FLOW-MODIFYING ELEMENT, ESPECIALLY A RUDDER

Abstract: Element, such as a rudder, and aircraft wing, a boat keel, a hydrofoil or an airfoil or the like is adapted to move through water or air and is so designed that the water or the air is allowed to enter at the upstream edge of the element into and through a hollow space within said element and to leave said element at the trailing edge thereof, said hollow space within said element being divided into two halves by a central longitudinal partition (6) within said element, such that said element on either side of the said central partition (6) has a flow gap which, optionally, is divided into parallel passages by transverse partitions (4a, 4b, 5a-5c), the arrangement being such that the flow of water or air through and out of the gap between the central partition (6) and that side of the element which, in response to the angular deflection or profile, forms the suction side of said element, will be substantially larger than through the other gap.

Description: FLOW-MODIFYING ELEMENT, ESPECIALLY A RUDDER The present invention relates to a rudder for boats and ships or, in other words, a rudder that can be used both for small vessels which are usually classed as "boats"' and for larger vessels, and both for propeller- driven vessels and sailing vessels. However, the rudder according to the invention also has other fields of application, for instance as a stabilizer, trim flap, keel and centerboard and, pos¬ sibly, also fields of application outside the maritime sphere, for instance in aircraft, as a wind deflector, for example on large trucks, as well as other uses. Generally speaking, the invention thus is applicable - to flow-modifying elements, but will be described in the following substantially with reference to ships' rudders. It is an old-established notion to make a rudder hollow from its leading edge to its trailing edge, and this notion has been brought up again from time to time. U.S. patent specification 2,961,987 points out by way of introduction, and quite correctly, that the deflec¬ tion of a rudder sets up hydrodynamic pressure on the pressure side of the rudder and a sub—normal pressure on the suction side of the rudder, whereby a strong eddy is produced in the vicinity of the rudder, pro- ducing a restraint on the ship's speed without having any useful effect on the desired rudder action. To re¬ duce the flow resistance and to avoid eddies in order to reduce the propulsion resistance, this patent spe¬ cification proposes a rudder having a series of flow passages which extend alternately from the opposite sides of the rudder from a vertical line near the lead¬ ing edge of the rudder to the trailing edge thereof, the flow passages which extend at an angle relative to the rudder plane from one side of the rudder cross- OMPI ing the corresponding passages proceeding from the op¬ posite side of the rudder without intersecting these passages because they lie in different vertical planes. The water is intended to flow into the passages proceed- ing from the pressure side of the rubber and to flow out on the suction side. However, this prior art construction does not pro¬ vide any favourable effect on drag and lift because the passages cross the rudder diagonally and, besides, set up a high flow resistance, for which reason they permit neither a sufficient throughflow quantity nor a sufficient flow velocity to achieve the objects stat¬ ed in this patent specification. A further disadvantage is that the known rudder upon zero rudder deflection contrary to a favourable effect causes considerable difficulties because the passage arrangement illustrated sets up a high water resistance and makes the rudder unstable. Finally, it should be mentioned that the passages of the known rudder cause constructional differences increasing the costs. The object of the present invention is to provide a rudder which has a favourable effect both on the pres¬ sure side and on the suction side and stabilizes the ship's way through the water from zero position of the rudder to maximum rudder deflections. These objects have now been achieved in that the rudder according to the invention has been given the characteristic features stated in claim 1 and, for pre- ferred embodiments, the characteristic features which are stated in claims 2-8. The invention will be described in more detail below, reference being had to the embodiments illustrat¬ ed in the accompanying drawings in which Fig. 1 is a schematic view of a sailing-boat of the fin-keel type having a hollow rudder and a hollow