WO1994021914A2 - Flow body - Google Patents

Flow body Download PDF

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Publication number
WO1994021914A2
WO1994021914A2 PCT/EP1994/000848 EP9400848W WO9421914A2 WO 1994021914 A2 WO1994021914 A2 WO 1994021914A2 EP 9400848 W EP9400848 W EP 9400848W WO 9421914 A2 WO9421914 A2 WO 9421914A2
Authority
WO
WIPO (PCT)
Prior art keywords
flow body
side wall
hull
flow
wall parts
Prior art date
Application number
PCT/EP1994/000848
Other languages
French (fr)
Other versions
WO1994021914A3 (en
Inventor
Günter Pöschl
Original Assignee
Ppv Verwaltungs Ag
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Ppv Verwaltungs Ag filed Critical Ppv Verwaltungs Ag
Priority to AU64276/94A priority Critical patent/AU6427694A/en
Publication of WO1994021914A2 publication Critical patent/WO1994021914A2/en
Publication of WO1994021914A3 publication Critical patent/WO1994021914A3/en

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H25/00Steering; Slowing-down otherwise than by use of propulsive elements; Dynamic anchoring, i.e. positioning vessels by means of main or auxiliary propulsive elements
    • B63H25/44Steering or slowing-down by extensible flaps or the like
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H1/00Propulsive elements directly acting on water
    • B63H1/30Propulsive elements directly acting on water of non-rotary type
    • B63H1/36Propulsive elements directly acting on water of non-rotary type swinging sideways, e.g. fishtail type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/148Blades with variable camber, e.g. by ejection of fluid
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03BMACHINES OR ENGINES FOR LIQUIDS
    • F03B17/00Other machines or engines
    • F03B17/06Other machines or engines using liquid flow with predominantly kinetic energy conversion, e.g. of swinging-flap type, "run-of-river", "ultra-low head"
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/20Hydro energy
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Definitions

