SHIP'S STEM DUCT WITH AIRFOIL SECTION

Abstract: The invention refers to the stem duct (2) of a ship (1) used to achieve the reduction of the ship's propulsion wave height and the improvement in the laminarity of the flow around the ship's bow (3), so that the ship would be able to move with an increased speed and/or with reduced fuel consumption. The duct is mounted on each side of the bow frontal surface and has an airfoil section (6) fitted, arranged in the direction of the flow, with its leading edge at the duct inlet and its trailing edge at the duct outlet. Following mounting of the duct, a passage (7) is created for the flow, between the duct's interior surface, consisting of the convex airfoil surface, and the ship's bow surface (3). The flow passing through the abovementioned passage acquires an increased speed and a reduced pressure, thereby leading to an improved slip of the ship.

Description: SHIP'S STEM DUCT WITH AIRFOIL SECTION THE FIELD OF THE ART The present invention refers to the technical field of hydrodynamics, and in particular to the means and methods for improving the flow characteristics of sailing vessels. Specifically, it refers to the stem duct of a ship, featuring an airfoil section and achieving a significant improvement in the ship's flow characteristics. THE PRIOR ART In shipping technology in general, efforts have been made to reduce the frictional resistance and the wave making resistance encountered by ships, and, consequently, to improve their sailing through the compact mass of water they traverse. For this reason, and especially for the limitation of the height of the bow wave that the ship has to encounter, a technique has been established, according to which the fore body of the ship's hull is modulated in a bulb or ball shape. In this way, the wave making resistance encountered by the ship is reduced. The ship's frontal surface through, namely the extensive bow area participating in the process of making way to propel the ship through the water, is very wide. Taking into consideration that the propulsion resistance is proportional to the square of the ship's velocity, then the increase of power needed to overcome this resistance, is also proportional. To overcome this problem and to reduce the propulsion resistance and the wave making energy that the ship's frontal surface encounters, the attachment of a duct on the ship's stem has been proposed in the past (E.E. Petromano- lakis, WO 92/22456) . As the ship impacts to the water mass through this duct, which extends in height above and beneath the ship's waterline, and not with it's entire frontal surface, the reduction of the wave making resistance created by the ship's propulsion is expected. It was not possible however for such a duct - acting as a wave making resistance absorber - to produce the expected results, since it was not possible to differentiate the flow through the duct from the sea water flow around the frontal surface of the ship significantly, although a small variation was possible. Other attempts of the prior art, like the French Patent FR-A-1 017897, have produced negative results, since not only they did not achieve the reduction of the wave making resistance developed during ship' s propulsion, but furthermore they comprised moving parts, which reqired the supply of power by the ship's main engine. The result was negative as far as the power required for the ship's propulsion was concerned. Further, WO-A-82 03055 (SEE) proposed a pipe to convey water from the stem to the stern of the ship, in order to use it at this point for the propulsion of revolving elements. This is a totally different aspect; furthermore it is highly uncertain if it can be implemented, because of the friction, the turbulence etc. Other documents of the prior art which have attempted to solve the same abovementioned problems are DE-C-931090 (Kuckuck) , DE-A-30 45977 (M.A.N. AG) , DE-A-3508203 (WIESER) and FR-A-847445 (TISCHENBACH) . Most of these patents do not disclose any kind of hydrodynamic section and more particularly airfoil section, whereas they do not achieve to create differentiated flow in the passages defined interiorly of the duct as compared to flow external to the duct. Prior art documents fail to create this necessary differentiated condition, because they on the one hand have an open end and not closed bottom, whereas on the other hand they extend at an insufficient height above the ship's waterline. Characteristically, DE-C-931090 defines in the specification and illustrates in the drawings, the height of the duct above ship's waterline to be such as to make the duct visible above waterline, which is a height that cannot ensure separation of the flow within the duct from the flow outside it. Experimental work on the proposed stem duct has proven that the airfoil configuration and orientation of the duct with respect to the vessel's bow is of significant importance for achieving the optimum results with regard to the increase in the water flow within the duct and correspondingly decreased pressure interior to the stem duct and flow depression downstream of