fin-keel according to the invention, Fig. 2 is perspective and more detail- ed view of a hollow rudder according to the invention, Fig. 3 is a schematic section of a part of the rudder shown in Fig, 2, Fig. 4 is a perspective view of the rudder shown in Fig. 1, mounted behind a tail piece, Fig. 5 illustrates an alternative embodiment of a hollow rudder according to the invention, Fig. 6 is ' a diagram illustrating the concepts "drag" and "lift" applicable to all rudders, Fig. 7 illustrates, in the form of a diagram, the relations between drag and speed in a hol- low rudder of the type which is shown in Fig. 6 and which has a NACA 0015 profile modified according to the invention, and Fig. 8 illustrates, in a similar diagram, an unmodified (conventional) NACA 0015 rudder. Figs. 9 and 10 illustrate the relation between lift and speed in a modified NACA 0015 rudder according to - the invention and an unmodified NACA 0015 rudder, re¬ spectively, Fig. 11 illustrates, in the form of a dia¬ gram, the effect of Reynolds' number on the lift and drag coefficients in an unmodified NACA 0015 rudder and a NACA 0015 rudder modified according to the inven¬ tion, and Fig. 12 is a corresponding comparison diagram (non-dimensional) between the modified and the unmodified NACA 0015 rudder at a given speed through the water. The rudder 1 and the fin-keel 2 as shown in Fig. 1 are designed in accordance with the invention and ba¬ sically correspond to the hollow rudder according to the invention, as shown in Fig. 2. The rudder shown in Fig. 2 has an outer shape which, at least in broad outline, corresponds to the outer shape of a conventional rudder. However, the rudder is hollow and comprises two outer side walls 3a, 3b which at the upper and lower rudder edges are intercon¬ nected by edge walls 4a, 4b. Furthermore, the two side walls are interconnected by means of a number of pa- rallel transverse partitions 5a-5c. Extending between the upper and lower edge walls 4a, 4b, in the central plane of the rudder, is a continuous central wall 6 protruding at the trailing edge of the rudder. ^ U tΛt OMPI As will appear from Fig. 2, the rudder is open at its leading edge, and the hollow space within the rud¬ der is divided, by the partitions referred to above, into eight parallel passages 7 arranged in two juxtapos- ed rows, the outlets of said passages being provided at 8 at the trailing edges of the side walls 3a, 3b. The rudder shape causes the passages 7 to taper such that the outlets at the edge 8 are essentially narrower than the inlets at the leading edge of the rudder. Within the region of the trailing part of the rud¬ der, the side walls have a series of holes 9 arranged in vertical and horizontal rows. These holes may have the shape which is illustrated in Fig. 3 where the rud¬ der walls 3a, 3b have been bent inwardly at the trailing edges of the holes. Fig. 3 indicates, by arrows 10, the flow direction through the passages 7 and the out¬ flow through the holes at zero deflection of the rudder, i.e. the flow is symmetrical in both directions. Water entering at the leading edge of the rudder will, of course, also leave the rudder at the outlets at the trailing edge of the rudder. Fig. 4 shows the rudder illustrated in Fig. 2 at a given rudder angle. The water flow (see the flow ar¬ rows) on the suction side has no adverse effect on the water flow on the pressure side, but affects the rela¬ tive sub-normal pressure on the suction side at the trailing part of the rudder and, because of the outflow of the water through the holes and through the passage outlets at the trailing edge of the rudder between the central wall 6 and the side wall 3a on the suction side, causes a considerable reduction in turbulence. It appears from Fig. 4 that the above-described shape of the holes, with inwardly bent walls 11 inter¬ cepting the water-flow, may to some extent increase the outflow of the water through the holes 9 * To simplify presentation, Fig. 2 shows the holes 9 only in the upper half the side wall 3b, but naturally also the lower half should be provided with similar holes. Furthermore, the number of the vertical rows of holes may be increased or decreased in order respec¬ tively to increase and decrease the apertured rudder area in response to the rudder construction, the rud¬ der shape and the rudder size. Fig. 5 illustrates an alternative embodiment in which the rows of holes are replaced by vertical open gaps to increase the water discharge. Fig. 5 merely shows a relatively wide gap 12 from the upper edge of the rudder to its lower edge. However, as