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EP 0 037 865 B1 |
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EUROPEAN PATENT SPECIFICATION |
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Mention of the grant of the patent: |
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22.08.1984 Bulletin 1984/34 |
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Date of filing: 09.04.1980 |
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International Patent Classification (IPC)3: B63H 25/46 |
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Valve system for controlling the direction of fluid discharge from a nozzle in a thruster
system
Ventilsystem zur Steuerung der Ausströmrichtung eines Fluidums aus einer Düse bei
einem Schubsystem
Système à clapet pour la commande de direction de l'écoulement de fluide à partir
d'une tuyère dans une système de poussage
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| (84) |
Designated Contracting States: |
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DE GB NL |
| (43) |
Date of publication of application: |
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21.10.1981 Bulletin 1981/42 |
| (71) |
Applicants: |
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- Weir Pumps Limited
Glasgow G44 4EX
Scotland (GB)
- Weir Warmtekracht B.V.
NL-3087 AG Rotterdam (NL)
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| (72) |
Inventors: |
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- Karstel, George
NL-3087 AG Rotterdam (NL)
- McConnell, Thomas Alexander
Glasgow, G44 4EX (GB)
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| (74) |
Representative: Arthur, John William et al |
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Cedarwood
Buchanan Castle Estate
Drymen GB-Glasgow G63 0HX GB-Glasgow G63 0HX (GB) |
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| |
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| Note: Within nine months from the publication of the mention of the grant of the European
patent, any person may give notice to the European Patent Office of opposition to
the European patent
granted. Notice of opposition shall be filed in a written reasoned statement. It shall
not be deemed to
have been filed until the opposition fee has been paid. (Art. 99(1) European Patent
Convention).
|
[0001] The present invention relates to a thruster system for use in marine craft including
ducting for location in the hull of the craft, the ducting having a pair of opposed
discharge outlets discharging externally of the hull, means for directing a fluid
flow through the ducting to the discharge outlets and control means for controlling
the flow discharge. More especially the system can be used in a ship's bowthrusting
system.
[0002] Water jet propulsion systems are known in the marine art for propelling ships as
an alternative to conventional propellor propulsion: this is particularly beneficial
for use in water conditions where there would be a high risk of fouling of the propellor
or where there is small water depth mitigating against the use of a propellor. Such
a marine craft water jet propulsion system is shown in U.S. Patent 3,824,946, wherein
an impeller driven by the main engine of the marine craft draws in water via an aperture
in the craft's bottom and directs the water via ducting to a rearward discharge. The
system additionally includes a pair of vanes located externally at the discharge and
pivotal about parallel vertical axes whereby the discharge direction of the water
jet can be varied to provide a steering effect. The conventional rudder can be dispensed
with and the variable direction water jet has the advantage of enabling the craft
to be manoeuvred even when the craft has little motion or way on. Further, the vanes
of U.S. Patent US-A-3,824,946 can be set to divert the water jet through 180° and
thereby provide rearward propulsion for the marine craft.
[0003] In the marine industry it is also established practice to fit ships with bow thrusting
devices to improve manoeuvrability, thereby reducing dependence on tugs when moving
in confined waters such as in rivers, canals or when docking or undocking. These use
water jets created by impellers in the manner as shown in U.S. Patent US-A-3,824,946
but directed to have a transverse component of discharge.
[0004] Bow thrusting systems typically consist of a pump, which may be driven by an auxilliary
diesel engine, electric or hydraulic motor, discharging through a system of ducting
and/or flow control devices. One example of a previous bow thrusting system is described
in published UK patent application No. 2007174A. The bow thrusting system of UK patent
application No. GB-A-2007174 comprises lateral ducting providing opposed lateral water
discharges in the forward section of the ship's hull; water is pumped to the ducting
from an aperture in the ship's bottom. Vane means located centrally in the ducting
are operable to direct the water to a selected one of the discharges or to both discharges.
Additionally, nozzle means are provided in each discharge and controllable, for example
by further vanes, whereby the water discharged from the ducting can be given a definite
forward or rearward component of motion, in addition to a purely transverse discharge
direction.