the same. Many of the patents of the cited prior art fail to provide advantageous outcome due to the fact that they either have an adverse airfoil configuration, as by way of example airfoils with concave interior surface or they are located so as to create adverse water flow conditions interior to the duct, as by way of example an orientation forming a continously diverging flow passage. Thus, the main object of the present invention is to effectively overcome the abovementioned disadvantages and drawbacks of the prior art and propose a ship' s stem duct with such a configuration and orientation, that will ensure the differentiation of the characteristics of the flow interiorly to the stem duct from the flow outside it, so as to create an increased water flow speed through the passage in between the stem duct and the bow frontal surface compared to the water flow speed outside it, thereby causing the reduction of pressure interior to the stem duct and a flow depression downstream from the stem duct, the above resulting to a proportional decrease in the resistance to the ship's propulsion. In this way the ship's slip is improved and the result is a speed increase and/or a decrease in the power consumption with corresponding reduction in the fuel consumption. A further object of the present invention is to provide the proposed stem duct with an orientation and an airfoil configuration, such as to advantageously render the results of increased water flow speed and decreased pressure within the interior of the duct relative to the speed and pressure around the outer surface of the same, the optimum duct orientation and airfoil configuration being that of an airfoil having a convex interior surface and forming a flow passage on either side of the vessel's bow, which initially converges and subsequently diverges in a rearward direction of the ship. All these and other objects, characteristics and advantages of the present invention will be clarified in the detailed description below. BRIEF DESCRIPTION OF THE DRAWINGS The present invention will be made clear to those skilled in the art, by reference to the accompanying drawings, in which are depicted some illustrative but not restrictive embodiments of the invention. Fig. 1 presents a side view of a ship with a bulb/ball stem, without a propulsion resistance reducing stem duct. Fig. 2 presents a top view of the bow section of the ship of Fig. 1, with a diagram of the streamlines formed during the propulsion of the ship. Fig. 3 presents a front view of a fore body section of the ship of Fig. 1. Fig. 4 presents the side view of a ship with bulb/ball stem, additionally fitted with a stem duct with airfoil section, which generally follows the bow configuration and is closed on top, welded at the sides of the ship. Fig. 5 presents a top view cross section along the waterline of the ship of Fig. 4. Fig. 6 presents the front view of a fore body section of the ship of Fig. 4. Fig. 7 presents a top cross sectional view of the fore body of the ship of Fig. 4, with a diagram of the streamlines formed during the propulsion of the ship. Fig. 8 presents the side view of a ship with bulb/ball stem, additionally fitted with a stem duct of airfoil section, attached to the side of the ship through a set of supporting elements. Fig. 9 presents a top cross sectional view along the waterline of the ship of Fig. 8. Fig. 10 presents the front view of a fore body section of the ship of Fig. 8. Fig. 11 presents the side view of aship with bulb/ball stem, with a stem duct beginning exactly at the stem line and generally following the ship's lines. Fig. 12 presents the side view of a ship, where the stem duct is fitted internally with a set of parallel plates, arranged longitudinally to render a laminar flow through the stem duct. Fig. 13 presents a top cross sectional view of the fore body of the ship of Fig. 12. Fig. 14 presents a front view of a fore body section of the ship of Fig. 12. Fig. 15 presents a perspective side view of the ship's fore body section, with the stem duct having a shape different from the ship's stem lines. Fig. 16 presents a diagram of horsepower / speed for a common vessel, for a vessel with a bulb/ball stem and for a vessel equipped with the stem duct of the invention. DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS Referring now to the accompanying drawings, we will describe certain preferred, illustrative embodiments of the invention. Initially, in Figs. 1,2 and 3, are presented the perspective side view, top view and front view of a vessel 1 with bulb/ball 3, but without the stem duct of the invention. As indicated particularly in Fig. 2, the fluid streamlines around the bow frontal surface maintain the same density before and after the stem, on both sides of the bow frontal surface. The effect of fitting the stem duct of the invention around the ship' s bow frontal surface, as diagramatically and illustratively presented in Fig.7, is the differentiation of the flow characteristics and especially a reduced density of the streamlines 5, downstream the stem duct. In Figs. 4,5 and 6 are presented the