is the case with the holes in Fig. 2, the number of the gaps 12 and their widths are selected according to the rudder shape and size. The drag and lift forces acting on a rudder are illustrated in Fig. 6. To the lift and drag coefficients j . and C_, re¬ spectively, the following relation applies: C L = _—, and 0.5p*V *s C D 0.5ρ*V^-s ein L = lift D = drag p = 1000 kρ/m 3 V = speed (m/s) 2 s = movable rudder area ( ) As will appear from the above and is shown in Fig. 4, the rudder according to the invention acts in such a manner that the water flow through the rudder at zero deflection will be symmetrical, i.e. the water outflow on both sides of the rudder will be the same and have a favourable effect on the separation and the turbulence and .cause a corresponding reduction of the resistance. At all rudder angles, from zero and upwards, it has been found that the tendency to rudder vibrations is eliminated, and furthermore it has been found that the rudder action at rudder deflection is essentially improved. The results of comparison model tests made with a hollow rudder according to the invention and a con- ventional rudder having the same profile (NACA 0015) with respect to "drag" and "lift" (see Fig. ζ and the above relation) will now be accounted for. Both rudders, including the tail piece, had a pro¬ file according to NACA 0015..In the above description and in the following, the rudder according to the in- ' vention is called a "modified NACA 0015 rudder", while the comparison rudder is called an "unmodified NACA 0015 rudder". Both rudders had been surface-treated in the same manner and were tested with the same tail piece and rudderstock. The rudderstock was permanently con- - nected to the tail piece. The tests were conducted at the Institute of Ship Hydromechanics at Chalmers Univer¬ sity of Technology, in the small basin of the Institute which has a length of 25 m, a width of 1.8 m, and a depth of 1 m. Travelling across the basin is a carriage with means for the exact fixation and connection of the test object. Provided in conjunction with the basin is a control room in which the towing speed is read and the forces are recorded by recording instruments. For the rudder tests, the rudderstock was fixed to the carriage in such a manner that the rudder was located in the middle of the basin and such that the distance between the upper edge of the rudder and the water surface was the same as the distance between the lower edge of the rudder and the bottom (0.15 m) . Tranducers for measuring drag and lift were applied to the rudderstock. The towing speed was read with an accuracy of 0.01 m/s. Drag and lift were read on the recorder with an accuracy of 5 N. The two rudder models "modified NACA 0015 rudder" (the hollow rudder according to the invention) and the "unmodified NACA 0015 rudder" were each tested in six test runs. "BUREA Figs. 7 and 8 illustrate the drag in kp as a func¬ tion of the speed in m/s for the rudder angle 0°, 5°, 10°, 20°, 30° and 35°. The comparison shows that the drag for the modified NACA 0015 rudder according to the invention (Fig. 7), at all rudder angles tested, is higher than for the comparison rudder (Fig. 8) . The corresponding lift values are accounted for in Figs. 9 and 10 where Fig. 9 shows the modified NACA 0015 rudder according to the invention and Fig. 10 shows the comparison rudder (the unmodified NACA 0015 rudder) . At all rudder deflection angles tested, the lift values are higher for the rudder according to the invention than for the comparison rudder. The diagram shown in Fig. 11 compares the effect - of the Reynolds' number on the lift and drag coeffi¬ cients at α = 10°. The full lines show the drag, and the broken lines show the lift. As will appear, the rudder according to the inven- tion gives a far better lift at the same drag than the unmodified NACA 0015 rudder. This is confirmed by Fig. 12 which shows a non-dimensional comparison between the rudder according to the invention and the unmodified NACA 0015 rudder at a speed of E = 1.45 m/s. It should be noted that the essential improvements accounted for above and afforded by the present inven¬ tion in relation to a conventional rudder having the same profile, were obtained before optimal flow gaps and holes could be established. An important feature of this invention is the cen¬ tral wall 6 dividing the gap-shaped hollow space, which is open at the leading edge of the rudder, into two juxtaposed spaced apart gaps with outlets at the trail¬ ing edge of the rudder. Otherwise, several modifications are possible, such as the