[0005] It is the main object of the present invention to provide a bow thrusting system
which is of simplified construction but which enables a higher degree of ship manoeuvrability
in comparison with prior systems. This object is met in the present invention by having
each discharge outlet of the lateral ducting comprising a diverging outlet portion
when viewed in plan view and by providing valve means to control the direction of
fluid flow through each discharge outlet or preclude fluid flow from the outlet, comprising
a pair of pivotal vanes at each discharge outlet having parallel pivot axes.
[0006] Preferably the parallel pivot axes of the vanes are located at the inlet to the diverging
outlet portion so that a portion of each vane projects into the diverging outlet portion.
[0007] Preferably further, each diverging outlet portion has a divergence angle of approximately
90°. In operation of the above thruster system according to the present invention,
the vanes at each discharge outlet can pivot in unison to control the direction of
water discharge, or be pivoted in a contra-direction to close the discharge outlet
when the water discharge is to recur from the other side only so as to create a turning
movement on the vessel. Thus, with opposed transverse discharges in a ship's bow thrusting
system, by selective operation of the valve vanes it is possible to achieve desired
sideways movements and also forward and reverse motions: turning movements are also
possible. There is no need for any additional central control vane system for selective
water flows to the discharge outlets, since in the present invention this control
is achieved by the vane pairs at the discharge outlets: this provides a simplification
in the construction. Further in contrast to the system of UK patent GB-A-2007174 each
vane pair of the present invention enables selection of a precise direction of water
discharge from an outlet anywhere in the range from the pure transverse direction
to a preferred angle of 45° on either side of said transverse direction: this enables
a high degree of manoeuvrability to be achieved.
[0008] An embodiment of the present invention will now be described by way of example with
reference to the accompanying drawings wherein:-
Fig. 1 shows a bottom view of a bow thruster system in a ship, in accordance with
the present invention.
Fig. 2 shows a cross-sectional side elevation of the thruster system of Fig. 1, and
Figs. 3 to 8 show various operational modes of the valve means of the thruster system
of Figs. 1 and 2.
[0009] Referring to Figs. 1 and 2, a transverse thruster 1 is fitted into a ship's hull
2 towards the bow thereof and comprises a transverse duct 3 close to the bottom 4
of the hull 2 and a pair of venturi-type discharges (or nozzles) 5 at opposite ends
of the duct 3 discharging externally of the hull 2. A central lateral duct 6 opens
into the transverse duct 3 and houses a pump 7 comprising an axial flow impeller 8,
flow to the impeller 8 being via a frustrum inlet 9 at the ships bottom 4. The impeller
is mounted on a shaft rotor 10 and located by a thrust collar 11 and a sleeve bearing
12, and the rotor 10 is driven by a suitable motor (not shown) e.g. electric or hydraulic
motor or a diesel engine, via a right angle gearbox 13 the outlet 14 from which is
connected to the rotor 10 by coupling 15. The weight of the pump rotating element
and the pump axial hydraulic thrust is carried on a thrust bearing located in the
right angled gearbox. A shaft seal (25) is fitted to the rotor 10 below the coupling
15.
[0010] The pump 7 is set at as low as possible relative to the bottom of the ship to ensure
that the impeller 8 is fully submerged under all conditions of ship loading. The discharges
5 on the other hand may or may not be submerged under all loading conditions.
[0011] Control of flow from each of the discharges 5 is achieved by diverter valves 16 each
comprising a pair of parallel aerofoil vanes 17 fixed to parallel rotary shafts 18
supported in bearings 19. The shafts 18 are rotated by motors 20 (e.g. electrical
or hydraulic) via gearboxes 21, and it is a feature of the arrangement that the shafts
18 (and vanes 17) of each valve 16 can be rotated in unison or in a contra-direction.
As can be seen in Fig. 1 each discharge 5 includes a diverging outlet frustrum 22,
and the axes of the shafts 18 of each valve 16 are located in the plane containing
the frustum inlet end with a portion of each vane projecting into the frustrum.
