TURBINE WITH FLOW DIVERTER AND FLOW DIVERTER FOR TURBINES

Abstract

A turbine (1) with flow diverter (2) comprises a support frame (25) adapted to be anchored to a fixed or movable structure, an impeller (3) rotatably mounted about a rotation axis (R) to the support frame (25) and having a front inlet section for the flow and a plurality of blades (4, 4′, 4″, . . . ) adapted to move continuously upon the rotation produced by the flow between a pushing position and an advancing position in correspondence of the front section, a main flow diverter (2) adapted to be anchored to the support frame (25) and having a peripheral wall (7) adapted to at least partially blind the front section with respect to the flow auxiliary diverter (13) extending from a first section (14) facing one or more blades (4′) in the advancing position to a second section (15) facing one or more blades (4) in pushing position. The auxiliary diverter (13) comprises a plurality of substantially curvilinear conduits (16) in reciprocal side by side position along a substantially radial direction, each conduit (16) having a first opened end (16′) facing the blades (4′) in the advancing position and a second opened. end (16″, 16′″) placed in correspondence of the conveying duet (8).

Claims

1. A turbine (1) with flow diverter (2), comprising: a support frame (25) adapted to be anchored to a fixed or movable structure; an impeller (3) rotatably mounted about a rotation axis (R) to said support frame (25) and having a front inlet section for the flow and a plurality of blades (4, 4′, 4″, . . . ) adapted to move continuously upon the rotation produced by the flow between a pushing position and an advancing position in correspondence of said front section; a main flow diverter (2) adapted to be anchored to said support frame (25) and having a peripheral wall (7) adapted to at least partially blind said front section with respect to the flow; an auxiliary diverter (13) extending from a first section (14) facing one or more blades (4′) of said plurality in said advancing position to a second section (15) facing one or more blades (4) of said plurality in said pushing position; characterized in that said auxiliary diverter (13) comprises a plurality of substantially curvilinear conduits (16) in reciprocal side by side position along a substantially radial direction, each of said conduits (16) having a first opened end (16′) facing the blades (4′) of said plurality in the advancing position and a second opened end (16″, 16′″) placed in correspondence of said conveying duct (8).

2. Turbine as claimed in claim 1, characterized in that said curvilinear conduits (16) are adapted to at least partially return the operating fluid from said first inlet section (14) of the flow bad(to said second output section (15) to allow the entering of the flow returning from the advancing blades (4′) through said first ends (16′) and the feeding thereof toward said pushing blades (4) through said second ends (16″) to increase the torque produced by the flow on said impeller (3).

3. Turbine as claimed in claim 2, characterized in that said main diverter (2) comprises a main conveying duct (8) for the working fluid having a flow inlet port (9) and a flow outlet port (10) facing one or more blades (4) of said plurality in said pushing position.

4. Turbine as claimed in claim 1, characterized in that said main conveying duct (8) substantially converges toward said outlet port (10) to narrow the section for the passage of the flow toward said impeller (3) and increase the speed of the fluid.

5. Turbine as claimed in claim 4, characterized in that said conveying duct (8) comprises a substantially planar or slightly concave first deflection side wall (17) and a second deflection side wall (18) facing said first side wall (17).

6. Turbine as claimed in claim 5, characterized in that said second side wall (18) has a convexity outwardly or inwardly directed with an outlet edge (12) radially staggered and decentered with respect of said rotation axis (R) to allow the inlet fluid to at least partially hit also one or more blades (4′) in the return position.

7. Turbine as claimed in claim 6, characterized in that said outlet section (15) is in fluidic communication with said conveying duct (8).

8. Turbine as claimed in claim 7, characterized in that said second ends (16″) of said curvilinear conduits are directly opened into said main conveying duct (8).

9. Turbine as claimed in claim 6, characterized in that said curvilinear conduits (16) are adapted to allow the flow to enter from said second section (15) to be sent toward said blades (4′) in advancing position through said first section (14) and said first ends (16′).

10. Turbine as claimed in claim 9, characterized in that said side conduits (16) have inlet edges (36) having a distance from said axis of rotation (R) decreasing along the direction going from the side conduit (16) closer to said main conveying duct (8) toward the farthest.

11. Turbine as claimed in claim 9, characterized in that said auxiliary diverter (13) comprises a return side duct (37) adapted to receive the flow produced by the rear blades (4′″) to canalize it toward said blades (4′) in advancing position.