  • the invention relates to a flow body in accordance with the preamble of claim 1.
  • Such a flow body in form of a flap has already become known for use in an apparatus for utilizing hydromechani- cal energy from DE 34 40 499 Al, to which closer refe- rence is made below.
  • Flow bodies such as the hulls of ships can be guided du ⁇ ring their movement in the water by a rudder serving as a guiding apparatus.
  • a rudder serving as a guiding apparatus.
  • the flow impinges on the rudder, which leads to a unilateral in ⁇ crease of the flow resistance of the combination of hull and rudder, thus making the hull turn in the water.
  • the increase of the flow resistance leads to an un- desirable reduction of the speed and thus to a waste of kinetic energy.
  • the flow body In the apparatus known from the above-mentioned DE 34 40 499 Al the flow body usually stands inclined in a flowing watercourse.
  • the flow body substantially consists of a rotatable flap and a control fin swivellably attached at its end situated downstream, which forms a guiding appa ⁇ ratus.
  • the impingement of the flow on the flap and the control fin leads to a rotation thereof, which is used for generating energy.
  • the force is used for generating energy which is generated by the impingement of the flow on the flow body situated in ⁇ clined with respect to the flow.
  • the flow resistance pro ⁇ quizd by the flow body is relatively high, as in a rud- der, although only relatively little energy is obtained. Under low flow speeds, in particular, the apparatus does not have a particularly high efficiency.
  • the DE utility model 7802290 relates to a rudder or a fin which is attached as an annex to a body of a water or air vehicle.
  • the rudder consists of a carrying structure or an elastic skin encompassing the structure which limits a hollow chamber. By activating the rudder the skin is den- ted on one side in the manner of a airfoil wing and the opposite side is dented outwardly.
  • This known rudder has a lower flow resistance than usual rudders with rigid control surfaces. Nevertheless, this known rudder also leads to the fact that on displacing the rudder the whole flow resistance of the combination of body (i.e. flow body) and rudder is increased substantially and leads to an undesirable reduction in speed and thus to a waste of kinetic energy.
  • the flow body in accordance with the invention which is provided with a body with two opposite side wall parts, does not require a separate rudder as a guiding appara ⁇ tus.
  • the flow body Owing to the changeability of the shape of its outer side wall parts the flow body can be provided with an un- symmetrical shape by means of an adjusting device, which leads to a rotation of the whole body.
  • the body thus steers or guides itself in the water by the change of its shape per se and can be curved by the adjusting device as required, so that it maintains a shape beneficial to the flow and thus provides little resistance to the water.
  • the transition between shape-changeable side wall parts and non-shape-changeable side wall parts should al ⁇ ways be continuous, so that vortices will not arise and thus flow losses are kept to a minimum.
  • a novel guiding apparatus is integrated in the flow body by the invention and it is not attached like a rudder.
  • the guiding apparatus integrated in the flow body uses side wall parts of the hull of the flow body which are chan- geable in shape.
  • the adjusting device can be used to wi ⁇ den and constrict the inner hollow chamber differently, so that the flow body receives an unsymmetrical form with respect to its longitudinal axis and thus guides itself in the flow.
  • the flow resistance of the flow body is very low during the guidance, as a rudder or the like which is subject to impingement of the flow is avoided and becomes unnecessary.
  • the side wall parts are adjustable in such a way that the body is provided with practically conti- nuously adjustable different wing profiles. Owing to the arrangement of the flow body as a wing profile the flow resistance is reduced considerably.
  • the lifting effect of a wing profile is used for guidance.
  • the wing profile is provided with a right and a left side wall part with different curvatures. This re ⁇ sults in different pressures on the side wall parts of the wing profile in a flow, so that the shape of each side wall part results in a pressure or suction side of the wing profile, depending on the desired guiding direc ⁇ tion.
  • the pressure difference in the side wall parts of the flow body supports additionally the guiding movement of the flow body, which is a result of its unsymmetrical shape per se. In this way an easy guidability of the flow body with the lowest possible flow resistance is enabled in accordance with the invention.
  • the shape-changeable side wall parts may consist of seve ⁇ ral rigid parts composed in the manner of segments, which by means of a suitable adjusting device such as servomo ⁇ tors can form different overall shapes.
  • the shape-chan ⁇ geable side wall parts are flexible and thus the smoo ⁇ thest possible shape of the overall body is maintained in this manner.
  • the whole body in its entirety is shape-changeable. It is sufficient if there are shape-changeable side wall parts.
  • the flexible side wall parts could extend, for example, belt-like around the hull and be provided with a low height.
  • the shape-changeable side wall parts form the ou ⁇ ter sides of chambers which are parts of the body.
  • the adjusting device can expand and constrict the chambers in a different manner and thus form their outer sides diffe ⁇ rently.
  • the two chambers may be provided in the embodiment of the invention in accordance with claim 9 with at least one connecting conduit, through which the chamber content, preferably being air or, generally, any liquid, can flow from one chamber to the laterally opposite chamber. If the flow body is situated slightly inclined to the flow, the water presses the air from one chamber into the other and thus produces a shape change in the flow body and guides it.
  • the chamber content preferably being air or, generally, any liquid
  • a spoiler flap which is attached on the bow of the body in the embodiment of the invention in accordance with claim 11, can change the flow on the side wall parts additionally and facilitate the guidance, in particular when in the embodiment of the invention in accordance with claim 12 the flow is deflectable from one side wall part to the other side wall part.
  • the spoiler flap is arranged on the bow of the body and the shape-changeable side wall parts are arranged behind the spoiler flap, i.e., in the direction towards the end of the body; within the scope of the present invention, however, the reversed arrangement would also be possible.
  • the spoiler flap is provided so as to increase the flow resistance as little as possible, which is achieved in the embodiment of the invention in accordance with claim 13 in such a way that the spoiler flap consists of two opposite outer side wall parts which are preferably not changeable and which are movable in the body on actuating the spoiler flap in the embodiment of the invention in accordance with claim 14.
  • the flow body in accordance with the invention is used for utilizing hydromechanical energy or if it is used itself, for example, as a rudder with a low flow resi- stance of a common hull of a ship, the flow body is in possession of a rotational axis. Its position is ad ⁇ justable in the longitudinal direction of the cross sec ⁇ tion of the body in the embodiment in accordance with claim 20, so that the ratio of the forces acting, on the flow body in front of the rotational axis and behind the rotational axis is adjustable. The farther the rotational axis is arranged towards the body end, the easier it is to turn and guide it, but also the more unstable the flow body will be in the water.
