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GB1600994A - Ship propellor ducts - Google Patents

Ship propellor ducts Download PDF

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Publication number
GB1600994A
GB1600994A GB2229677A GB2229677A GB1600994A GB 1600994 A GB1600994 A GB 1600994A GB 2229677 A GB2229677 A GB 2229677A GB 2229677 A GB2229677 A GB 2229677A GB 1600994 A GB1600994 A GB 1600994A
Authority
GB
United Kingdom
Prior art keywords
duct
propeller
sectional
ship
thickness
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
Application number
GB2229677A
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.)
Lips BV
Original Assignee
Lips BV
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 Lips BV filed Critical Lips BV
Priority to GB2229677A priority Critical patent/GB1600994A/en
Publication of GB1600994A publication Critical patent/GB1600994A/en
Expired legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H5/00Arrangements on vessels of propulsion elements directly acting on water
    • B63H5/07Arrangements on vessels of propulsion elements directly acting on water of propellers
    • B63H5/14Arrangements on vessels of propulsion elements directly acting on water of propellers characterised by being mounted in non-rotating ducts or rings, e.g. adjustable for steering purpose

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Ocean & Marine Engineering (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)

Description

(54) IMPROVEMENTS RELATING TO SHIP PROPELLER DUCTS (71) We, LIPS B.V., a Limited Liability Company organised and existing under the laws of the Kingdom of the Netherlands, of Lipsstraat 52, Drunen, The Netherlands, do hereby declare this invention, for which we pray that a patent may be granted to us, and the method by which it is to be performed, to be particularly described in and by the following statement: This invention relates to a duct for a ship's propeller, and in particular to a stationary duct for a marine propeller. Such a duct is sometimes referred to as a propeller nozzle, sometimes referred to as a Kort nozzle.
Basically the invention pertains to the principle of improving or increasing the thrust of a marine propeller by surrounding the rotating propeller with a stationary annular body or duct attached to the hull of a ship, this duct having a foil shape in any axial section. Due to the action of the annular body or duct, the inflow of water to the propeller in general is accelerated. The annular body produces thereby a positive extra thrust force to the ship.
Propulsion devices of this kind are well known and used for ships which have to produce high thrust at low ship speeds, such as tugboats or trawlers. The annular body or duct also offers a means of increasing the efficiency of heavily loaded propellers at moderate ship speeds. However, the advantage of the thrust action of the conventional duct is reduced at increased higher ship speeds. At maximum speed of the ship generally the thrust action of the duct is strongly reduced. Hence the frictional losses of the duct, which are associated with the higher water flow velocities along the duct body, cause a loss in speed of the ship. The present invention aims to provide a propeller duct wherein the disadvantage of the frictional losses are at least partially avoided.
According to the present invention, there is provided a duct for a ship's propeller, the duct being provided with means for attachment at the top and bottom thereof to the hull of the ship, the duct having a foil shape in axial section in any plane intersecting the axis of the duct, which section varies continuously around the circumference of the duct, reaching a first maximum sectional length and/or sectional thickness at the top and a second maximum sectional length and/or sectional thickness at the bottom thereof, the sectional length and/or thickness reducing continuously to a minimum sectional length and/or a minimum sectional thickness in the regions of high water velocities, that is the regions between a horizontal median axial plane and the bottom of the duct.Thus, the shape of the duct is adapted to the wake of the ship in order to reduce frictional losses by presenting the smallest contact area where the water velocity is highest.
As a duct, according to the present invention, exposes a reduced surface in the reglon of high water entrance velocities, the frictional losses at full speed of the ship will be minimised. Another advantage is that a duct according to the invention, having its maximum length at top and bottom, thus offers ample means for strong attachment to the hull of the ship.
A further advantage of the duct, according to the invention, is that the mass distribution favourably influences the natural frequency of the duct, so that resonance vibrations caused by the propeller blades cycling can be avoided.
An embodiment of the invention will be described with reference to the accompanying drawings. Figure 1 of the drawings designates, as an example, the inflow velocity distribution of a ship at the entrance of the propeller duct, the variation of water velocities being caused by the ship's wake.
The circle 1 indicates the inner diameter of the duct. The circle 2 indicates the propeller boss with the axis of rotation 3, while 4 is the sole-piece of the vessel. A multitude of lines 5 show the inflow velocity distribution, the number 1.0 0.95 0.9 .... 0.2 indicating the relation between the maximum (or undisturbed) flow velocity, represented by 1.0 and occurring in the regions at 4 o'clock and 8 o'clock in Figure 1, and the disturbed flow velocity occurring at points around the circumference.
Figure 2 shows a longitudinal section through the propeller duct 6 surrounding a rotating propeller consisting of blades 7 extending radially from a propeller boss 2.
The propeller is mounted for rotation in the stern 8 of a ship. Reference numeral 9 shows the dimensions of the longest axial section of the duct where the duct is attached to the hull by means of a head-box 4a. As can be seen from Figure 1 the water velocities here are low. Reference numeral 10 shows the dimensions of the shortest axial section at a point where, as can be seen from Figure 1, the water velocities are high. In order to reduce the contact area of the duct with the water at this region the sectional thickness may be reduced as well as, or as an alternative to, the reduction in sectional length. Reference numeral 11 indicates the dimensions of the bottom section of the duct and the attachment to the sole-piece 4. The sectional dimensions of the duct are gradually decreased from the top and bottom of the duct to both sides, without discontinuities in length or thickness.
WHAT WE CLAIM IS: 1. A duct for a ship's propeller, the duct being provided with means for attachment at the top and bottom thereof to the hull of the ship, the duct having a foil shape in axial section in any plane intersecting the axis of the duct, which section varies continuously around the circumference reaching a first maximum sectional length and/or sectional thickness at the top and a second maximum sectional length and/or sectional thickness at the bottom thereof the sectional length and/or thickness reducing continuously to a minimum sectional length and/or a minimum sectional thickness in the regions of high water velocities, that is the regions between a horizontal median axis plane and the bottom of the duct.
2. A propeller-duct substantially as described with reference to the accompanying drawings.
**WARNING** end of DESC field may overlap start of CLMS **.