12. Turbine as claimed in claim 1, characterized in that said main diverter (2) comprises a side conveying duct (33) opposite to said auxiliary diverter (13) with respect of said main conveying duct (8) and having an outlet (35) facing respective blades (4″) in advancing position.

13. Turbine as claimed in claim 12, characterized in that said main diverter (2) comprises an anchoring frame (21) having an upper transverse element (22) and a lower transverse element (23) for the rigid connection of said side deflection walls (17, 18) and means (27) for the rotatable connection of said flow diverter (2) to said support frame (25), said rotatable connection means (27) being adapted to allow the rotation of said main diverter (2) about a central axis (C) substantially coaxial with said rotation axis (R) in an independent manner with respect to the rotation of said impeller (3).

14. Turbine as claimed in claim 1, characterized in that said conveying duct (8) houses thereinside a plurality of deflecting elements (29) each having a laminar or profiled body with a corresponding wing profile, said deflection elements (29) being at least partially overlapping and radially staggered with each other to divert the flow lines and slow down the flow direct to the blades (4′) in advancing position.

15. (canceled)

Description

BRIEF DISCLOSURE OF THE DRAWING

[0048] Further features and advantages of the invention will become more apparent in light of the detailed description of some preferred but not exclusive embodiments of a turbine with flow diverter according to the invention, illustrated by way of non-limiting examples with the aid of the accompanying drawings, wherein:

[0049] FIG. 1 is a schematic cross-sectional view of a turbine of the invention in a first preferred embodiment;

[0050] FIG. 2 is a schematic cross-sectional view of a first variant of the turbine of FIG. 1;

[0051] FIG. 3 is a schematic cross-sectional view of a second variant of the turbine of FIG. 1;

[0052] FIG. 4 is a schematic cross-sectional view of a third variant of the turbine of FIG. 1,

[0053] FIG. 5 is a schematic cross-sectional view of a turbine in a second preferred embodiment;

[0054] FIG. 6 is a schematic cross-sectional view of a turbine in a third preferred embodiment;

[0055] FIG. 7 is a schematic cross-sectional view of a first variant of the turbine of FIG. 6;

[0056] FIG. 8 is a schematic cross-sectional view of a second variant of the turbine of FIG. 6;

[0057] FIG. 9 is a schematic cross-sectional view of a turbine of the invention in a fourth preferred embodiment;

[0058] FIG. 10 is a front view of the turbine of FIG. 9;

[0059] FIG. 11 is a top view of the turbine of FIG. 9;

[0060] FIG. 12 is a cross-sectional view of the turbine of FIG. 9;

[0061] FIG. 13 is a perspective view of a turbine provided with a flow diverter according to a fifth preferred embodiment.

BEST MODES OF CARRYING OUT THE INVENTION

[0062] With reference to the accompanying figures a turbine provided with flow diverter is shown, which turbine according to a first type of application may be used in a preferred but not limiting way in home applications or in small premises for commercial and industrial uses, in particular for micro wind or micro hydro applications.

[0063] However, the turbine according to the present invention may also find application by immersion within pipelines or water conduits and in systems for the energy recovery from either rivers or marine currents, tidal power and the like, as will also be explained hereinafter.

[0064] FIG. 1 schematically illustrates a first preferred but not exclusive configuration of a turbine according to the invention, generally indicated by 1, which essentially comprises a main flow diverter 2 and an impeller 3 rotatably mounted around a central axis of rotation R on a support frame, not shown in this figure, which can be anchored in turn to a fixed or movable structure, also not illustrated.

[0065] In a known manner, the impeller 3 will have a plurality of blades 4, 4′, 4″, 4′″ integral with each other to rotate upon the action of the fluid so that from time to time at least one blade 4 is in the pushing position with respect to a front section designed for the entering of the flow, i.e. in the position in which it is invested by the main flow (whose feed direction is indicated by arrows) to produce the rotation of the central axis R.

[0066] At the same time one or more additional blades 4′ will be in an advancing position, i.e., in a position in which they are not directly hit by the main flow.

[0067] The blades 4, 4′, 4″, 4′″ may be mutually separated or defined by a suitably shaped single body with a central stem 5 defining the axis of rotation R and from which the concave surfaces 6, 6′, 6″, 6′″ which the flow acts on in the pushing phase extend, to generate a torque adapted to produce the rotation of the impeller 3.

[0068] The flow diverter 2 will be anchored in a fixed or removable manner to the support frame by means of suitable connection means, also not shown in this figure.

[0069] In a particular configuration, the connection means will be of the rotary type to allow the rotation of the diverter 2 around a central axis C coaxial to the axis of rotation R of the impeller 3 in an independent manner with respect to the latter.