  • the rotational axis is provided in the embodiment of the invention in accordance with claim 21 with adjustable stops so as to prevent a rotation by 180°, i.e., a com- plete turnover of the flow body.
  • adjustable stops so as to prevent a rotation by 180°, i.e., a com- plete turnover of the flow body.
  • This is arranged in the embodiment of the invention in accordance with claim 22 in such a way that the rotational axle is adjustable in the longitudinal direction of the body cross section in such a way that under a maximum rotational angle of the flow body there prevails on it an approximate balance of moments.
  • each side wall part is held axially di ⁇ placeable in a positive guiding means at the body end in the embodiment of the invention in ac ⁇ cordance with claim 23.
  • Fig. 1 shows a top view on a first embodiment of a flow body in accordance with the invention which is arranged as the hull of a ship;
  • Fig. 2 shows a cross-sectional view of a second embodi ⁇ ment of the flow body in accordance with the invention, in which it can be used for utili ⁇ zing hydromechanical energy in a river-run po- was plant;
  • Fig. 2a shows an end view along the line Ila-IIa in Fig. 2;
  • Fig. 3 shows the flow body in accordance with Fig. 2 in a side view
  • Fig. 3a shows the flow body in accordance with Fig. 2 in a front view,-
  • Fig. 3b shows a further embodiment of the flow body with several movable spoiler flaps
  • Fig. 4 shows the bow of the flow body in accordance with Fig. 2 as a detail on an enlarged scale,-
  • Fig. 4a shows the flow body in accordance with Fig. 2 with various positions of the actuated spoiler flap
  • Figs. 5a-5c show three successive phases of a rotation of the flow body in accordance with Fig. 2.
  • Fig. 1 shows a flow body in form of a hull 10 of a ship.
  • the hull 10 has a right and left side wall part 12 and 14, which are spaced apart from one another and which form a hollow chamber or inner chamber of the hull.
  • the side wall parts 12, 14 are arranged flexibly and are shape-changeable by means of an adjusting device 22 which is arranged in the hollow chamber and which is only sche ⁇ matically indicated in Fig. 1.
  • the side wall parts 12, 14 and the adjusting device 22 form in combination a stee- ring or guiding apparatus.
  • the adjusting device 22 consists of several hydraulic cylinders, of which only one is shown.
  • the ship is not provided with a rudder.
  • the side wall parts 12, 14 are adjusted by the adjusting device 22 in such a way that it results in a symmetrical cross-sectional pro ⁇ file with respect to a longitudinal plane A of hull 10.
  • the shape of the right side wall part is deformed inwardly in the direction of longitudinal plane A by an adjusting device allocated thereto and not shown in Fig. 1.
  • the adjusting device 22 allocated to the left side wall part 14 deforms it in such a way that the side wall part 14 is curved further outwardly.
  • the flow resi ⁇ stance of the unsymmetrically formed hull 10 is thus dif ⁇ ferent on both sides of longitudinal plane A and leads to the desired drive of the hull in a left curve. Even the smallest displacements of the side wall parts 12, 14 are sufficient for guiding the flow body without allowing it to change substantially its overall form which is benefi ⁇ cial to the flow.
  • the shape of hull 10 as shown in Fig. 2 is even more fa- vourable to the flow.
  • the flow body is provided here with a wing profile, i.e., it is curved stronger at its bow 20 and tapers towards the hull end 21 with a low curvature.
  • This flow body is used in the embodiment described herein for utilizing hydromechanical energy in a river-run power plant. It consists substantially of a hull 10 which con ⁇ sists at its bow 20 of non-shape-changeable rigid side walls and, adjacent thereto in the direction towards its hull end 21, of a shape-changeable right side wall part 12 and of a shape-changeable left side wall part 14.
  • a struc ⁇ ture 24 in the shape of a T-beam, provided with a short flange 25 and a long bridge 26 which is at a right angle thereto and which extends in the longitudinal plane A of hull 10.
  • Two chambers are laterally adjacent to bridge 26, i.e, a right and a left chamber 16 and 18, respecti ⁇ vely, which consist of foldable bellows and which are filled with air.
  • the outer sides of the chambers 16, 18 consist of shape-changeable side wall parts 12 and 14 which are made from flexible material. In the present case this is polycarbonate reinforced with glass fibres.
  • the side wall parts 12, 14 are held axially displaceably in a form-closed guiding means 50 provided on the hull end 21, which is clearly shown in Fig. 2a.
  • the guiding means 50 is arranged as a dovetail guiding means.
  • the adjusting device 22 is a connecting conduit in bridge 26, through which air can flow from one chamber into the other. Chambers 16, 18 themselves are hermeti ⁇ cally sealed with respect to the outside environment.
  • the adjusting device 22 is provided in addition to the connecting conduit 52 with a pneumatic or hydraulic pumping apparatus arranged additionally therein (depending on whether the chambers are filled with air or liquid) which pumps the air or liquid from one chamber to the other chamber and thus changes the shape of the side wall parts 12, 14.
  • the spoiler flap 30 for chan ⁇ ging the flow on the side wall parts 12, 14.
  • the spoiler flap 30 consists of two outer side wall parts which are situated opposite of one another and whose shape is non- changeable. These parts are a right side wall 32 and a left side wall 34 which are connected to one another through a toggle joint or lever 40 and which are jointly rotatable about a bow axle 38.
  • the side wall parts 12, 14 do not extend over the whole height of hull 10, but that they only form a kind of central part between the rigid parts 54, 56.
  • the chamber 18 is provided with a valve 57, through which both chambers 16, 18 are filled with air. Should the chambers 16, 18 fall below a certain minimum pressure after a prolonged operational period, air can be pumped in again through valve 57.
  • the side walls 32, 34 of the spoiler flap 30 also do not extend over the whole height of hull 10, as is shown in Fig. 3a. It is possible that the side walls 32, 34 themselves, as well as the side wall parts 12, 14 themselves, are subidivided into fixed and movable parts. The latter is shown in Fig.
  • Hull 10 is attached on part 54, which shows to ⁇ wards the water surface, to a rotational axle 42, through which the movement of the flow body in the water can be transmitted to the river-run power plant and can be con- verted into energy.
  • This movement of the flow body can be a translatory (into and out of the drawing plane of Fig. 3, for which a guiding means is provided which is not shown) and/or a rotary movement (about the rotational axle 42) and the rotational axle 42 may thus optionally serve as a rotary shaft.
  • a maximum angle of rotation . is adjustable by means of adjustable stops 44, 46 on the ro ⁇ tational axle 42, which angle lies between 15 and 25 de ⁇ grees so as to prevent a stall effect.
  • Fig. 4 shows the bow 20 of the flow body in greater de ⁇ tail.
  • the rotational axle 42 is attachable to part 54 in various axial positions and can thus be optimized in its position depending on the flow speed of the water.
  • the toggle joint 40 can be actuated via a control device in form of a hydraulic or pneumatic working cylinder 36 which is rotatably attached between the bow axle 38 and the toggle joint 40, as is clearly shown in the illustra ⁇ tions in Figs. 2, 4, 4a and 5c.
  • a locking bolt 58 which is connected to a piston rod of the working cylinder 36, extends between the toggle joint 40 and a leading surface 28 which is situated transversally to the hull 10 and which is formed by a front surface of the short flange 25 of the structure 24 showing towards the bow 20.