[0012] In operation of the thruster 1, e.g. when the ship is manoeuvering in confined waters
or is docking or undocking, the pump 7 is driven to discharge water into the duct
3 and the desired manoeuvre is achieved by controlled thrusting discharge of the water
by means of diverter valves 16, as is illustrated in Figs. 3 to 6 and outlined as
follows:
Fig. 3. For sideways motion to port (leftwards) the port valve 16 is closed by contra-
rotation of vanes 17 to bring the vane leading tips into engagement with duct 3 and
all the thrusting discharge is in a normal direction via the starboard discharge 5.
Fig. 4. This is similar to Fig. 3 but with the set up for sideways motion to starboard
(rightwards).
Fig. 5. In this arrangement the vanes 17 of each valve 16 are pivoted in unison but
with the vanes of one valve opposite to those of the other to give reverse motion.
Fig. 6. In this case the vanes 17 are oppositely pivoted relative to Fig. 5 for forward
motion.
[0013] It is also possible to impart turning movement by pivoting the vanes 17 in unison
as shown in Figs. 7 and 8: this operational mode is more effective where the thruster
is located closer to the centre of turning (centre of gravity) of the ship.
[0014] Where the thruster is at a substantial distance from the centre of turning, it will
be appreciated that the arrangements of Figs. 1 and 2 will also impart turning movements.
[0015] Valve position selection can be carried out remotely e.g. from the ship's bridge
control room. The angle of pivoting of each vane may be varied for fine manoeuvres,
and the thrust can be adjusted by varying the pump speed to give alteration of the
water flow through the ducting.
[0016] The above valve arrangement provides efficient control of the direction of the discharging
flow and hence correspondingly efficient thrusting in any of the desired directions
as described.
1. A thruster system for use in marine craft including ducting for location in the
hull of the craft, the ducting having a pair of opposed discharge outlets discharging
externally of the hull, means for directing a fluid flow through the ducting to the
discharge outlets and control means for controlling the flow discharge characterised
in that each of the discharge outlets (22) comprises a diverging outlet portion when
viewed in plan view (Fig. 1) and in that valve means (16) are provided to control
the direction of fluid flow through each discharge outlet (22) or preclude fluid flow
from the outlet, said valve means (16) comprising a pair of pivotal vanes (17) at
each discharge outlet (22) having parallel pivot axes (18).
2. A thruster system as claimed in claim 1 characterised in that the parallel pivot
axes (18) of the vanes (17) are located at the inlet to the diverging outlet portion
(22) so that a portion of each vane (17) projects into the diverging outlet portion.
3. A thruster system as claimed in claim 1 or 2 characterised in that the vanes (17)
are pivotal to bring a tip thereof into contact with a wall of the ducting (3) upstream
of said diverging outlet portion (22).
4. A thruster system as claimed in any of the preceding claims characterised in that
each diverging outlet -portion comprises wall portions (22) diverging outwardly in
planar view to meet a side (2) of the marine craft.
5. A thruster system as claimed in claim 4 characterised in that the angle of divergence
of the wall portions (22) approximates to 90°.
6. A thruster system as claimed in any one of the preceding claims characterised in
that the valve means (16) are located in the throat of a venturi-nozzle discharge
(5).
7. A thruster system as claimed in any one of the preceding claims characterised in
that the vanes (17) are mounted on rotatable shafts (18) which are driven by motor
means (20,21).
8. A thruster system as claimed in any one of the preceding claims, characterised
in that the vanes (17) are of aerofoil form.
1. Système pousseur destiné à être utilisé dans des embarcations marines, comportant
un système de conduits destinés à être placés dans la coque de l'embarcation, le système
de conduits possédant une paire d'orifices de sortie opposés débitant à l'extérieur
de la coque, des moyens permettant de diriger, au travers du système de conduits,
un débit de fluide arrivant aux orifices de sortie et des moyens de commande servant
à commander la sortie du fluide, caractérisé en ce que chacun des orifices de sortie
(22) comprend une partie qui diverge quand on la voit en plan (Fig. 1 ) et en ce que
des organes formant valve (16) sont prévus pour commander la direction du débit de
fluide sortant de chaque orifice de sortie (22), ou interdire le débit par cet orifice,
lesdits organes formant valve (16), montés à chaque orifice de sortie, comportant
une paire d'aubes (17), montées à pivotement, munies d'arbres de pivotement parallèles,
(18).
