Vessel for operating on a body of water, comprising an aft foil for generating a thrust force and adjustment means for adjusting an angle of incidence of the aft foil

Abstract

The invention relates to a vessel (1) comprising a hull (2) for non-planing operation, during operation displaying a waterline (3) and having a forward direction in a horizontal plane (4) with a forward portion, an aft portion (5), and a central portion, the aft portion having a smaller water displacement relative to a water displacement of the central portion; and an aft, primary foil (6) affixed to the aft hull portion with a connecting member (7), configured to be below the waterline during operation, spaced from the hull, the aft foil having a span, a chord, a profile, a leading edge (8) and a trailing edge (9) relative to the forward direction, characterized by adjustment means (10) connected to the aft foil and configured for adjusting an angle of incidence (.sub.c, af) of the chord of the aft foil.

Claims

1. A vessel (1) for operating on a body of water comprising: a hull (2), designed for non-planing operation on the water body, during operation displaying a waterline (3) and having a forward direction in a horizontal plane (4) with a forward portion, an aft portion (5), and a central portion, the hull being configured to have the aft portion with a smaller water displacement relative to a water displacement of the central portion; and an aft, primary foil (6) affixed to the aft hull portion with one or more connecting members (7), configured to be below the waterline during operation, and spaced from the hull, the aft, primary foil having a span (b.sub.af), a chord (c.sub.af), a profile, a leading edge (8) and a trailing edge (9) relative to the forward direction, providing the aft foil with a configuration suitable for generating a lift force (L.sub.af) having a forwardly-directed thrust component, wherein adjustment means (10) is connected to the aft foil, wherein the adjustment means are arranged for rotating the aft foil around a center of pressure, at or near a quarter-chord location of the aft foil, and configured for adjusting an angle of incidence (.sub.c, af) of the chord of the aft foil to an estimated or measured angle of incidence (.sub.if) of an incoming flow (20) upstream of the aft foil, below the hull, to obtain a highest possible thrust from the aft foil.

2. The vessel according to claim 1, wherein the aft foil is provided with a shaft (11) aligned in bearings (36) extending in a span-wise direction of the aft foil, at the center of pressure of the aft foil, wherein the adjustment means are configured for rotating the aft foil around the shaft.

3. The vessel according to claim 1, wherein the adjustment means are connected to a control system configured to allow for controlling the angle of incidence (.sub.c, af) of the chord of the aft foil according to a cyclic pattern, whereby the aft foil can perform a flapping motion for propelling the vessel.

4. The vessel according to claim 1, wherein the adjustment means are fitted with a stop device (12) to limit minimum and maximum angles of incidence (.sub.c, af-min, .sub.c, af-max) of the chord of the aft foil.

5. The vessel according to claim 1, wherein a secondary foil (13) is connected to the aft foil, upstream of the aft foil, via a connection device (14).

6. The vessel according to claim 5, wherein the secondary foil is connected to the aft foil via a connection device configured for allowing the chord of the secondary foil to keep an angle of incidence (.sub.c, sf) irrespective of the angle of incidence of the chord of the aft foil (.sub.c, af) to which the secondary foil is connected.

7. The vessel according to claim 5, wherein the secondary foil has a smaller span (b.sub.sf) or smaller chord length (L.sub.c, sf) than the aft foil.

8. The vessel according to claim 1, wherein the adjustment means comprise an actuating mechanism (15) connected to the aft foil.

9. The vessel according to claim 1, wherein the adjustment means comprise an actuating mechanism (16) connected to the secondary foil.

10. The vessel according to claim 6, wherein the aft foil and the secondary foil possess a symmetrical foil section.

11. The vessel according to claim 1, comprising two aft foils separated in a transverse direction of the vessel, each aft foil being provided with separate adjustment means (10).

12. The vessel according to claim 5, wherein the connection device comprises a force or strain gauge (19) to measure a lift force on the secondary foil.

13. A method for operating a vessel according to claim 1, comprising the step of operating the adjustment means for rotating the aft foil around a center of pressure, at or near a quarter-chord location of the aft foil, and for controlling the angle of incidence (.sub.c, af) of the chord of the aft foil (c.sub.af) to an estimated or measured angle of incidence (.sub.if) of the incoming flow (20) upstream of the aft foil, below the hull, to obtain the highest possible thrust from the aft foil.