perspective side view, the top view and the front view of a vessel 1 with a bulb / ball 3 and with the airfoil section stem duct 2 of the invention fitted. Naturally, the duct can also be installed to ships without a bulb / ball. The stem duct 2 of the invention is fitted at the bow of the ship 1 and on both sides of its frontal surface, extending in height above and beneath the ship's waterline. The height of the duct 2 above the ship' s waterline is preferably such, that the upper part of the duct exceeds the expected maximum wave height, e.g. 5 - 6 meters above the waterline. In any case the proposed stem duct extends at a height such that under any conditions of ship's loading it lies above the water and the flow within the duct is separated from the flow outside it. Beneath the waterline, the duct can reach down to the bulb / ball 3, if it exists, or even to cover it, concealing it inside. The duct 2 generally follows the morphology, i.e. the geometry of the ship's stem lines and it closes at the bottom. The duct can extend in the direction of the flow, fore or aft the bow, or occupy any intermediate position. Preferably, a position is selected, where the duct protrudes fore of the bow in the direction of the flow, by approximately half its length. The duct 2 can be partially or fully opened or closed at the top, always satisfying the condition that the flow within the duct is absolutely separated from the flow outside it. In Figs. 4,5,6 a duct is presented, with converging walls that close on top, attached and welded to the ship's sides, whilst in Figs. 8,9 and 10 a ship is presented, with the stem duct 2 open on top, attached to the ship's sides through an appropriate set of supporting elements 4. When such supporting elements 4 are used, they should preferably have a hydrodynamic section, convex on both sides, arranged in the direction of the flow, or alternatively they may be pipes of any conventional form. In the constructions presented in Figs. 4,5 and 6 with the duct closed on top and in the construction presented in Figs. 8,9, 10 with the duct 2 open on top, attached to the ship 1 through the supporting elements 4, the duct generally appears to follow in shape the general morphology of the bow in the vertical direction. It is possible however that the duct has a different shape. Thus the duct can be arranged around the bow frontal surface, with any geometrical shape, in any case different than the general morphology of the bow frontal surface in the vertical direction, as by way of example is presented in the perspective side view of Fig. 15. It is also pointed out that the stem line of a ship, equipped with a stem duct can be either parallel or inclined to the normal vertical, the ship being regarded in still position. The incident line around the duct 2 can also be inclined, with inclination similar or different than the inclination of the stem line. As illustratively presented in Fig.11, the incident line of duct 2 follows exactly the ship's stem line. The duct 2 can be used with any bow morphology in general. By way of example, the ship's bow adequately thinned along the line of incidence of sea water may be preferable. When the stem duct proposed in the present invention is installed, a passage 7 is formed for the flow, between the interior surface of duct 2 and the bow frontal surface. The flow passage 7 includes at least one inlet opening and at least one outlet opening for the water flow on each side of the ship. The characteristic feature of the duct 2 of the present invention is that the duct walls have an airfoil section in the lognitudinal direction of the flow, from the abovementioned at least one inlet opening to the abovementioned at least one outlet opening, on both sides of the ship 1. This airfoil section has its leading edge at the abovementioned at least one flow inlet opening and its trailing edge at the abovementioned at least one flow outlet opening. The convex side of the airfoil section duct 2 constitutes the internal surface of the duct, so that a higher flow speed and a correspondingly lower pressure is created in the internal convex side with respect to the external side of the duct, as known by the airfoil theory. The duct's external side may have either a flat or a slightly concave surface. Conseqeuently, such a section of the duct 2 of the invention causes the water mass passing through the passage 7 to gain an increased speed in relation to the water mass flowing around the external walls of the duct 2. This differentiation of the flow velocity results in a pressure drop inside the duct and in the creation of depression downstream the duct 2, thus rendering an improved laminar flow around the vessel's bow, decrease of the bow wave height and consequently achieving a better slip, of the vessel. As presented in Figs. 12, 13 and 14 the proposed airfoil section duct can have a series of projecting guide plates 6 to render an improved laminar flow, attached longitudinally on its internal surface. Guides plates 6 preferably have an airfoil section and are oriented with their leading edge at the abovementioned flow inlet opening