  • the loc ⁇ king bolt 58 snaps into a bore 59 in the leading surface 28 when it is aligned in the longitudinal plane A and thus prevents a movement of spoiler flap 30.
  • Fig. 4a shows two positions of the spoiler flap 30.
  • the spoiler flap 30 is allowed to rotate about the bow axle 38 including cylinder 38 and thus to set approximately in the direction of flow W (the position of the spoiler flap 30 turned to the right in Fig. 4a) .
  • the direction of the flow of the water is indicated in Figs. 5a-5c by an arrow W.
  • the toggle joint 40 is stretched (Fig. 2 or Fig. 4) and the side walls 32, 34 provide in combination with all other parts of the hull 10 the latter with the profile of a streamlined body which body has a low flow resistance.
  • the left side wall part 14 is flowed against by the water directly and compressed inwardly in the direction of longitudinal plane A.
  • the side wall part 12 becomes the suction side and the side wall part 14 becomes the pressure side of the flow body which was previously streamlined and which now has the form of an airfoil.
  • the part of the hull 10 situated behind the rotational axis 45 in the direction of the flow is thus subjected in Fig. 5a to a strong force which is directed to the right, which tends to turn the flow body counterclockwise. This force is the result, on the one hand, of the flow impinging on the left side wall part 14 and, on the other hand, of the pressure diffe ⁇ rence between side wall part 12 and 14.
  • a pumping apparatus or the like is not re ⁇ quired, because the flow which deforms the side wall part 14 automatically brings about the optimal wing foil pro ⁇ file by pressing the air into the right chamber 16 and also deforming the side wall part 12.
  • the adjusting de ⁇ vice 22 consists here only of the connecting conduit 52.
  • the force acting behind the rotational axle 42 and direc ⁇ ted to the right results in torque which is counterclock ⁇ wise.
  • This torque is opposed by clockwise torque which is a result of the force which acts on the flow body in front of the rotational axle 42.
  • the difference of these torques can be increased (rotational axle is situa ⁇ ted closer to bow 20) or, when the rotational axle 42 is situated in a centre of mass of the wing profile, it can be nearly balanced (rotational axle 42 is closer to hull end 21) .
  • the optimal position of the rotational axle 42 depends on the flow speed and of the type of the river- run power plant in which the flow body is used.
  • the leading chamber On incre ⁇ asing flow speed the leading chamber is curved in a more concave manner and the opposite chamber is curved more strongly in a convex manner. This leads to other wing profile shapes with other centre of mass positions.
  • the rotational axle 42 is connected to the hull 10 via an axially adjustable carriage 43. By means of adjustment of the carriage 43 the rotational axle 42 can follow the centre of mass displaced by change in profile. If the river-run power plant exclusively uses the rotational movement of the flow body, the rotational axle 42 is situated closer to the hull end 21.
  • the river-run power plant mainly uses the above-men ⁇ tioned translatory movement of the flow body, which is then transversally displaceable between the banks of a river
  • the rotational axle 42 is situated in the centre of mass, as is shown in Figs. 2 to 5c, i.e., on the flow body there is present a near balance of the moments and a maximum lateral force is applied to the rotational axle 42.
  • Fig. 5a the whole flow body, whose rotational axle 42 is held on a transversally displaceable carriage (not shown) , is subjected to a strong resultant force which is directed to the right.
  • the flow body thus moves transver ⁇ sally to the flow without rotating about the rotational axle 42.
  • the working cylinder 36 retracts its piston rod, the toggle joint 40 flips together and the side wall parts move towards one another and into hull 10, as is clearly shown in Figs. 2 and 5b.
  • the locking bolt 58 disengages from the bore 59 in the leading sur ⁇ face 28, the spoiler flap 30 is freely rotatable about the bow axle 38.
  • the spoiler flap 30 adjusts automati ⁇ cally to direction of flow W.
  • leading surface 28 which is curved in a slightly concave manner, is now subjected directly to the flow, there is a dynamic pressure between leading surface 28 and left side wall 34, so that the spoiler flap 30 is rotated further coun ⁇ terclockwise and is no longer precisely symmetrical in the direction of flow W, as is shown in Fig. 5.
  • the water, which would actually flow to the left side wall part 14 can flow to the side wall part 12 thorugh a gap 60 formed in hull 10 between the leading surface 28 and one end of the left side wall 34.
  • the water flowing through gap 60 leads to a break-off of the flow on the side wall part 12 and thus leads to a high drop in pres ⁇ sure.
  • the flow body begins to rotate counterclockwise.
  • Gap 60 thus closes again and the cylinder 36 is actuated again and nearly stretches toggle joint 40 through (as shown in Fig. 2) .
  • a right part of the leading surface 28 is again covered by the left side wall 34 and a left part of the leading surface 28, not yet covered, supports the rapid rotation of the flow body beyond the position which is precisely in the direction of flow W.
  • the volumes of the right and the left chamber 16 and 18 are balanced more and more during the rotation until finally the right chamber 16 has a smaller volume than the left chamber 18.
  • the loc- king bolt 58 Shortly after the flow body has rotated beyond a position which is precisely in the direction of flow W, the loc- king bolt 58 is again in the direction of longitudinal plane A and engages.
  • the flow body thus is provided with a shape and position which is mirrored to the representa ⁇ tion in Fig. 5a and thus rotates in its end position (Fig. 5c) which is limited by stops 44 and 46 on the ro- tational axle 42.
  • the flow body is subjected in this po ⁇ sition to a force directed to the left and moves back to the opposite bank, wherein the movement processes as ex ⁇ plained above take place in reversed order.
  • the spoiler flap 30 as shown in the position in Fig. 5c is actuated again, whe ⁇ reby the side walls 32 and 34 are moved towards each other again and into the hull 10.
  • the stops 44, 46 are adjustable for setting the maximum angle of rotation of the flow body, because in the case of an excessive inclined position of the flow body to the flow an excessive bending stress on the whole flow body may occur and thus stall might occur.
  • the bridge 26 may be part of the adjusting device 22.
  • the bridge for ex ⁇ ample, may be arranged in the manner of a "spine", na ⁇ mely, for example, as a chain of mutually supportive joints which can be controlled by two parallel cable li- nes in such a way that the bridge bends to the one or the other side, whereby it remains stable and may transmit forces.
  • spring-resilient bodies can be introduced which ensure that whenever the the cable lines transmit the same force on either side of the joint chain, said joints return to the neutral or initial posi ⁇ tion.
  • the flow body would be provided with the bow axle 38 as the swivelling axle and the spoiler flap 30 could be omitted.
  • a further probable embodiment of the adjusting device consists in the flow body in that the bridge 26 is provi ⁇ ded with a double wall and the intermediate space is fil ⁇ led with an electrostatic liquid which can be stiffened by applying a voltage.
  • the electrostatic liquid becomes rigid by the application of the voltage, it freezes like ice.
  • the bridge can be optionally made flexible or inflexible by applying a respective voltage.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Ocean & Marine Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
  • Steering Controls (AREA)