arrangement of the outlets at the trailing edge of the rudder, considering that the holes 9 or the gaps (slots) 12 in the side walls 3a, 3b offer essential advantages in respect of the desired modification of the flow and the pressure di¬ stribution. Rudders and keels generally are symmetrical in relation to a vertical central plane and the flow pas¬ sages then preferably are symmetrically arranged on either side of the central partition 6. Aircraft wings, on the other hand, and also trim flaps generally have opposite sides which are non-symmetrical relative to one another, and in that case it is conceivable or even necessary to dispose the flow passages on one and the other side of a partition non-symmetrically in relation to one another, and it may also be advantageous to pro¬ vide the passages with closable flaps or the like, for instance at the inlets. SURE PA-PI

Claims: u AMENDED CLAIMS (received by the International Bureau on 29 Oetober 1982 (29.10.82)) 1. An element for use as a rudder, keel, part of a keel, stabilizer, trim flap, centerboard in ships, wing or rudder profile in aircraft, part of such wing or rudder profile, or as a flow deflecting visor, said element having a downstream edge and an upstream edge and comprising at least two wall means (3a, 3b, 6) de¬ fining at least one space (7) - therebetween, the outer side of at least one wall means (3a and/ or 3b) consti¬ tuting a flow surface for a fluid flowing from the up- stream edge of said element to the downstream edge there¬ of, and at least one space (7) having at least one inlet within the region of the upstream edge of said element, c h a r a c t e r i s e d in that at least one (3a and/ or 3b) of said wall means has outflow openings (9, 12) opening within the area of the said flow surface at a distance upstream of the downstream edge of said element, for discharging fluid, such as water or air, from said space out over an essential region of said flow surface at the downstream edge portion thereof. 2. An element as claimed in claim 1, c h a r a c ¬ t e r i s e d in that said wall means comprise a cen¬ tral partition (6) and two side walls (3a, 3b) disposed at a distance from and on either side of said central partition (6) symmetrically with respect thereto, each of said side walls defining a space (7) relative to said central partition (6) , and that the two spaces (7) on either side of said central partition (6) have inlets for the inflow of water or air at the upstream edge of said element (1) and outlets within the region of the downstream edge of said element. 3. An element as claimed in claim l or 2, c h a ¬ r a c t e r i s e d in that it forms a first element arranged as an extension downstream of a streamlined second element, in relation to which said first element is angularly adjustable, said second element having a downstream edge located adjacent and extending along the inlet opening of said first element, said inlet opening being located in and extending along the up- stream edge of said first element (Fig. 4) . 4. An element as claimed in any one of the pre¬ cedeing claims, c h a r a c t e r i s e d in that said outlet openings are a number of openings (9) arranged in vertical and horizontal rows. 5. An element as claimed in claim 4, c h a r a c ¬ t e r i s e d in that the downstream edges of the open¬ ings (9) are bent inwardly for intercepting and deflect¬ ing fluid flowing through said spaces. 6. An element as claimed in any one of claims 1-5, c h a r a c t e r i s e d in that said openings are - slots (12) substantially parallel to the inlet edge of said element. 7. An element as claimed in any one of claims 2-6, c h a r a c t e r i s e d in that the central parti- tion (6) is positioned in the central plane of said element (1) and extends from the upstream edge of said element to and beyond the downstream edges of said side walls (3a, 3b) . 8. An element as claimed in claims 2 and 3, c h a - r a c t e r i s e d in that the said spaces or each space is divided into several parallel flow passages (7) by means of transverse walls (4a, 4b, 5a-5c) . EDITORIAL NOTE The applicant failed to renumber the amended claims in accordance with Section 205 of the Administrative Instructions. In the absence of any specific indication from the applicant as to the correspon¬ dence between origina- and amended claims, these claims are published as filed and as amended.

Inventors: AOKERBLOM BENGT, AOKERBLOM, BENGT
Applicants: AKERBLOM BENGT, AOKERBLOM, BENGT
Application year: 1982
Main classification: B63H25
IPC codes: B63B1, B63B3, B63H25, B64C21