SYSTEM FOR RECOVERING ENERGY FROM RENEWABLE SOURCES
20180195496 ยท 2018-07-12
Inventors
Cpc classification
Y02E10/74
GENERAL 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
F03G6/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2210/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D3/061
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2240/212
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02E10/728
GENERAL 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
F03D3/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02B10/30
GENERAL 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
F05B2240/213
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03G6/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D9/45
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03G6/045
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02B10/70
GENERAL 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
F05B2240/13
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2220/602
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02E10/46
GENERAL 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
F03D3/005
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D9/37
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F24S10/30
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D3/0454
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F03D9/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03G6/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D3/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D9/45
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D3/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A system for recovering energy from renewable sources comprises a first conduit (2) for the flow of a working fluid, heating means (3) of the fluid in the first conduit (2) adapted to promote the flow thereinside, a turbine (4) having a conveyor (5) in fluid communication with the first conduit (2) and an impeller (6) adapted to be connected to generating means (8) for the generation of energy for receiving the flow sent by the first conduit (2) and intercepted by the conveyor (5) to operate the generating means (8).
Claims
1. A system for recovering energy from renewable sources, comprising: a first conduit (2) for the flow of a working fluid; heating means (3) of said fluid in said first conduit (2) adapted to promote the flow thereinside; characterized by comprising a turbine (4) having a conveyor (5) in fluid communication with said first conduit (2) and an impeller (6) adapted to be connected to generating means (8) for the generation of energy for receiving the flow sent by said first conduit (2) and intercepted by said conveyor (5) and operating said generating means (8).
2. System as claimed in claim 1, characterized in that said impeller (6) has one or more blades (15) adapted to move between a thrust position and a return position upon rotation of said impeller (6), said conveyor (5) having a supplying mouth (16) for the flow in a position facing the blade (15) in said thrust position and a side wall (17) at least partially wrapping said impeller (5).
3. System as claimed in claim 2, characterized in that said turbine (4) comprises a flow diverter (18) which extends from an input section (19) facing one or more blades (15) in said return position to an output section (20) facing one or more blades (15) in said thrust position and in fluid communication with said conveyor (5) to return at least partially the working fluid toward the latter and increase the torque produced by the flow on said impeller (6).
4. System as claimed in claim 3, characterized in that said flow diverter (18) is divided into a plurality of return ducts (21) substantially curvilinear and in. mutually side-by-side position.
5. System as claimed in claim 1, characterized in that said heating means (3) comprise a heater device (9) operating with a renewable energy source, such as a solar thermal device (14), a solar concentration device or the like, having a second conduit (10) for the circulation of a heating fluid fluidically connected to said first conduit (2).
6. System as claimed in claim 5, characterized in that said heating means (3) comprise a heat exchanger (11) having a primary circuit (12) fluidically connected to said first conduit (2) and a secondary circuit (13) fluidically connected to said second conduit (10).
7. System as claimed in claim 6, characterized in that said heat exchanger (11) is arranged upstream of said conveyor (5) with respect to the fluid flow.
8. System as claimed in claim 1, characterized in that said turbine (4) comprises a conveying duct (40) jointed to said first conduit (2) upstream of said impeller (6) and designed to speed up the flow entering said impeller (6).
9. System as claimed in claim 8, characterized in that said turbine (4) comprises an acceleration duct (27) jointed to said first conduit (2) downstream of said impeller (6) and designed to speed up the flow outcoming from said impeller (6).
10. System as claimed in claim 1, characterized by comprising a ventilated wall (22) having an anchoring structure (23) adapted to be secured to a facade (F) of a building and a coating (24) fixed to said anchoring structure (23) at a predetermined distance (d) from the facade (F) to define a gap (25) therewith, which gap (25) having an upper edge (26) at least partially open, said first conduit (2) being housed into or defined by said gap (25).
11. System as claimed in claim 10, characterized in that said conveyor (5) of said turbine (4) is in fluid communication with said gap (25) for receiving a flow of air raising thereinto and to be sent to said impeller (6).
12. System as claimed in claim 11, characterized in that said conveyor (5) is defined by an extension of the curvilinear end (17) of said coating (24) which extends beyond said upper edge (26) of said gap (25).