Abstract

A flow body with a hull (10) is provided with a steering or guiding apparatus consisting of shape-changeable side wall parts (12, 14) and an adjusting device (22) for adjusting the shape of the side wall parts (12, 14). The flow body is adjustable by the side wall parts (12, 14) with respect to its longitudinal plane (A) into an unsymmetrical, preferably wing profile shape, by which it becomes steerable. The side wall parts (12, 14) preferably consist of outer sides of opposed lateral chambers (16, 18) which are connected to one another. Different wing profiles are adjustable via different chamber volumes.

Description

FLOW BODY
Description
Technical Field
The invention relates to a flow body in accordance with the preamble of claim 1.
Background Art
Such a flow body in form of a flap has already become known for use in an apparatus for utilizing hydromechani- cal energy from DE 34 40 499 Al, to which closer refe- rence is made below.
Flow bodies such as the hulls of ships can be guided du¬ ring their movement in the water by a rudder serving as a guiding apparatus. By displacement of the rudder with respect to the longitudinal plane of the body the flow impinges on the rudder, which leads to a unilateral in¬ crease of the flow resistance of the combination of hull and rudder, thus making the hull turn in the water. The increase of the flow resistance, however, leads to an un- desirable reduction of the speed and thus to a waste of kinetic energy.
In the apparatus known from the above-mentioned DE 34 40 499 Al the flow body usually stands inclined in a flowing watercourse. The flow body substantially consists of a rotatable flap and a control fin swivellably attached at its end situated downstream, which forms a guiding appa¬ ratus. The impingement of the flow on the flap and the control fin leads to a rotation thereof, which is used for generating energy. In this known apparatus only the force is used for generating energy which is generated by the impingement of the flow on the flow body situated in¬ clined with respect to the flow. The flow resistance pro¬ duced by the flow body is relatively high, as in a rud- der, although only relatively little energy is obtained. Under low flow speeds, in particular, the apparatus does not have a particularly high efficiency.
The DE utility model 7802290 relates to a rudder or a fin which is attached as an annex to a body of a water or air vehicle. The rudder consists of a carrying structure or an elastic skin encompassing the structure which limits a hollow chamber. By activating the rudder the skin is den- ted on one side in the manner of a airfoil wing and the opposite side is dented outwardly. This known rudder has a lower flow resistance than usual rudders with rigid control surfaces. Nevertheless, this known rudder also leads to the fact that on displacing the rudder the whole flow resistance of the combination of body (i.e. flow body) and rudder is increased substantially and leads to an undesirable reduction in speed and thus to a waste of kinetic energy.
Disclosure of Invention
It is the object of the present invention to improve a flow body in accordance with the preamble of claim 1 in such a way that it becomes more easily steerable or guidable and nevertheless has a lower flow resistance and that by the steering or guiding less energy is consumed. Its use in utilizing hydromechanical energy is to provide the flow body with a higher efficiency.
The object is achieved in accordance with the invention by the features of claim 1.
The flow body in accordance with the invention, which is provided with a body with two opposite side wall parts, does not require a separate rudder as a guiding appara¬ tus. Owing to the changeability of the shape of its outer side wall parts the flow body can be provided with an un- symmetrical shape by means of an adjusting device, which leads to a rotation of the whole body. The body thus steers or guides itself in the water by the change of its shape per se and can be curved by the adjusting device as required, so that it maintains a shape beneficial to the flow and thus provides little resistance to the water. It is also possible to provide individual side wall parts with a changeable shape and to provide others non-chan- geably. The transition between shape-changeable side wall parts and non-shape-changeable side wall parts should al¬ ways be continuous, so that vortices will not arise and thus flow losses are kept to a minimum.
The principal difference of the invention with respect to the state of the art in accordance with the above-mentio¬ ned DE utility model 78 02 290 is that no rudder is atta- ched to the flow body in accordance with the invention. A novel guiding apparatus is integrated in the flow body by the invention and it is not attached like a rudder. The guiding apparatus integrated in the flow body uses side wall parts of the hull of the flow body which are chan- geable in shape. The adjusting device can be used to wi¬ den and constrict the inner hollow chamber differently, so that the flow body receives an unsymmetrical form with respect to its longitudinal axis and thus guides itself in the flow. The flow resistance of the flow body is very low during the guidance, as a rudder or the like which is subject to impingement of the flow is avoided and becomes unnecessary.
Preferable embodiments of the invention are formed by the subject matters of the subclaims.
In the embodiment of the invention in accordance with claims 2 and 3 the side wall parts are adjustable in such a way that the body is provided with practically conti- nuously adjustable different wing profiles. Owing to the arrangement of the flow body as a wing profile the flow resistance is reduced considerably.
In the embodiment of the invention in accordance with claim 4 the lifting effect of a wing profile is used for guidance. The wing profile is provided with a right and a left side wall part with different curvatures. This re¬ sults in different pressures on the side wall parts of the wing profile in a flow, so that the shape of each side wall part results in a pressure or suction side of the wing profile, depending on the desired guiding direc¬ tion. The pressure difference in the side wall parts of the flow body supports additionally the guiding movement of the flow body, which is a result of its unsymmetrical shape per se. In this way an easy guidability of the flow body with the lowest possible flow resistance is enabled in accordance with the invention.
The shape-changeable side wall parts may consist of seve¬ ral rigid parts composed in the manner of segments, which by means of a suitable adjusting device such as servomo¬ tors can form different overall shapes.
It is particularly advantageous if in the arrangement of the invention in accordance with claim 5 the shape-chan¬ geable side wall parts are flexible and thus the smoo¬ thest possible shape of the overall body is maintained in this manner. For the guidance of the flow body in accor- dance with the invention it is not required that the whole body in its entirety is shape-changeable. It is sufficient if there are shape-changeable side wall parts. The flexible side wall parts could extend, for example, belt-like around the hull and be provided with a low height.
In the embodiment of the invention in accordance with claim 6 the shape-changeable side wall parts form the ou¬ ter sides of chambers which are parts of the body. The adjusting device can expand and constrict the chambers in a different manner and thus form their outer sides diffe¬ rently.
This can be made in the embodiment of the invention in accordance with claim 8 by a pneumatic or hydraulic pum¬ ping apparatus.
The two chambers may be provided in the embodiment of the invention in accordance with claim 9 with at least one connecting conduit, through which the chamber content, preferably being air or, generally, any liquid, can flow from one chamber to the laterally opposite chamber. If the flow body is situated slightly inclined to the flow, the water presses the air from one chamber into the other and thus produces a shape change in the flow body and guides it.
A spoiler flap, which is attached on the bow of the body in the embodiment of the invention in accordance with claim 11, can change the flow on the side wall parts additionally and facilitate the guidance, in particular when in the embodiment of the invention in accordance with claim 12 the flow is deflectable from one side wall part to the other side wall part. For reasons of stabi¬ lity it is preferable when the spoiler flap is arranged on the bow of the body and the shape-changeable side wall parts are arranged behind the spoiler flap, i.e., in the direction towards the end of the body; within the scope of the present invention, however, the reversed arrangement would also be possible.
The spoiler flap is provided so as to increase the flow resistance as little as possible, which is achieved in the embodiment of the invention in accordance with claim 13 in such a way that the spoiler flap consists of two opposite outer side wall parts which are preferably not changeable and which are movable in the body on actuating the spoiler flap in the embodiment of the invention in accordance with claim 14.