and their trailing edge at the flow outlet opening. Each one of these guide plates is mounted at either both the interior surface of each of the side wall portions of the duct and the corresponding bow side surface or it is mounted at either the duct's wall portions or at the correspoding one of the bow side surfaces. Slots can also be provided along or across the distance between the side wall portions of the duct and the bow sides, so as to allow vertical communication of water flow within the flow passages in between consecutive guide plates. A similar series of projecting guide plates can also be fitted to the duct's external surface. Experiments have been conducted on a model, using the duct of the invention with airfoil coefficients CD=0.012 and CL=-1.3. An improvement of the flow characteristics resulted from these experiments. Thus, the towing resistance was reduced by a percentage of around 7.5% and a corresponding horsepower saving of around 10% - 12% was achieved for the vessel. The reduction of the above experimental data onto a real vessel was performed by the FROUDE method. The above experiments were conducted with a bare hull model, without a rudder, a propeller, etc. The results are presented in the attached table, where the horsepower values are shown for different values of speed. Three cases are presented: the case of a vessel with a small bulb without the proposed duct of the invention (Case A) ; the case of the same vessel with an improved bulb, specifically designed by the National Technical University of Athens with the scope of comparing the invention with the state of the art (Case B) ; and the case of a vessel with a small bulb, as in case A, on which the stem duct of the invention was installed (Case C) . The percentages referred to in the attached table indicate a relative increase (+) or decrease (-) of the horsepower, in comparison with case A of a ship with a small bulb and without a stem duct. The same results also appear in the diagram of Fig. 16. VESSEL SPEED VERSUS HORSEPOWER VESSEL SPEED CASE A CASE B CASE C (KNOTS) VESSEL WITH VESSEL WITH VESSEL WITH SMALL BULB IMPROVED BULB STEM DUCT WITHOUT DUCT OF INVENTION 14 2264 2581 + 14% 2031 -10% 15 2885 3213 + 11% 2548 -12% 16 3652 3695 + 1% 3197 -12.5% 17 4442 4508 + 1% 4066 - 8.5% 18 5582 5310 + 5% 5000 -11.6% 19 6672 6442 -3% 6068 -9% 19.5 7613 7361 -3% 7029 -8% 20 8779 7641 -13% 7726 -12% Regarding the proposed stem duct, it must be pointed out that its location on the bow, its height above and beneath the ship' s waterline, its length along the direction of the flow, its inclination with respect to the vessel's symmetry axis and its distance from the ship's hull are determined in accordance with the bow morphology, the hull coefficients and the vessel's speed. At this point it has to be mentioned that the description of the present invention was made by reference to some illustative embodiments and that the ivention is not limited to those. Thus any modification or alteration regarding the shape, the size, the dimensions, the materials and the construction and assembly components of the proposed stem duct with an airfoil section is considered to be included in the aims and scope of the present invention, as long as it does not constitute a new inventive step and does not contribute to the technical evolution of the prior art. From the analysis of the experiments made on the abovementioned model for the specific airfoil with CD=0.012 and CL=1.3, resulted the following formula for the determination of duct's location i.e. of the airfoil inclination with respect to the vessel's symmetry axis, which has to lie in the range of values defined by: A2-A1=0.0425L ± 0.005L where, as presented in the accompanying Fig. 5, Al is the minimum distance between the duct's interior surface and the ship' s bow frontal surface and A2 is the distance between the duct's trailing edge and the ship's bow frontal surface, where A2 is measured from the innermost end of the duct's trailing edge. Both Al and A2 are measured along the same waterline and L is the length of the airfoil in the direction of the flow. Consequently, a preferred embodiment of the invention implies that all waterlines within the sea water satisfy the above formula and the inclination of the airfoil section is maintained as constant as possible on all waterlines. Naturally, the above formula defines a preferable range of values for the duct airfoil and its spacing from the ship' s bow frontal surface. From the above it follows that a preferred orientation of the proposed stem duct with respect to the bow frontal surface is such that the water flow passage between an interior surface of the stem duct and the bow on either side of the bow of the ship initially converges and subsequently diverges in a rearward direction of the ship. An experimental application of the airfoil section stem duct of the invention has already been made on a real vessel and specifically on the F/B RODOS, under Greek flag, registered in Rhodes island and owned by DANE SEA-LINE Company. This experimental application has given very satisfactory results.

