (3)

Application NumberPriority DateFiling DateTitle
FI20022265AFI115210B (en)2002-12-202002-12-20 Device in a propulsion system
FI200222652002-12-20
PCT/FI2003/000978WO2004056654A1 (en)2002-12-202003-12-19Arrangement in a propulsion system

Publications (2)

Publication NumberPublication Date
EP1578662A1 EP1578662A1 (en)2005-09-28
EP1578662B1true EP1578662B1 (en)2010-11-17

Family

ID=8565138

Family Applications (1)

Application NumberTitlePriority DateFiling Date
EP03767842AExpired - LifetimeEP1578662B1 (en)2002-12-202003-12-19Arrangement in a propulsion system

Country Status (15)

CountryLink
US (1)US20060172632A1 (en)
EP (1)EP1578662B1 (en)
JP (1)JP4005601B2 (en)
KR (1)KR101127484B1 (en)
CN (1)CN1729123A (en)
AT (1)ATE488427T1 (en)
AU (1)AU2003292278B2 (en)
CA (1)CA2509401C (en)
DE (1)DE60335026D1 (en)
DK (1)DK1578662T3 (en)
ES (1)ES2356628T3 (en)
FI (1)FI115210B (en)
NO (1)NO334694B1 (en)
RU (1)RU2304545C2 (en)
WO (1)WO2004056654A1 (en)

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JP2008149746A (en)*2006-12-142008-07-03Nakashima Propeller Co LtdContra-rotating propeller device for ship
CN103097238B (en)*2010-07-122016-09-21罗尔斯-罗伊斯股份公司 marine vessel with propulsion unit
FI123164B (en)2010-12-212012-11-30Waertsilae Finland Oy WATER VESSEL
JP5972711B2 (en)*2012-08-222016-08-17三菱重工業株式会社 Counter-rotating propeller propulsion type ship
EP2897858A4 (en)*2012-09-242016-07-06Rolls Royce AbCounter rotating pod with flap
CN105270588A (en)*2015-10-302016-01-27佛山市神风航空科技有限公司Symmetric double-stage propelling device for ship
CN105523160A (en)*2016-01-052016-04-27上海船舶研究设计院Hub connecting structure of forward propeller and rear propeller of contrarotating propeller
WO2017158203A1 (en)2016-03-182017-09-21Rolls-Royce Marine AsLifeboat ramp
CN112061361B (en)*2020-10-102022-05-27宁波海伯集团有限公司Marine propeller

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DE606119C (en)1933-11-121934-11-24Nicholas Wladimir Akimoff Device to increase the efficiency of a screw propeller
CA1341138C (en)*1986-06-302000-11-14Minnesota Mining And Manufacturing CompanyFluorine-containing chiral smectic liquid crystals
CA1289821C (en)*1986-07-311991-10-01Michihito OguraScrew propeller boss cap with fins
JPS641690A (en)*1987-06-241989-01-06Ishikawajima Harima Heavy Ind Co LtdPropeller idling device
EP0758606A1 (en)*1995-08-161997-02-19Schottel-Werft Josef Becker GmbH & Co KG.Hub cap for ship propellers
RU2115589C1 (en)*1996-06-251998-07-20Государственный научно-исследовательский и проектно-конструкторский институт по развитию и эксплуатации флота "Гипрорыбфлот"Shipboard propulsion engine plant, type swinging propeller
US6899576B2 (en)*1997-11-072005-05-31Schottel Gmbh & Co. KgTwin-propeller drive for watercraft
JPH11222188A (en)1998-02-091999-08-17Hitachi Zosen Corp Chip vortex energy recovery system for ships
FI110595B (en)*2000-01-282003-02-28Abb Oy Arrangements in vessels, procedure for utilization of space in vessels and arrangements in installation of propulsion unit
US6280284B1 (en)*2000-03-172001-08-28Carl WinefordnerToy submarine with counter rotating propellers
FI116129B (en)*2003-04-072005-09-30Waertsilae Finland Oy Watercraft Propulsion Unit
FI20030556A0 (en)*2003-04-112003-04-11Abb Oy Method and equipment for steering the ship

Also Published As

Publication numberPublication date
RU2304545C2 (en)2007-08-20
KR20050084403A (en)2005-08-26
DE60335026D1 (en)2010-12-30
DK1578662T3 (en)2011-02-21
FI20022265A7 (en)2004-06-21
WO2004056654A1 (en)2004-07-08
RU2005122954A (en)2006-01-20
CN1729123A (en)2006-02-01
KR101127484B1 (en)2012-03-23
JP4005601B2 (en)2007-11-07
ATE488427T1 (en)2010-12-15
NO20053510L (en)2005-07-18
EP1578662A1 (en)2005-09-28
ES2356628T3 (en)2011-04-11
AU2003292278B2 (en)2008-10-09
NO334694B1 (en)2014-05-12
JP2006510532A (en)2006-03-30
AU2003292278A1 (en)2004-07-14
CA2509401C (en)2011-07-19
FI115210B (en)2005-03-31
US20060172632A1 (en)2006-08-03
CA2509401A1 (en)2004-07-08
FI20022265A0 (en)2002-12-20

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