13. System as claimed in claim 1, characterized in that said heat exchanger (11) is placed at the base of said gap (25) and is optionally provided with one or more fans adapted to force the rising of the heated air flow towards said conveyor (5).
14. System as claimed in claim 1, characterized in that said turbine (4) comprises a stator (28) having a plurality of first radial channels (29) for ejecting flow each having an inlet (30) connected to said first conduit (2) and an outlet (31) facing a respective blade (15) of said impeller (6).
15. System as claimed in claim 14, characterized in that said stator (28) comprises a plurality of second radial channels (32) each having an inlet (35) connected to an auxiliary duct (34) open towards the outside for the input of an air flow and an outlet (36) facing a respective blade (15) of said impeller (6).
16. System as claimed in claim 15, characterized in that said first radial channels (29) are alternated to said second radial channels (32).
17. System as claimed in claim 16, characterized in that the outputs (31, 36) of said first (29) and second radial channels (32) are facing respective blades (15) of said impeller (6) with an inclination such as to produce a respective output fluid jet incident the respective blade (15) with an angle comprised between 80 and 100.
18. System as claimed in claim 17, characterized in that said turbine (4) is of the Darrieus type with a plurality of blades (15) arranged peripherally to said stator (28).
Description
BRIEF DISCLOSURE OF THE DRAWINGS
[0035] 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 system according to the invention, illustrated by way of non-limiting example with the aid of the accompanying drawing tables wherein:
[0036]
[0037]
[0038]
[0039]
[0040]
[0041]
[0042]
BEST MODES OF CARRYING OUT THE INVENTION
[0043]
[0044] As will become more clear from the following description, the system may assume different configurations depending on the available space, on the devices used and on the purpose without particular limitations.
[0045] In particular, the system 1 according to the invention may be integrated within water pipelines for mini- or micro-hydric applications.
[0046] In its most basic form, the system, generally designated by 1, comprises a first conduit 2 for the flow of a working fluid, for example air or other gas or mixture of gases, or water or other liquid, heating means 3 of the fluid within the first conduit 2 adapted to promote the flow thereinside, and a turbine 4 having a conveyor 5 in fluid communication with the first conduit 2 and an impeller 6 adapted to receive the flow from the first conduit 2 intercepted by the conveyor 5.
[0047] In a known manner the impeller 6 will have a rotation shaft 7 operatively coupled to means for generating electrical or mechanical energy 8, not described in detail since of per se known type, which will be operated by the rotation of the impeller 6 triggered by the flow coming from the conveyor 5.
[0048] The heating means 3 comprise a heating device 9 having a second conduit 10 for the circulation of a second heating fluid fluidically connected to the first conduit 2.
[0049] The heating device 9 is suitably connected to a heat exchanger 11 positioned upstream of the turbine 4 with respect to fluid flow and having a primary circuit 12 fluidically connected to the first conduit 2 and a secondary circuit 13 fluidically connected to the second conduit 10. The heat exchanger 11, simply schematized in the figure, may be selected between those commonly available on the market, without particular limitations, and in particular may be of the coil type.
[0050] In a particular variant, not shown, the primary circuit 12 may be connected to a hydraulic circuit of a building served by the system wherein there will be a flow of hot water heated by an appropriate burner, or it may be provided with its own burner.
[0051] Preferably, the heating means 3 of the fluid flowing in the heat exchanger 11 will be selected between the devices operating with renewable energy sources.
[0052] In preferred manner, the heating means 3 comprise a common solar thermal device 14 adapted to be installed on a building, either on the roof or on a facade, or fixed to a support structure, also far away from the building or from the consumption served by the system, or arranged externally to the pipe in the case of hydraulic applications.
[0053] The solar device 14 will have a circulation duct 10 of the heating fluid fluidically connected to the primary circuit 12 of the exchanger 11.
[0054] The solar device 14 may also be of the heat storage type so as to store thermal energy thereinside to be released at a later time depending on the needs.
[0055] According to a not illustrated variant, the solar device 14 may be of the concentration type or the like.
[0056] The first conduit 2 arranged to convey the air, water or another heated fluid towards the turbine 4 may have any shape, for example with circular or rectangular cross section, and may be open or closed.
[0057] The heat exchanger 11 will generally be arranged at the base of the first conduit 2 or in any case upstream of the turbine 4 and will be possibly provided with one or more fans, not shown, adapted to force the raising of the heated flow towards the conveyor 5.