Claims: CLAIMS 1. A stem duct (2) for use on a ship (1) having a bow including opposed bow sides and a bow frontal surface, said stem duct comprising wall portions adapted to be mounted to the bow of the ship (1) and to extend close to the bow frontal surface and upwardly on the opposed bow sides, and under any condition of ship's loading, said stem duct (2) being characterised in that it has a closed bottom end and defines a water flow passage (7) between an interior surface of said stem duct (2) and the bow, water flowing in said passage (7) being separated from water flowing outside it, said wall portions each including an airfoil portion extending generally in a longitudinal direction of the ship (1), said airfoil portions having on the opposed bow sides of the ship a leading edge defining at least one inlet opening of said water flow passage (7) and a trailing edge defining at least one outlet opening of said water flow passage (7), the airfoil portions having convex interior surfaces, said flow passages converging and then diverging in a rearward direction of the ship, wherein said convex interior surfaces increase the speed of water passing through said flow passages relative to the speed of water flowing around the outer surface of said stem duct (2) , to create a reduced pressure interior to said stem duct (2) and a flow depression downstream from said stem duct (2) . 2. The stem duct of claim 1, characterised in that it is shaped to substantially follow the shape of the oposed bow sides. 3. The stem duct of claim 1, characterised in that said airfoil portions are adapted to be mounted to the opposed bow sides such that an upper end of the airfoil portions are closed being welded on each side of the bow frontal surface of said ship (1), whereby is defined a perimetrically closed stem duct (2) . 4. The stem duct of claim 1, characterised in that it comprises supporting elements (4) adapted to be mounted to the opposed bow sides such that said stem duct (2) is partially open at the top on either side of the ship (1). 5. The stem duct of claim 3 or 4, characterised in that it comprises vertically spaced guide plates with airfoil section projecting inwardly from the interior surface of each of said side wall portions and adapted to extend generally in the longitudinal direction of the ship up to the opposed bow sides so as to enhance laminar water flow through said flow passages (7) , wherein the airfoil section of said guide plates is oriented with its leading edge at said inlet opening of said water flow passage (7) and its trailing edge at said outlet opening of said water flow passage (7) . 6. The stem duct of claim 3 or 4, characterised in that it comprises vertically spaced guide plates with airfoil section, projecting inwardly from the interior surface of each said side wall portions and adapted to extend generally in the longitudinal direction of the ship, so as to enhance laminar water flow through said flow passages (7), wherein the airfoil section of said guide plates is oriented with its leading edge at said inlet opening of said water flow passage (7) and its trailing edge at said outlet opening of said water flow passage (7) , and wherein said vertically spaced guide plates are mounted at either said interior surface of each said side wall portions or at each corresponding one of said bow sides and/or are provided with slots along or across the distance in between said side wall portions and said bow sides, so as to allow vertical communication of water flow within said flow passages (7) . 7. The stem duct of claim 1, wherein said stem duct has a flat exterior surface. 8. The stem duct of claim 1, wherein said stem duct has a concave exterior surface. 9. The stem duct of claim 1, characterised in that said side wall portions extend to a height above the waterline when the ship is in motion, such that under any condition of ship' s loading to obstruct sea water flowing within said flow passages (7) from coming in contact with water flowing outside it. 10. The stem duct of claim 1, wherein said wall portions are adapted so as to extend forwardly of the bow frontal surface. 11. The stem duct of claim 1, wherein said wall portions are adapted so as to extend aft of the bow frontal surface. 