14. The method according to claim 13, comprising the step of determining the angle of incidence (.sub.if) of the incoming flow upstream of the aft foil from a lift force (L.sub.sf) exerted on the secondary foil, the lift force (L.sub.sf) being directly related to the angle of incidence (.sub.if) of the incoming flow.

15. The method according to claim 13, comprising the step of operating the control system to allow for controlling the angle of incidence (.sub.c, af) of the chord of the aft foil according to a cyclic pattern, whereby the aft foil can perform a flapping motion for propelling the vessel.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) The present invention will be explained hereafter with reference to exemplary embodiments of a vessel and a method according to the invention and with reference to the drawings. Therein:

(2) FIG. 1 shows a schematic cross-sectional side view of the autonomous lift-control configuration;

(3) FIG. 2 shows a schematic cross-sectional side view of the stop device;

(4) FIGS. 3a-3b show cross-sectional side views of the aft foil and the secondary foil being connected by a connecting device with a double-hinge arrangement;

(5) FIGS. 4a-4c show schematic cross-sectional side views of the aft foil with an actuating mechanism in the form of a piston/round bar arrangement, wherein the actuating mechanism connects to the aft foil at a position behind the shaft;

(6) FIG. 5 shows a schematic cross-sectional plan view of the actuating mechanism according to FIGS. 4a-4c;

(7) FIGS. 6a-6c show schematic cross-sectional side views of the aft foil with an actuating mechanism in the form of a piston/round bar arrangement, wherein the actuating mechanism connects to the aft foil at a position in front of the shaft;

(8) FIG. 7 shows a schematic cross-sectional side view of the aft foil and the secondary foil with an actuating mechanism in the form of a piston/round bar arrangement, wherein the actuating mechanism connects to the secondary foil;

(9) FIGS. 8a-8b show schematic cross-sectional side views of the secondary foil with an actuating mechanism in the form of a piston/round bar arrangement;

(10) FIG. 9 shows a schematic plan view of the aft foil and the secondary foil with the piston/round bar arrangement fitted in secondary struts;

(11) FIG. 10 shows a schematic plan view of the aft foil and the secondary foil, wherein the aft foil is separated in a port and starboard part to be separately activated by the adjustment means; and

(12) FIGS. 11a-11d summarize the main exemplary embodiments of the invention.

DETAILED DESCRIPTION

(13) FIG. 1 shows a schematic cross-sectional side view of the autonomous lift-control configuration. FIG. 1 more specifically shows a vessel 1, such as a sailing yacht or boat or a motor-driven vessel, during operation on a water body with a waterline 3. Preferably, the non-planing vessel 1 according to the invention operates in a (relatively low) speed regime corresponding to a Froude number of lower than 0.5, such as lower than 0.4. A primary, aft foil 6 having a leading edge 8 and a trailing edge 9 is connected to an aft portion 5 of the hull 2 of the vessel 1, such as the transom 21, with one or more appropriate connection members 7, such as one or more struts 22, for instance having backward sweep as shown. The aft foil 6 is configured to be below the waterline 3 during operation and is spaced from the hull 2. The hull 2 is configured for non-planing operation, and has a forward direction in a horizontal plane 4, i.e. during operation the horizontal plane 4 will usually be aligned with the forward direction of the vessel 1 and the waterline 3. The aft portion 5 has furthermore a smaller water displacement relative to a water displacement of a central portion of the vessel 1. The aft foil 6 has a configuration suitable for generating a lift force (L.sub.af, L.sub.af) having a forwardly-directed thrust component. The struts 22 connect to the aft foil 6 at the center of pressure, i.e. approximately at a distance of L.sub.c, af from the leading edge 8 of the aft foil 6. During operation, when the vessel 1 is moving in the forward direction, a flow is generated below the hull 2. The incoming flow 20, 20 has a certain angle of incidence .sub.if, .sub.if with respect to the horizontal plane 4. The chord c.sub.af of the aft foil 6 is orientated with respect to the horizontal plane 4 at an angle of incidence .sub.c, af, .sub.c, af (being 0 degrees in FIG. 1).