If the flow body in accordance with the invention is used for utilizing hydromechanical energy or if it is used itself, for example, as a rudder with a low flow resi- stance of a common hull of a ship, the flow body is in possession of a rotational axis. Its position is ad¬ justable in the longitudinal direction of the cross sec¬ tion of the body in the embodiment in accordance with claim 20, so that the ratio of the forces acting, on the flow body in front of the rotational axis and behind the rotational axis is adjustable. The farther the rotational axis is arranged towards the body end, the easier it is to turn and guide it, but also the more unstable the flow body will be in the water.
The rotational axis is provided in the embodiment of the invention in accordance with claim 21 with adjustable stops so as to prevent a rotation by 180°, i.e., a com- plete turnover of the flow body. This is arranged in the embodiment of the invention in accordance with claim 22 in such a way that the rotational axle is adjustable in the longitudinal direction of the body cross section in such a way that under a maximum rotational angle of the flow body there prevails on it an approximate balance of moments.
To allow a change of the axial length of the side wall parts owing to the different shapes which the side wall parts can assume, at least one end of each side wall part is held axially diεplaceable in a positive guiding means at the body end in the embodiment of the invention in ac¬ cordance with claim 23.
Brief Description of Drawings
Embodiments of the flow body in accordance with the in¬ vention are described below in greater detail by refe¬ rence to the enclosed drawings, in which:
Fig. 1 shows a top view on a first embodiment of a flow body in accordance with the invention which is arranged as the hull of a ship; Fig. 2 shows a cross-sectional view of a second embodi¬ ment of the flow body in accordance with the invention, in which it can be used for utili¬ zing hydromechanical energy in a river-run po- wer plant;
Fig. 2a shows an end view along the line Ila-IIa in Fig. 2;
Fig. 3 shows the flow body in accordance with Fig. 2 in a side view;
Fig. 3a shows the flow body in accordance with Fig. 2 in a front view,-
Fig. 3b shows a further embodiment of the flow body with several movable spoiler flaps;
Fig. 4 shows the bow of the flow body in accordance with Fig. 2 as a detail on an enlarged scale,-
Fig. 4a shows the flow body in accordance with Fig. 2 with various positions of the actuated spoiler flap;
Figs. 5a-5c show three successive phases of a rotation of the flow body in accordance with Fig. 2.
Best Mode of Carrying Out the Invention
Fig. 1 shows a flow body in form of a hull 10 of a ship. The hull 10 has a right and left side wall part 12 and 14, which are spaced apart from one another and which form a hollow chamber or inner chamber of the hull. The side wall parts 12, 14 are arranged flexibly and are shape-changeable by means of an adjusting device 22 which is arranged in the hollow chamber and which is only sche¬ matically indicated in Fig. 1. The side wall parts 12, 14 and the adjusting device 22 form in combination a stee- ring or guiding apparatus. In Fig. 1 the adjusting device 22 consists of several hydraulic cylinders, of which only one is shown. The ship is not provided with a rudder. It is steered or guided in the water by the guiding appara- tus. During a straight ahead passage the side wall parts 12, 14 are adjusted by the adjusting device 22 in such a way that it results in a symmetrical cross-sectional pro¬ file with respect to a longitudinal plane A of hull 10. When hull 10 is to drive a curve to the left, the shape of the right side wall part is deformed inwardly in the direction of longitudinal plane A by an adjusting device allocated thereto and not shown in Fig. 1. Simulta¬ neously, the adjusting device 22 allocated to the left side wall part 14 deforms it in such a way that the side wall part 14 is curved further outwardly. The flow resi¬ stance of the unsymmetrically formed hull 10 is thus dif¬ ferent on both sides of longitudinal plane A and leads to the desired drive of the hull in a left curve. Even the smallest displacements of the side wall parts 12, 14 are sufficient for guiding the flow body without allowing it to change substantially its overall form which is benefi¬ cial to the flow.
The shape of hull 10 as shown in Fig. 2 is even more fa- vourable to the flow. The flow body is provided here with a wing profile, i.e., it is curved stronger at its bow 20 and tapers towards the hull end 21 with a low curvature. This flow body is used in the embodiment described herein for utilizing hydromechanical energy in a river-run power plant. It consists substantially of a hull 10 which con¬ sists at its bow 20 of non-shape-changeable rigid side walls and, adjacent thereto in the direction towards its hull end 21, of a shape-changeable right side wall part 12 and of a shape-changeable left side wall part 14. In the interior of the flow body there is arranged a struc¬ ture 24 in the shape of a T-beam, provided with a short flange 25 and a long bridge 26 which is at a right angle thereto and which extends in the longitudinal plane A of hull 10. Two chambers are laterally adjacent to bridge 26, i.e, a right and a left chamber 16 and 18, respecti¬ vely, which consist of foldable bellows and which are filled with air. The outer sides of the chambers 16, 18 consist of shape-changeable side wall parts 12 and 14 which are made from flexible material. In the present case this is polycarbonate reinforced with glass fibres. The side wall parts 12, 14 are held axially displaceably in a form-closed guiding means 50 provided on the hull end 21, which is clearly shown in Fig. 2a. The guiding means 50 is arranged as a dovetail guiding means. In Fig. 2 the adjusting device 22 is a connecting conduit in bridge 26, through which air can flow from one chamber into the other. Chambers 16, 18 themselves are hermeti¬ cally sealed with respect to the outside environment. When using the flow body in accordance with Fig. 2 as the hull of a ship, which is also possible, it is preferable when the adjusting device 22 is provided in addition to the connecting conduit 52 with a pneumatic or hydraulic pumping apparatus arranged additionally therein (depending on whether the chambers are filled with air or liquid) which pumps the air or liquid from one chamber to the other chamber and thus changes the shape of the side wall parts 12, 14.
On bow 20 there is arranged a spoiler flap 30 for chan¬ ging the flow on the side wall parts 12, 14. The spoiler flap 30 consists of two outer side wall parts which are situated opposite of one another and whose shape is non- changeable. These parts are a right side wall 32 and a left side wall 34 which are connected to one another through a toggle joint or lever 40 and which are jointly rotatable about a bow axle 38.
In the side view of the flow body in accordance with Fig. 3 it can be seen that the side wall parts 12, 14 do not extend over the whole height of hull 10, but that they only form a kind of central part between the rigid parts 54, 56. The chamber 18 is provided with a valve 57, through which both chambers 16, 18 are filled with air. Should the chambers 16, 18 fall below a certain minimum pressure after a prolonged operational period, air can be pumped in again through valve 57. The side walls 32, 34 of the spoiler flap 30 also do not extend over the whole height of hull 10, as is shown in Fig. 3a. It is possible that the side walls 32, 34 themselves, as well as the side wall parts 12, 14 themselves, are subidivided into fixed and movable parts. The latter is shown in Fig. 3b for the side wall part 12. This is subdivided into mo- vable side wall parts 12 and 12" and a fixed side wall part 13. Hull 10 is attached on part 54, which shows to¬ wards the water surface, to a rotational axle 42, through which the movement of the flow body in the water can be transmitted to the river-run power plant and can be con- verted into energy. This movement of the flow body can be a translatory (into and out of the drawing plane of Fig. 3, for which a guiding means is provided which is not shown) and/or a rotary movement (about the rotational axle 42) and the rotational axle 42 may thus optionally serve as a rotary shaft. A maximum angle of rotation . is adjustable by means of adjustable stops 44, 46 on the ro¬ tational axle 42, which angle lies between 15 and 25 de¬ grees so as to prevent a stall effect.
Fig. 4 shows the bow 20 of the flow body in greater de¬ tail. The rotational axle 42 is attachable to part 54 in various axial positions and can thus be optimized in its position depending on the flow speed of the water. The toggle joint 40 can be actuated via a control device in form of a hydraulic or pneumatic working cylinder 36 which is rotatably attached between the bow axle 38 and the toggle joint 40, as is clearly shown in the illustra¬ tions in Figs. 2, 4, 4a and 5c. A locking bolt 58, which is connected to a piston rod of the working cylinder 36, extends between the toggle joint 40 and a leading surface 28 which is situated transversally to the hull 10 and which is formed by a front surface of the short flange 25 of the structure 24 showing towards the bow 20. The loc¬ king bolt 58 snaps into a bore 59 in the leading surface 28 when it is aligned in the longitudinal plane A and thus prevents a movement of spoiler flap 30.