12. Ship's stem duct with airfoil section according to the above claims 1-9, wherein the location of said duct on the ship's bow, the geometrical shape of said airfoil section, the height of said duct above and beneath the ship's waterline, its length along the direction of the flow, its inclination with respect to the vessel's symmetry axis and its distance from the ship's hull are determined in accordance with the bow morphology, the hull coefficients and the ship's speed. AMENDED CLAIMS [received by the International Bureau on 08 July 1996 (08.07.96)- original claims 1 and 2 amended; original claims 9-11 cancelled;' new claim 9 added; claim 12 is renumbered claim 10; remaining claims unchanged (4 pages)] 1. A stem duct (2) for use on a ship (1) having a bow including opposed bow sides and a bow frontal surface, said stem duct comprising wall portions adapted to be mounted to the bow of the ship (1) and to extend close to the bow frontal surface and upwardly on the opposed bow sides, a water flow passage (7) being defined between an interior surface of said stem duct (2) and the bow, said stem duct (2) being characterised in that it is mounted externally to the bow, extending aft and forwardly of the bow frontal surface and has a closed bottom end and in that said side wall portions extend to a height above the waterline when the ship is in motion, such that under any condition oi ship's loading to obstruct sea water flowing within said flow passages (7) from mixing with water flowing outside it, said wall portions each including an airfoil portion extending generally in a longitudinal direction of the ship (1), said airfoil portions having on the opposed bow side-:" of the ship a leading edge defining at least one inlet opening of said water flow passage (7) and a trailing edge defining at least one outlet opening of said water flov-, passage (7) , the airfoil portions having convex inteπoi surfaces, said flow passages converging and then diverging in a rearward direction of the ship, wherein said convex interior surfaces increase the speed of water passing through said flow passages relative to the speed of water flowing around the outer surface of said stem duct (2) , to create a reduced pressure interior to said stem duct (2) and a flow depression downstream from said stem duct (2) . 2. The stem duct of claim 1, characterised in that it is shaped to substantially follow the shape of the oposed bow sides, substantially equal distance being obtained between wall portions of said duct and said opposed bow sides. 3. The stem duct of claim 1, characterised in that said airfoil portions are adapted to be mounted to the opposed bow sides such that an upper end of the airfoil portions are closed being welded on each side of the bow frontal surface of said ship (1) , whereby is defined a perimetrically closed stem duct (2) . 4. The stem duct of claim 1, characterised in that it comprises supporting elements (4) adapted to be mounted to the opposed bow sides such that said stem duct (2) is partially open at the top on either side of the ship (1) . 5. The stem duct of claim 3 or 4, characterised in that it comprises vertically spaced guide plates with airfoil section projecting inwardly from the interior surface of each of said side wall portions and adapted to extend generally in the longitudinal direction of the ship up to the opposed bow sides so as to enhance laminar water flow through said flow passages (7) , wherein the airfoil section of said guide plates is oriented with its leading edge at said inlet opening of said water flow passage (7) and its trailing edge at said outlet opening of said water flow passage (7) . 6. The stem duct of claim 3 or 4, characterised in that it comprises vertically spaced guide plates with airfoil section, projecting inwardly from the interior surface of each said side wall portions and adapted to extend generally in the longitudinal direction of the ship, so as to enhance laminar water flow through said flow passages (7), wherein the airfoil section of said guide plates is oriented with its leading edge at said inlet opening of said water flow passage (7) and its trailing edge at sai outlet opening of said water flow passage (7), and wherein said vertically spaced guide plates are mounted at either said interior surface of each said side wall portions or at each corresponding one of said bow sides and/or are provided with slots along or across the distance in betweer said side wall portions and said bow sides, so as to allow vertical communication of water flow within said flow passages (7) . 