(14) Upstream of the aft foil 6 adjustment means 10 are provided comprising a secondary foil 13 connected to the leading edge 8 of the aft foil 6 by means of a connection device 14. The adjustment means 10 are connected to the aft foil 6 and configured for adjusting the angle of incidence (.sub.c, af, .sub.c, af) of the chord of the aft foil 6 and thus the angle of attack of the aft foil 6. The adjustment means 10 comprising the secondary foil 13 are arranged for rotating the aft foil 6 around a center of pressure of the aft foil 6, preferably at a quarter-chord location of the aft foil 6. Thereto, the aft foil 6 is provided with a shaft 11 extending in a span-wise direction of the aft foil 6 (i.e. perpendicular to the plane of the drawing), at the center of pressure of the aft foil 6. The secondary foil 13 is then configured for rotating the aft foil 6 around the shaft 11.

(15) A lift force L.sub.sf, L.sub.sf will be generated on the secondary foil 13 by the incoming flow 20, 20. The magnitude and direction thereof will depend on the speed and angle of incidence .sub.if, .sub.if of the incoming flow. The lift force L.sub.sf, L.sub.sf on this secondary foil 13 is directly related and representative of the effective inflow angle (.sub.if, .sub.if). With the embodiment shown in FIG. 1, the lift force L.sub.sf, L.sub.sf on the secondary foil 13 can be advantageously used as a guide or sensor for setting the value of the angle of incidence and thus the angle of attack of the aft foil 6. The principle involved is related to a technique known in the literature as direct lift-control and it is based on actively adjusting the angle of attack of a foil to obtain the desired lift. By connecting the secondary foil 13 to the aft foil 6 and by fitting e.g. the shaft 11 aligned in bearings transversely in the aft foil 6, the latter is able to rotate upwards by the leading edge 8 when an upward lift on the secondary foil 13 leads to an upwards movement thereof (causing the aft foil 6 to be subjected to a moment M or M) and downwards by the leading edge 8 when a downwards lift on the secondary foil 13 leads to a downwards movement thereof. The configuration as shown in FIG. 1 could be referred to as an autonomous direct lift-control configuration. To optimize performance, the leading edge 8 of the aft foil 6 and the trailing edge of the secondary foil 13 are preferably spaced apart at a distance of between 1.0-8.0 times, more preferably 1.0-4.0 times the chord length L.sub.c, sf of the secondary foil 13. Preferably, the secondary foil 13 has a smaller span (b.sub.sf) and/or smaller chord length (L.sub.c, sf) than the aft foil 6, such as a span b.sub.sf of 0.1-0.5 times, for instance 0.2-0.4 times, the span b.sub.c, af of the aft foil 6 and/or a chord length L.sub.c, sf of 0.1-0.5 times, for instance 0.2-0.4 times, the chord length L.sub.c, af of the aft foil 6. Preferably, the aft foil 6 and/or the secondary foil 13 have a symmetrical, streamlined foil section. The connection device 14 may also comprise a force or strain gauge 19 to measure the lift force on the secondary foil 13. Other measurement means or estimation means for measuring or estimating the angle of incidence of the incoming flow are also conceivable. For optimum accuracy, such measurement or estimation means are preferably to be arranged upstream of the aft foil 6, below the hull 2, such as at a position below the aft, narrowing/constricting portion 5 of the hull 2. Preferably, such means are arranged at an upstream distance from the leading edge 8 of the aft foil 6 of 1.0-4.0 times, more preferably 1.0-2.0 times the chord length L.sub.c, af of the aft foil 6. Alternatively, the estimation (means) may comprise the (indirect) derivation or calculation of the angle of incidence of the incoming flow based on, for instance, the oscillatory motions of the vessel, such as by means of a control system.

(16) The position of the struts 22 may vary depending on the strength and stiffness requirements of the shaft 11. A particular strut configuration is that whereby the struts 22 are positioned at the tips of the aft foil 6, with a third strut situated in the symmetry plane of the aft foil 6 when the span of the aft foil 6 is otherwise too large (or when the port and starboard parts of the aft foil need to be separately activated). A particular two-strut configuration is that whereby the bending load in the shaft 11 is minimized, which requires the struts 22 to be located inboard from the tips of the aft foil 6 at a specific location.