Claims (2)

**WARNING** start of CLMS field may overlap end of DESC **. the duct. The circle 2 indicates the propeller boss with the axis of rotation 3, while 4 is the sole-piece of the vessel. A multitude of lines 5 show the inflow velocity distribution, the number 1.0 0.95 0.9 .... 0.2 indicating the relation between the maximum (or undisturbed) flow velocity, represented by 1.0 and occurring in the regions at 4 o'clock and 8 o'clock in Figure 1, and the disturbed flow velocity occurring at points around the circumference. Figure 2 shows a longitudinal section through the propeller duct 6 surrounding a rotating propeller consisting of blades 7 extending radially from a propeller boss 2. The propeller is mounted for rotation in the stern 8 of a ship. Reference numeral 9 shows the dimensions of the longest axial section of the duct where the duct is attached to the hull by means of a head-box 4a. As can be seen from Figure 1 the water velocities here are low. Reference numeral 10 shows the dimensions of the shortest axial section at a point where, as can be seen from Figure 1, the water velocities are high. In order to reduce the contact area of the duct with the water at this region the sectional thickness may be reduced as well as, or as an alternative to, the reduction in sectional length. Reference numeral 11 indicates the dimensions of the bottom section of the duct and the attachment to the sole-piece 4. The sectional dimensions of the duct are gradually decreased from the top and bottom of the duct to both sides, without discontinuities in length or thickness. WHAT WE CLAIM IS:
1. A duct for a ship's propeller, the duct being provided with means for attachment at the top and bottom thereof to the hull of the ship, the duct having a foil shape in axial section in any plane intersecting the axis of the duct, which section varies continuously around the circumference reaching a first maximum sectional length and/or sectional thickness at the top and a second maximum sectional length and/or sectional thickness at the bottom thereof the sectional length and/or thickness reducing continuously to a minimum sectional length and/or a minimum sectional thickness in the regions of high water velocities, that is the regions between a horizontal median axis plane and the bottom of the duct.
2. A propeller-duct substantially as described with reference to the accompanying drawings.
GB2229677A 1978-05-24 1978-05-24 Ship propellor ducts Expired GB1600994A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2229677A GB1600994A (en) 1978-05-24 1978-05-24 Ship propellor ducts

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2229677A GB1600994A (en) 1978-05-24 1978-05-24 Ship propellor ducts

Publications (1)

Publication Number Publication Date
GB1600994A true GB1600994A (en) 1981-10-21

Family

ID=10177085

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2229677A Expired GB1600994A (en) 1978-05-24 1978-05-24 Ship propellor ducts

Country Status (1)

Country Link
GB (1) GB1600994A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2179312A (en) * 1985-08-19 1987-03-04 Hollming Oy Turnable propeller assembly
US4796836A (en) * 1985-02-28 1989-01-10 Dieter Schatzmayr Lifting engine for VTOL aircrafts
ES2317799A1 (en) * 2008-08-01 2009-04-16 Juan Jose Romero Vazquez Propulsion system with helix and fixed nozzle regarding the helice (Machine-translation by Google Translate, not legally binding)
WO2013169116A1 (en) * 2012-05-08 2013-11-14 Rolls-Royce Marine As Propulsion unit for maritime vessel including a nozzle exhibiting a curved following edge at the outlet of the nozzle

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4796836A (en) * 1985-02-28 1989-01-10 Dieter Schatzmayr Lifting engine for VTOL aircrafts
GB2179312A (en) * 1985-08-19 1987-03-04 Hollming Oy Turnable propeller assembly
ES2317799A1 (en) * 2008-08-01 2009-04-16 Juan Jose Romero Vazquez Propulsion system with helix and fixed nozzle regarding the helice (Machine-translation by Google Translate, not legally binding)
ES2317799B1 (en) * 2008-08-01 2010-03-17 Juan Jose Romero Vazquez PROPULSION SYSTEM WITH HELICE AND FIXED TOWER REGARDING HELICE.
WO2013169116A1 (en) * 2012-05-08 2013-11-14 Rolls-Royce Marine As Propulsion unit for maritime vessel including a nozzle exhibiting a curved following edge at the outlet of the nozzle
US20150093241A1 (en) * 2012-05-08 2015-04-02 Rolls-Royce Marine As Propulsion Unit for Maritime Vessel Including a Nozzle Exhibiting a Curved Following Edge at the Outlet of the Nozzle
NO338816B1 (en) * 2012-05-08 2016-10-24 Rolls Royce Marine As Rotary propulsion unit for maritime vessels comprising a nozzle exhibiting a curved following edge at the outlet of the nozzle
US9821896B2 (en) 2012-05-08 2017-11-21 Rolls-Royce Marine As Propulsion unit for maritime vessel including a nozzle exhibiting a curved following edge at the outlet of the nozzle

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19930524