[0070] For some applications, such as in the case in which the turbine 1 operates by immersion in water pipes, for example in so-called mini-hydro applications, the diverter 2 may be connected to the frame of the turbine 1 or directly to an outer support structure in a fixed manner, so as to intercept the current always according to the main direction of flow.

[0071] The diverter 2 will comprise a supporting frame, not illustrated, which will be provided with the aforesaid connecting means, possibly of the rotary type, as well as a peripheral wall 7 which extends peripherally to the impeller 3 so as to at least partially occlude the front section.

[0072] Preferably, the side wall 7 will have axial extension greater than the axial dimension of the blades 4, 4′, 4″, 4′″ of the impeller 3 to allow the accelerated current to invest completely these latter and ensure a uniform effect over the entire axial development of the impeller 3. The peripheral wall 7 comprises a main conveying conduit 8 adapted to convey the working fluid toward the impeller 3. The main duct 8 has an outer inlet port 9 for the fluid and an inner outlet port 10 facing the blade 4 of the impeller 3 which in turn is located in the pushing position for sending the accelerated flow thereto.

[0073] The main conveying duct 8 will extend preferably for the whole axial development of the peripheral wall 7 and will have edges 11, 12 facing one another and converging towards the central axis C to restrict the passage section of the flow towards the blades 4 of the impeller 3 and to increase the speed thereof and consequently the spin number.

[0074] In the case in which means are provided for rotatable and independent connection, such means may be suitably designed to allow the diverter 2 to remain always in the optimum position of operation, corresponding to the position in which the outlet section 10 of the flow is frontal and axially aligned with respect to the primary direction of the flow, to have always maximum flow of the fluid toward the impeller 3.

[0075] The remaining part of the peripheral wall 7 may be partially or totally closed or totally open, as illustrated in the figures.

[0076] The flow diverter 2 also comprises an auxiliary diverter 13 that extends from an inlet section 14 which faces the advancing blade 4′ to an outlet section 15 in fluid communication with the main conveying duct 8.

[0077] In this first configuration, the auxiliary diverter 13 is adapted to return at least partially the working fluid hitting the advancing blade 4′ toward the blade 4 in the pushing position in order to exploit a greater amount of fluid and further increase the torque produced by the flow on the impeller 3.

[0078] The auxiliary diverter 13 is suitably formed by a plurality of return conduits of the flow, generally indicated by 16, each having a first open end 16′ facing the blade 4′ in the advancing position and able to allow the entrance of the flow returning from the same blade 4′ and a second open end 16″ placed in correspondence of the main conveying conduit 8. Then, the second open ends 16″ of the curvilinear conduits 16 will be suitable to bring the fluid back to the main conveying duct 8 in order to return on the blades in the pushing position 4.

[0079] The return conduits 16 are substantially curvilinear, mutually side by side along a direction substantially radial and preferably narrowing towards the outlet section 15 to increase the speed of the flow.

[0080] The radius of curvature r of the conduits 16 may have any values without any particular limitations and is preferably not too narrow, with central angles greater than 45° to avoid the occurrence of phenomena of compression of the fluid with possible onset of turbulent motion. From the same FIG. 1 it is observed that the main conveying duct 8 comprises a first side wall 17 and a second deflection side wall 18 facing each other and converging towards the outlet port 10, so as to obtain the acceleration of the flow.

[0081] The first wall 17 is substantially flat with a maximum angle α with respect to a median plane π passing through the central axis C and substantially parallel to the input direction of the main flow between 10° and 35°, so as to not create compression zones of the fluid.

[0082] In turn, the second wall 18 has convexity directed outwards and angle β reduced in correspondence with its outlet edge 12, again in order to avoid compression of the fluid. Moreover, the outlet edge 12 of the second wall 18 will be radially staggered and offset from the axis of rotation R so that the outlet port 10 of the main conveying duct 8 is wider than the radius of the impeller 3 to allow the flow entering the impeller 3 to invest at least partially also the blade 4′ in the advancing position.

[0083] FIG. 2 shows a particular variant of the turbine 1 of FIG. 1, wherein the main conveying duct 8 has a greater convergence to define a greater narrowing and increase the effect of acceleration of the flow, with the return ducts 16 which in turn show a more accentuated curvature.

[0084] In both variants illustrated above it is observed that the output sections 15 of the return conduits 16 are in fluid communication with the conveying conduit 8.

[0085] In particular, the second ends 16″ of the curvilinear conduits 16 are open directly into the conveying duct 8.