(17) FIG. 2 shows a schematic cross-sectional side view of the stop device 12. The stop device 12 may comprise a cam 23 arranged on the non-rotating (non-shaft) part of the aft foil 6. Therein, the cam 23 is arranged inside a recess 24 of the shaft 11, wherein the recess extends in a circumferential direction along the circumference of the shaft 11. The length of the circumferential recess 24 is based on the maximum range of rotation permitted to the shaft 11 and could for instance be between 2 and +2 degrees with respect to the chord c.sub.af of the aft foil 6. In principle, the cam 23 and recess 24 combination could be arranged anywhere on the circumference of the shaft 11, but a location close to the chord c.sub.af is preferred.

(18) The drawback of this system is that once the secondary foil 13 is in its highest or lowest position (and the aft foil 6 at its maximum, respectively, minimum angle of attack) the flow needs to change direction by an appreciable angle before the secondary foil 13 adopts the opposite position. This can be illustrated by an example as follows. Suppose the inflow angle is 5 degrees relative to the horizontal in the aft and upwards direction. The upwards directed lift on the secondary foil 13 will then push it upwards exerting a moment on the aft foil 6 forcing it to tilt up by the leading edge 8. When the stop device 12 on its shaft allows for an angle of attack setting of +2 degrees the aft foil 6 will adopt an angle of attack of +2 degrees when the shaft 11 passes through the location of the centre of pressure and the friction of the shaft 11 in its bearings is not significant. The angle of attack of the secondary foil 13 is now also at +2 degrees to the horizontal. It follows that for the secondary foil to adopt a lower position the inflow angle will need to change by more than 7 degrees (from +5 degrees upwards to an angle less than 2 degrees downwards).

(19) FIGS. 3a-3b show cross-sectional side views of the aft foil 6 and the secondary foil 13 being connected by a connecting device with a double-hinge arrangement 25. The double-hinge arrangement 25 works by having two hinge points on the secondary foil 13 (spaced-apart in a direction perpendicular to the chord c.sub.sf of the secondary foil 13, such as on opposite sides of the chord c.sub.sf) to prevent spontaneous rotation of the secondary foil without a desired associated movement of the parallel linkage as shown, and, vice versa, to allow the parallel linkage to move as a result of a rotation of the aft foil 6, thereby rotating the secondary foil 13.

(20) FIGS. 4a-4c show schematic cross-sectional side views of the aft foil 6 with an aft foil actuating mechanism 15 (see FIGS. 11b and 11d) in the form of a piston/round bar arrangement. The actuating mechanism 15 connects to the aft foil 6 at a position behind the shaft 11. The actuating mechanism 15 may comprise one or more rod actuators or one or more piston-cylinder actuators, or a combination thereof. As shown in FIG. 4a, the piston/round bar arrangement, comprising a piston 26 and a round bar 27, is arranged in (one or more) streamlined struts 22. At a lower end of the round bar 27 a pin 29 is arranged engaging a slot 28 in the aft foil 6. By moving the round bar 27 in a length direction thereof, the orientation of the aft foil 6 can be adjusted. The streamlined strut 22 is swept backwards and consequently the round bar 27 extends at an angle with respect to the vertical.

(21) FIG. 5 shows a schematic cross-sectional plan view of the actuating mechanism according to FIG. 4a.

(22) FIGS. 6a-6c show schematic cross-sectional side views of the aft foil 6 with an actuating mechanism 15 in the form of a piston/round bar arrangement, wherein the actuating mechanism 15 connects to the aft foil 6 at a position in front of the shaft 11. In contrast with the embodiment as shown in FIGS. 4a-4c and 5, the round bar 27 now extends (and is arranged to move) in a vertical direction.

(23) FIG. 7 shows a schematic cross-sectional side view of the aft foil 6 and the secondary foil 13 with a secondary foil actuating mechanism 16 (please refer to FIG. 11c) in the form of a piston/round bar arrangement, wherein the actuating mechanism 16 connects to the secondary foil 13. The actuating mechanism 16 is arranged in a backwardly-swept strut 30 and is quite similar to the aft foil actuating mechanism 15 as described in the foregoing. The actuating mechanism 16 is used to rotate the secondary foil 13 and consequently to rotate the aft foil 6 around the shaft 11.