7. The stem duct of claim 1, wherein said stem duct has a flat exterior surface. 8. The stem duct of claim 1, wherein said stem duct has a concave exterior surface. 9. The stem duct of claim 2, mounted on a vessel in combination with adequately thinned said opposed bow sides. 10. Ship's stem duct with airfoil section according tc the above claims 1-9, wherein the location of said duct on the ship's ' bow, the geometrical shape of said airfoil section, the height of said duct above and beneath the ship' s waterline, its length along the direction of the flow, its inclination with respect to the vessel's symmetry axis and its distance from the ship's hull are determined in accordance with the bow morphology, the hull coefficients and the ship's speed. STATEMENT UNDER ARTICLE 19 This is my letter under Article 19(1 ), accompanying the amended claims and explaining these amendments. Having studied the documents of the prior art cited in the international search report, I have amended main claim 1 and dependent claim 2 of this appl ication, cancel led original claims 9-11 and added a new claim 9, so as to present the claims in a clearly distinctive manner from the prior art. With claims as presently amended, it is bel ieved that none of the documents of the prior art, taken alone or in combination, can teach the present invention, which in summary claims the be I owment i oned combination of distinctive features: a. The stem duct has an airfoi l section in the longitudinal direction of the vessel and defines an initial ly convergent and subsequently divergent passage for the flow of water, where the interior surface of the airfoi l duct is always suitably convex, whi lst the exterior surface might be either flat or concave . b. The airfoi l stem duct general ly extends in a height direction of the vessel from substantial l above to wel l below the vessel 's waterl ine under any condition of the vessel 's loading (as claimed in original claim 9, now cancel led and incorporated in main claim 1 ) and is always closed at the bottom, thereby defining a closed structure separating sea water flowing in the passage between the vessel and the duct from water flowing outside it. Even when the duct is open on top, due to its height, this condition is sti l l val id. c. The airfoi l stem duct extends aft and forwardly of the bow frontal surface, as depicted in the drawings and mentioned in the specification wherein is mentioned that the stem duct preferably protrudes fore of the bow by approxi ately half its length. The feature of the duct extending forwardly or aft of the bow frontal surface, initial ly claimed in original claims 10 and 11 , has presently been incorporated in main claim 1 , whi lst claims 10 and 11 have been cancel led. d. An embodiment of my airfoi l stem duct (figs. 8 and 10) i l lustrates it to fol low the form of the bow sides and/or of the bow frontal l ine, thereby rendering a substantial ly constant distance of the duct wal ls from the vessel 's wal ls, irrespective of the curvature of the latter, so as to define a substantial ly equal distance of the duct wal ls from the bow sides. Claim 2 has therefore been amended to clarify this feature and di fferentiate the claim from the cited art. Further newly added claim 9 defines the combination of the stem duct of the invention with a suitably thinned bow, which finds basis in the description (page 11 , l ines 10-12) . In the event that it is required by the examiners, a new drawing can be added to i l lustrate this embodiment. e. The guide plates mounted either on the interior or exterior surfaces of my stem duct have a hydrodynamic form and general ly fol low the form of the airfoi l surface, aiming at improving flow la inarity and thereby rendering a better mani festation of the di fferentiation in the flow within the duct from the flow outside it. It is final ly noted that claim 12 has been renumbered consecutively to become final claim 10 of the amended claims.

Inventors: PETROMANOLAKIS E EMMANUEL, PETROMANOLAKIS, E., EMMANUEL
Applicants: PETROMANOLAKIS E EMMANUEL, PETROMANOLAKIS, E., EMMANUEL
Application year: 1996
Main classification: B63B1
IPC codes: B63B1