2. Système pousseur selon la revendication 1, caractérisé en ce que les axes parallèles
de pivotement (18) des aubes (17) se trouvent à l'entrée de la partie divergente de
l'orifice de sortie (22), de sorte qu'une partie de chaque aube (17) fait saillie
dans la partie divergente de l'orifice.
3. Système pousseur selon la revendication 1 ou 2, caractérisé en ce que les aubes
sont montées à pivotement de façon qu'un de leurs bords puisse être amené à toucher
une paroi du système de conduits (3) en amont de ladite partie divergente de l'orifice
(22).
4. Système pousseur selon une quelconque des revendications précédentes, caractérisé
en ce que chaque divergent de sortie comprend des portions de paroi (22) qui divergent
vers l'extérieur (sur une vue en plan) et vont rencontrer un bord (2) de l'embarcation
marine.
5. Système pousseur selon la revendication 4, caractérisé en ce que l'angle de divergence
des portions de paroi (22) est voisin de 90°.
6. Système pousseur selon une quelconque des revendications précédentes, caractérisé
en ce que les organes formant valve (16) sont placés au col d'une sortie en forme
de buse de Venturi.
7. Système pousseur selon une quelconque des revendications précédentes, caractérisé
en ce que les aubes (17) sont montées sur des arbres pivotants (18) entraînés par
des organes moteurs (20,21).
8. Système pousseur selon une quelconque des revendications précédentes, caractérisé
en ce que les aubes (17) ont la forme d'un profil aérodynamique.
1. Schubsystem für ein Wasserfahrzeug mit einem in den Fahrzeugrumpf einbaubaren Kanal,
der zwei gegenüberliegende Ausstoß- öffnungen aufweist, die außerhalb des Rumpfes
ablassen, mit Mitteln, die einen Fluidstrom durch den Kanal zu den Ausstroßöffnungen
richten und mit Mitteln zur Steuerung der Ausströmung, dadurch gekennzeichnet, daß
jede Ausstoßöffnung (22) - in Draufsicht gesehen (Fig. 1) - einen divergierenden Auslaßteil
aufweist und daß Ventilmittel (16) zur Steuerung der Richtung des Fluidstromes durch
jede Ausstoßöffnung (22) oder zur Verhinderung des Fluidstromauslasses vorgesehen
sind, wobei das Ventilmittel (16) an jeder Ausstoßöffnung (22) mit zwei schwenkbaren
Flügeln (17) versehen ist, deren Drehachsen (18) parallel verlaufen.
2. Schubsystem nach Anspruch 1, dadurch gekennzeichnet, daß die parallelen Drehachsen
(18) der Flügel (17) an dem Eingang zu dem divergierenden Auslaßteil (22) angeordnet
sind, so daß ein Teil jedes Flügels (17) in den divergierenden Auslaßteil hineinragt.
3. Schubsystem nach Anspruch 1 oder 2, dadurch gekennzeichnet, daß die Flügel (17)
so schwenkbar sind, daß sie mit ihrer einen Spitze stromaufwärts zu dem divergierenden
Auslaßteil (22) eine Wand des Kanals (3) berühren.
4. Schubsystem nach den vorangegangenen Ansprüchen, dadurch gekennzeichnet, daß jeder
divergierende Auslaßteil Wandabschnitte (22) aufweist, die - in Draufsicht - auswärts
divergieren, um mit einer Seite (2) des Wasserfahrzeugs zusammenzutreffen.
5. Schubsystem nach Anspruch 4, dadurch gekennzeichnet, daß der Divergenzwinkel des
Wandabschnittes (22) sich 90° nähert.
6. Schubsystem nach den vorangegangenen Ansprüchen, dadurch gekennzeichnet, daß die
Ventilmittel (16) in dem Hals eines Venturidüsenauslasses (5) angeordnet sind.
7. Schubsystem nach den vorangegangenen Ansprüchen, dadurch gekennzeichnet, daß die
Flügel (17) auf drehbaren Wellen (18) angeordnet sind, die von Motormitteln (20, 21)
angetrieben werden.
8. Schubsystem nach den vorangegangenen Ansprüchen, dadurch gekennzeichnet, daß die
Flügel (17) Stromlinienflügelform aufweisen.