[0086] FIG. 3 shows a second variant of the turbine 1 described above, but differs from it, as well as for the shape of the impeller 3, however not limiting for the scope of protection of the present invention, for a different form of the return conduits 16 which define the auxiliary diverter 13, now having a double curvature.

[0087] In this configuration the auxiliary diverter 13, and consequently the return conduits 16, are not placed directly in fluid communication with the main conveying duct 8 but its output section 15, defined by the second open ends 16″ of the conduit 16, faces the blade 4 in the pushing position to send the recovered flow directly thereto keeping them substantially separated from the main flow.

[0088] Furthermore, the second deflection side wall 18 entirely covers the blade 4′ in the advancing position.

[0089] FIG. 4 shows a variant of the previous configuration in which the second side wall 18 has an end portion 18′ outwardly concave to divert the main flow and facilitate the entry of side flows.

[0090] FIG. 5 shows a third configuration of a turbine 1 according to the invention which has a further configuration of the impeller 3 funned by a plurality of blades 4, 4′, 4″ with a convex profile and a relatively small diameter to have reduced friction in the advancing step and wherein the main conveying duct 8 has a relatively narrow outlet port 10 on the load-bearing part of the blade 4 in the pushing position to increase significantly the speed of the flow.

[0091] FIG. 6 shows a fourth configuration of the turbine 1 wherein the auxiliary diverter 13 is adapted to intercept the main flow and to allow it to enter the ducts 16 to send it from the second curvilinear section 15 to the blades 4′ in the advancing position through the first section 14 and the first open ends 16′ of the curvilinear conduits 16.

[0092] There is also a side conveying duct 33 placed opposite to the auxiliary diverter 13 relative to the main diverter 2 and having an inlet 34 substantially close to the input section of the main conveying duct 8 and an outlet 35 facing to further blades 4″ in advancing position and in particular to the blades 4″ moving away from the pushing position.

[0093] The conveying ducts 8, 16 are sized so that the respective inlet edges 36 for the flow have a distance relative to the axis of rotation R which decreases in the direction going from the main conveying duct 8 to the outer curved conduit 16.

[0094] In this way each conveying conduit 16 may exploit the effect of speed increase of the flow that is generated in correspondence with the input edges 36.

[0095] FIG. 7 shows a first variant of this last configuration in which a lateral return conduit 37 adapted to receive the flow produced by the rear blades 4′″ is diametrically opposite to the side conveying duct 33 to channel it toward the blades 4′ in the advancing position. The input edges 36 are shown with non decreasing distances but may still be configured as shown in FIG. 6.

[0096] FIG. 8 shows a variant of FIG. 7 which essentially differs for a greater radius of curvature of the blades 4, 4′.

[0097] FIG. 9 shows in a partial way a fifth configuration of the turbine 1 according to the invention provided with an impeller 3, which in the figure is of the Helical Savonius type but which may also be different, and of the flow diverter 2 for which the auxiliary diverter 13 is not shown.

[0098] In this figure it is also noted that the impeller 3 is closed at the axial ends by an upper disc 19 and by a lower disc 20 which will connect the impeller 3 to the support frame.

[0099] In particular, in this configuration, as well as in the configuration of FIG. 1, the diverter 2 may be or not equipped with the auxiliary diverter 13, as the particular configuration of the conveyor duct 8 will still allow to obtain an advantageous effect of increase of torque because the compression zones of the fluid on the side deflection walls 17, 18 will be reduced also obtaining the above-mentioned pulling effect on the advancing blade 4′.

[0100] In this figure the conveying duct 8 is provided with an anchoring frame 21 having an upper transverse element 22 and a lower transverse element 23 substantially planar for the rigid connection of the two deflection side walls 17, 18.

[0101] Also in this case the second side wall 18 will be sized so as to uncover at least part of the blade 4′ in the advancing position along the inlet direction of the fluid toward the impeller 3, as can be observed from FIG. 10, and even more clearly in FIGS. 11 and 12.

[0102] From these last figures it is also noted that the two deflecting walls 17, 18 are substantially concave with a relatively high radius of curvature r′, r″ to avoid compression zones.

[0103] The second deflection wall 18 also presents a front appendix 24 whose aim is to shield the rear part of the advancing blade 4′ from the flow.

[0104] Also in this case the diverter 2 may be connected directly to the frame of the turbine 1 or to an external support structure by means of fixed or rotatably connecting means.

[0105] FIG. 13 shows a sixth configuration of the turbine 1 provided with diverter 2 which may comprise or less, as in the figure, the auxiliary diverter 13.