(24) FIG. 8a shows a schematic cross-sectional side view of the secondary foil 13 with the actuating mechanism 16 in the form of a piston/round bar arrangement according to FIG. 6, with three different orientations of the secondary foil 13 (I, II, III) being shown. The connection to the secondary foil 13 here is in the form of a pin/slot connection, with a pin 34 being able to slide back and forth in an accompanying slot 33 in the secondary foil 13, along the chord c.sub.sf of the secondary foil 13. Another variant is shown in FIG. 8b with the bar 32 extending in a vertical direction (again with three orientations (I, II, III) of the secondary foil 13 being shown).

(25) FIG. 9 shows a schematic plan view of the aft foil 6 and the secondary foil 13 with the piston/round bar arrangement fitted in the secondary struts 30 according to FIGS. 7 and 8a.

(26) FIG. 10 shows a schematic plan view of the aft foil 6 and the secondary foil 13 with the piston/round bar arrangement fitted in secondary struts 30 according to FIG. 8b, comprising a pair of secondary foils 13 separated in a transverse direction of the vessel (although only one is shown, on one side of the plane of symmetry 35 of the vessel 1). Analogously, an associated pair of aft foils 6 is provided with each aft foil 6 being provided with individual adjustment means 10 in the form of an individual secondary foil 13. Multiple shaft bearings 36 are shown to support the shaft 11 at spaced-apart positions along the length of the shaft 11. Preferably, bearings 36 are arranged near the struts 22 and at intermediate positions (such as halfway) between the struts 22.

(27) It should be noted that the dimensions shown in FIGS. 9 and 10 are merely exemplary.

(28) FIGS. 11a-11d show a summary of the main exemplary embodiments of the invention. From top to bottom, the autonomous direct-lift configuration is shown in FIG. 11a. The powered lift-control configurations are shown in FIGS. 11b and 11c, and FIG. 11d shows an exemplary embodiment of the powered lift-control configuration wherein the adjustment means 10 are connected to a control system for allowing the adjustment of the angle of incidence (.sub.c, af) of the chord of the aft foil 6 according to a cyclic pattern, whereby the aft foil 6 can perform a flapping motion for propelling the vessel 1. The secondary foil 13 is then omitted and the aforementioned actuating mechanism 15 can in principle be used for rotating the aft foil 6.

(29) It should be clear that the description above is intended to illustrate the operation of preferred embodiments of the invention, and not to reduce the scope of protection of the invention. Starting from the above description, many embodiments will be conceivable to the skilled person within the inventive concept and scope of protection of the present invention.

LIST OF REFERENCE NUMERALS

(30) 1. Vessel

(31) 2. Hull

(32) 3. Waterline

(33) 4. Horizontal plane

(34) 5. Aft portion

(35) 6. Aft foil

(36) 7. Connecting member

(37) 8. Leading edge

(38) 9. Trailing edge

(39) 10. Adjustment means

(40) 11. Shaft

(41) 12. Stop device

(42) 13. Secondary foil

(43) 14. Connection device

(44) 15. Aft foil actuating mechanism

(45) 16. Secondary foil actuating mechanism

(46) 17.

(47) 18.

(48) 19. Force or strain gauge

(49) 20. Incoming flow

(50) 21. Transom

(51) 22. Strut for fixing aft foil at c/4

(52) 23. Cam (stop device)

(53) 24. Recess (stop device)

(54) 25. Double-hinge arrangement

(55) 26. Cylinder

(56) 27. Bar

(57) 28. Slot in aft foil

(58) 29. Pin (to engage slot in aft foil)

(59) 30. Strut for fixing secondary foil

(60) 31. Cylinder

(61) 32. Bar

(62) 33. Slot in secondary foil

(63) 34. Pin (to engage slot in secondary foil)

(64) 35. Plane of symmetry of vessel

(65) 36. Shaft bearing

(66) c.sub.af=chord of aft foil

(67) c.sub.sf=chord of secondary foil

(68) b.sub.af=span of aft foil

(69) b.sub.sf=span of secondary foil

(70) L.sub.c, af=chord length of aft foil

(71) L.sub.c, sf=chord length of secondary foil

(72) L.sub.af=lift force on aft foil

(73) L.sub.sf=lift force on secondary foil

(74) .sub.c, af=angle of incidence of chord of aft foil

(75) .sub.c, sf=angle of incidence of secondary foil

(76) .sub.if=angle of incidence of incoming flow