Fig. 4a shows two positions of the spoiler flap 30. When the cylinder 36 is actuated and the locking bolt 58 di¬ sengages from the bore 59 (central position of spoiler flap 30 in Fig. 4a) , the spoiler flap 30 is allowed to rotate about the bow axle 38 including cylinder 38 and thus to set approximately in the direction of flow W (the position of the spoiler flap 30 turned to the right in Fig. 4a) .
The function of the flow body shall be explained below by reference to Fig. 4 and Figs. 5a to 5c.
The direction of the flow of the water is indicated in Figs. 5a-5c by an arrow W. At the beginning of the mo¬ vement of the flow body it is aligned inclined to the di¬ rection of flow W and the spoiler flap 30 is not ac- tuated, i.e., the toggle joint 40 is stretched (Fig. 2 or Fig. 4) and the side walls 32, 34 provide in combination with all other parts of the hull 10 the latter with the profile of a streamlined body which body has a low flow resistance. Owing to the inclined position of the flow body in accordance with Fig. 5a, the left side wall part 14 is flowed against by the water directly and compressed inwardly in the direction of longitudinal plane A. This leads to a concave shape of the side wall part 14. The volume of the left chamber 18 is thus reduced. The air thus displaced flows through the connecting conduit 52 into the right chamber 16 and increases its volume. As the structure 24 is rigid, the increase in the volume can only be brought about in that the right side wall part 12 deforms outwardly in a convex manner and is curved more strongly convexly than is the case in a position of the flow body precisely in the direction of the flow W, as is shown in Fig. 2. The fact that the right side wall part 12 is provided with a convex curvature and the left side wall part 14 is provided with a concave curvature results in different flow speeds on both side wall parts 12, 14. The side wall part 12 becomes the suction side and the side wall part 14 becomes the pressure side of the flow body which was previously streamlined and which now has the form of an airfoil. The part of the hull 10 situated behind the rotational axis 45 in the direction of the flow is thus subjected in Fig. 5a to a strong force which is directed to the right, which tends to turn the flow body counterclockwise. This force is the result, on the one hand, of the flow impinging on the left side wall part 14 and, on the other hand, of the pressure diffe¬ rence between side wall part 12 and 14. Between chambers 16 and 18 a pumping apparatus or the like is not re¬ quired, because the flow which deforms the side wall part 14 automatically brings about the optimal wing foil pro¬ file by pressing the air into the right chamber 16 and also deforming the side wall part 12. The adjusting de¬ vice 22 consists here only of the connecting conduit 52.
The force acting behind the rotational axle 42 and direc¬ ted to the right results in torque which is counterclock¬ wise. This torque is opposed by clockwise torque which is a result of the force which acts on the flow body in front of the rotational axle 42. Depending on the axial position of the rotational axle 42 the difference of these torques can be increased (rotational axle is situa¬ ted closer to bow 20) or, when the rotational axle 42 is situated in a centre of mass of the wing profile, it can be nearly balanced (rotational axle 42 is closer to hull end 21) . The optimal position of the rotational axle 42 depends on the flow speed and of the type of the river- run power plant in which the flow body is used. On incre¬ asing flow speed the leading chamber is curved in a more concave manner and the opposite chamber is curved more strongly in a convex manner. This leads to other wing profile shapes with other centre of mass positions. For optimal positioning the rotational axle 42 is connected to the hull 10 via an axially adjustable carriage 43. By means of adjustment of the carriage 43 the rotational axle 42 can follow the centre of mass displaced by change in profile. If the river-run power plant exclusively uses the rotational movement of the flow body, the rotational axle 42 is situated closer to the hull end 21. If, howe- ver, the river-run power plant mainly uses the above-men¬ tioned translatory movement of the flow body, which is then transversally displaceable between the banks of a river, the rotational axle 42 is situated in the centre of mass, as is shown in Figs. 2 to 5c, i.e., on the flow body there is present a near balance of the moments and a maximum lateral force is applied to the rotational axle 42. In Fig. 5a the whole flow body, whose rotational axle 42 is held on a transversally displaceable carriage (not shown) , is subjected to a strong resultant force which is directed to the right. The flow body thus moves transver¬ sally to the flow without rotating about the rotational axle 42.
When the flow body is to be rotated, for example when it has reached a bank and is to move back to the opposite bank, the working cylinder 36 retracts its piston rod, the toggle joint 40 flips together and the side wall parts move towards one another and into hull 10, as is clearly shown in Figs. 2 and 5b. As soon as the locking bolt 58 disengages from the bore 59 in the leading sur¬ face 28, the spoiler flap 30 is freely rotatable about the bow axle 38. The spoiler flap 30 adjusts automati¬ cally to direction of flow W. As, however, the leading surface 28, which is curved in a slightly concave manner, is now subjected directly to the flow, there is a dynamic pressure between leading surface 28 and left side wall 34, so that the spoiler flap 30 is rotated further coun¬ terclockwise and is no longer precisely symmetrical in the direction of flow W, as is shown in Fig. 5. In this way the water, which would actually flow to the left side wall part 14, can flow to the side wall part 12 thorugh a gap 60 formed in hull 10 between the leading surface 28 and one end of the left side wall 34. The water flowing through gap 60 leads to a break-off of the flow on the side wall part 12 and thus leads to a high drop in pres¬ sure. The flow body begins to rotate counterclockwise. Gap 60 thus closes again and the cylinder 36 is actuated again and nearly stretches toggle joint 40 through (as shown in Fig. 2) . A right part of the leading surface 28 is again covered by the left side wall 34 and a left part of the leading surface 28, not yet covered, supports the rapid rotation of the flow body beyond the position which is precisely in the direction of flow W. The volumes of the right and the left chamber 16 and 18 are balanced more and more during the rotation until finally the right chamber 16 has a smaller volume than the left chamber 18. Shortly after the flow body has rotated beyond a position which is precisely in the direction of flow W, the loc- king bolt 58 is again in the direction of longitudinal plane A and engages. The flow body thus is provided with a shape and position which is mirrored to the representa¬ tion in Fig. 5a and thus rotates in its end position (Fig. 5c) which is limited by stops 44 and 46 on the ro- tational axle 42. The flow body is subjected in this po¬ sition to a force directed to the left and moves back to the opposite bank, wherein the movement processes as ex¬ plained above take place in reversed order. As soon as the flow body is to rotate again, the spoiler flap 30 as shown in the position in Fig. 5c is actuated again, whe¬ reby the side walls 32 and 34 are moved towards each other again and into the hull 10.
The stops 44, 46 are adjustable for setting the maximum angle of rotation of the flow body, because in the case of an excessive inclined position of the flow body to the flow an excessive bending stress on the whole flow body may occur and thus stall might occur.
In extremely long flow bodies several adjacent chambers 16, 18 are preferable.
In a further embodiment of the flow body, which is not shown in the drawings, the bridge 26 may be part of the adjusting device 22. For this purpose the bridge, for ex¬ ample, may be arranged in the manner of a "spine", na¬ mely, for example, as a chain of mutually supportive joints which can be controlled by two parallel cable li- nes in such a way that the bridge bends to the one or the other side, whereby it remains stable and may transmit forces. Between the joints spring-resilient bodies can be introduced which ensure that whenever the the cable lines transmit the same force on either side of the joint chain, said joints return to the neutral or initial posi¬ tion. In this case the flow body would be provided with the bow axle 38 as the swivelling axle and the spoiler flap 30 could be omitted.
A further probable embodiment of the adjusting device consists in the flow body in that the bridge 26 is provi¬ ded with a double wall and the intermediate space is fil¬ led with an electrostatic liquid which can be stiffened by applying a voltage. The electrostatic liquid becomes rigid by the application of the voltage, it freezes like ice. In this manner the bridge can be optionally made flexible or inflexible by applying a respective voltage.