[0106] In this figures it is shown with more detail the frame 21 for the anchoring of the diverter 2 to the frame 25 of the turbine 1, which frame 25 will be provided with the axial rod 5 that connects the lower disc 20 to the shaft of a generator, not visible from the figure, for transforming the kinetic energy into electrical energy.

[0107] By way of example, the connecting means 27 will be of the rotary type, for example with roller bearings, ball or similar, which will allow the rotatably mounting on the stem of the support 5.

[0108] Furthermore, below the lower disc 20 an anchoring cage 28 will be arranged and provided with the aforesaid connecting hearing means 27 and which, with the diverter 2 mounted, will be placed peripherally to the generator, so as to leave it always accessible for any maintenance operation.

[0109] Further, in this configuration, the conveying duct 8 will house thereinside a plurality of deflection elements 29 each having a laminar or profiled body with a respective airfoil and at least partially overlapping each other and radially staggered.

[0110] The main task of these additional laminar or profiled bodies 29 will be to divert the current lines and slow the flow directed towards the blade 4′ in the advancing position to reduce the static pressure of the flow acting thereon and consequently increase the total torque.

[0111] According to the shown configuration, the laminar bodies 29 will be substantially similar to each other, with respective sections each having an airfoil with a concave outer edge and a convex inner edge.

[0112] It is also noted that one of the laminar bodies 29 will have a pair of concave outer edges cusp-joined and an inner plane edge, so that each outer edge is arranged in a position parallel to a corresponding outer edge of the two adjacent laminar bodies to create respective air ejection channels 30, which in a configuration not shown may possibly be placed in fluid communication with the conveying duct 8 to return the fluid rejected by the advancing blade 4′ back to the pushing blade 4.

[0113] The frame 21 will also include an airfoil 31 for orientation and stabilization of the flow integral with an upper disc-shaped wall 32 which joins the deflection walls 17, 18 in such a position as not to be invested by the flow generated by the impeller 3.

[0114] The primary function of the airfoil 31 will be to promote the rotation of the diverter 2 according to the main direction of fluid flow so as to align the inlet port 9 therewith, maintaining axially aligned, so as to maximize the effect of increase of the speed of the flow impacting on the blade 4 in the pushing position.

[0115] Besides this function comparable to that of a rudder, the airfoil 31 will have the function of producing a moment opposite to the moment produced by the laminar bodies 29 on the framework 21 to oppose to the rotation thereof and keep the inlet port 9 stable in correspondence of the main direction of the flow.

[0116] The airfoil 31 will be shaped to have not null incidence with respect to the flow when the frame 21 is in equilibrium condition, for example with an angle ranging between 5° and 45° with respect of the main direction of the flow, allowing the diverter 2 to be orientated so as to keep always in axis with the main direction of the flow.

[0117] Of course, different configurations are possible for the airfoil 31, which for example may be a hinged body of windmill type.

[0118] In addition, a brake may be provided, not shown, whose function will be to limit the angular speed of the diverter 2 in such a way to not make it rotate in an uncontrolled manner, avoiding high-frequency oscillations in the case of gusts and reducing the structural loads acting on the diverter itself.

[0119] The diverter 2 as described in the various configurations may be applied to any wind turbine with vertical axis, through appropriate adjustments of its configuration, which, however, will be essentially structural and do not modify the operation nor the essential elements for the definition of the scope of protection of the present invention.

[0120] The diverter 2 according to the present invention may equally be mounted on any turbine, not necessarily a wind turbine, and possibly arranged to operate with liquids or other gaseous fluids.

[0121] Of course, in the case where the turbine has not vertical axis or not is a wind turbine, the diverter 2 will still be designed to be arranged so as to at least partially envelop the impeller 3 thereof with the respective axes of rotation C, R substantially parallel with each other and its operation will be equivalent to that described above.

[0122] From above it appears evident that the turbine and the flow diverter according to the invention reach the intended object and in particular allow an increase of the maximum spin number of the turbine up to speed, while reducing the minimum speed of the fluid current required for the starter.

[0123] The diverter and the turbine according to the invention are susceptible of numerous modifications and variations, all falling within the inventive concept expressed in the attached claims. All the details may be replaced with other technically equivalent elements, and the materials may be different according to requirements, without departing from the scope of the present invention.

[0124] Even if the diverter and the turbine have been described with particular reference to the attached figures, reference numbers used in the description and in the claims are used to improve the intelligence of the invention and do not constitute any limitation the claimed scope.