Claims

Claims
1. A flow body, in particular for a river-run power plant for utilizing hydromechanical energy, with a hull (10) and a guiding apparatus for guiding the flow body in the water, characterized in that the guiding apparatus consists of shape-changeable side wall parts (12, 14) which outwardly limit at least one inner hollow chamber of the hull (10) and of an adjusting device (22) for ad- justing the shape of the side wall parts (12, 14) .
2. The flow body as claimed in claim 1, characterized in that the shape of the side wall parts (12, 14) is ad¬ justable by means of the adjusting device (22) in such a way that the hull (10) is provided with a wing profile.
3. The flow body as claimed in claim 1 or 2, characte¬ rized in that different wing profiles are adjustable with the side wall parts (12, 14) .
4. The flow body as claimed in claim 2 or 3, characte¬ rized in that by the shape of each side wall part (12, 14) one side of the wing profile can be arranged as the pressure side and the other side as suction side, and vice-versa.
5. The flow body as claimed in one of the claims 1 to 4, characterized in that the shape-changeable side wall parts (12, 14) are flexible.
6. The flow body as claimed in claim 5, characterized in that the hollow chamber of the hull (10) is provided with at least two opposed lateral chambers (16, 18) whose respective outer sides consist of shape-changeable side wall parts (12, 14) and that the adjusting device (22) may expand or constrict the chambers (16, 18) in a diffe¬ rent manner.
7. The flow body as claimed in claim 6, characterized by a symmetrical T-beam-like structure (24), with.a short flange (25) and a long bridge (26) which is situated at a right angle thereto and which extends in a longitudinal plane (A) of the hull (10) between the chambers (16, 18) .
8. The flow body as claimed in claim 7, characterized in that the adjusting device (22) is provided with at least one pneumatic or hydraulic pumping apparatus.
9. The flow body as claimed in one of the claims 6 to
8, characterized in that the adjusting device (22) for adjusting the shape of the shape-changeable side wall parts (12, 14) is provided with a connecting conduit (52) between the opposed lateral chambers (16, 18) .
10. The flow body as claimed in one of the claims 6 to
9, characterized in that the chambers (16, 18) consist of folding bellows.
11. The flow body as claimed in one of the claims 1 to
10, characterized in that at least one spoiler flap (30) is provided on the bow (20) of the hull (10) for changing the flow on the side wall parts (12, 14) .
12. The flow body as claimed in claim 11, characterized in that the spoiler flap (30) is swivellable about at least one bow axle (38) , so that the flow is deflectable from the one side of the hull (10) through the hull (10) to the other side wall part (12, 14) on the other side of the hull (10) .
13. The flow body as claimed in claim 11 or 12, charac¬ terized in that the spoiler flap (30) consists of two op¬ posed outer side walls (32, 34) .
14. The flow body as claimed in claim 13, characterized in that the side wall parts (32, 34) are swivellable to¬ wards one another and away from one another about the bow axle (38) .
15. The flow body as claimed in one of the claims 11 to 14, characterized by a control device (36) for swivelling the spoiler flap (30) .
16. The flow body as claimed in claim 15, characterized in that the side walls (32, 34) are connected via a tog¬ gle joint (40) to one another which is actuatable through the control device (36) .
17. The flow body as claimed in claim 15 or 16, charac¬ terized in that the control device (36) comprises a hydraulic or pneumatic working cylinder.
18. The flow body as claimed in claim 5, characterized in that the shape-changeable side wall parts (12, 14) of the hull (10) consist of polycarbonate reinforced by glass fibres.
19. The flow body as claimed in one of the claims 11 to 17, characterized by a leading surface (28) arranged transversal to the hull (10) behind the spoiler flap (30) , which surface can be flowed on when the spoiler flap (30) is actuated.
20. The flow body as claimed in one of the claims 1 to 19, characterized in that the hull (10) is attached to a rotational axle (42) whose position is adjustable in the longitudinal direction of its cross section.
21. The flow body as claimed in claim 20, characterized in that stops (44) which are adjustable on the rotational axle (42) are attached in such a way that owing to these a maximum angle of rotation α. of the hull (10) is ad- justable.
22. The flow body as claimed in claim 20 or 21, charac¬ terized in that the rotational axle (42) is adjustable in the longitudinal direction of the cross section of the hull (10) in such a way that an approximate balance of moments prevails in the flow body at a maximum angle of rotation α- of the hull (10) .
23. The flow body as claimed in one of the claims 1 to
22, characterized in that the shape-changeable side wall parts (12, 14) at the end (21) of the hull (10) are dis¬ placeable in a positive guiding means (50) .
PCT/EP1994/000848 1993-03-19 1994-03-17 Flow body WO1994021914A2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AU64276/94A AU6427694A (en) 1993-03-19 1994-03-17 Flow body

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DEP4308892.9 1993-03-19
DE4308892A DE4308892C2 (en) 1993-03-19 1993-03-19 Flow body

Publications (2)

Publication Number Publication Date
WO1994021914A2 true WO1994021914A2 (en) 1994-09-29
WO1994021914A3 WO1994021914A3 (en) 1994-11-24

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WO (1) WO1994021914A2 (en)
ZA (1) ZA941800B (en)

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WO1994021914A3 (en) 1994-11-24
AU6427694A (en) 1994-10-11
DE4308892C2 (en) 1997-01-09
DE4308892A1 (en) 1994-09-22
ZA941800B (en) 1994-10-26

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