[0058] According to a not shown variant, the first conduit 2 may be divided into one or more shaped vertical conduits for accelerating the flow towards the conveyor 5, for example with cross-section decreasing upwards to generate a Venturi effect.
[0059] Alternatively, the first conduit 2 may house thereinside such shaped conduits having an inlet section close to the heat exchanger 11 and an outlet section facing the inlet of the conveyor 5. The conduits may have any sectional shape, for example circular or rectangular, and may also be insulated or perforated in correspondence of the heat exchanger 11.
[0060] The turbine 4 may be any commercially available turbine and in a preferred but not exclusive embodiment will be of the type disclosed in the Italian patent application VI2013A000189 in the name of the same Applicant or more preferably according to any one of the configurations disclosed in the Italian patent application VI2014A000272, always in the name of the same Applicant, as shown in greater detail in
[0061] From this figure it is observed that the impeller 6 comprises a plurality of blades 15 adapted to alternately move between a thrust position and a return position upon rotation of the impeller 6.
[0062] In particular, the blades 15 are integral with each other to rotate unitarily following the action of the air flow so that from time to time at least one blade 15 is in the thrusting position corresponding to the position in which it is facing the supplying mouth 16 of the conveyor 5 designed to the entrance of the fluid flow, to be invested by the flow (whose advancing direction is indicated by arrows). At the same time at least one other blade 15 will be in return or advancing position.
[0063] The conveyor 5 has a side wall 17 which partially wraps around the impeller 6 and which may be defined by a first portion of the same first conduit 2, for example by an extension of the ends thereof in the case in which the turbine 4 is placed outside the first conduit 2.
[0064] The turbine 5 may also comprise a flow diverter 18 that extends from an inlet section 19 facing the blades 15 in advancing position to an output section 20 facing to the blades 15 in the thrust position and in fluid communication with the supplying mouth 16 of the conveyor 5, to restore at least partially the working fluid toward the blades 15 in the thrust position and increase the torque produced by the flow on the impeller 6.
[0065] The flow diverter 18 is divided into a plurality of return ducts 21, substantially curvilinear and mutually side by side.
[0066] The curvature radius of the return ducts 21 may have any values without particular limitations and is preferably not too narrow with angles at the center greater than 45 to avoid the occurrence of phenomena of compression of the fluid and consequent turbulent motion.
[0067]
[0068] As schematically shown in this figure, in a known manner the energy recovery ventilated wall 22 comprises an anchoring structure 23 adapted to be secured to the facade F of the building and a coating 24 fixed to the anchoring structure 23 at a predetermined distance d from the facade F to define therewith a gap 25 having an upper edge 26 at least partially open.
[0069] Although in the figure the diverter 18 is illustrated in a position such as to define a light with the upper edge 26, it may be arranged so as to occlude this light and if necessary may be disposed at least partially inside the gap 25.
[0070] The technical features of the anchoring structure 23 and the coating 24 will not be described more in detail as it will be clear that they are not limiting for the scope of protection of the present invention and may be selected between the structures and coatings commonly used for the realization and installation of known ventilated walls.
[0071] In a first variant the same gap 25 will define the first conduit for the circulation of the heated fluid.
[0072] In this case, the upper open edge 26 of the gap 25 is connected to the wind turbine 4 having the conveyor 5 in fluid communication with the gap 25 itself. In this way the impeller 6 may receive an air flow raising along the gap 25 and intercepted by the conveyor 5 to be brought into rotation around its central axis.
[0073] The rotation of the impeller 6 operates the energy generation means 8 which may comprise an electric generator having a power shaft connected to the central axis of rotation 7 of the impeller 6.
[0074] The turbine 4 may be dimensioned in function of the specific needs in terms of energy requirements, as well as the availability of space, and generally will be of the type suitable for micro-wind applications, and mini-water application with open channel.
[0075] For example, the turbine 4 may have a bearing frame to be fixed in a stable manner directly to the building or to the same anchoring structure 23 of the coating 24, so that the impeller 6 has a horizontal central rotation axis.
[0076] In a particular embodiment the conveyor 5 will have a side wall 17 which partially wraps around the impeller 6 and which will be defined by an extension of the curvilinear ends of the coating 24 which extends beyond the upper edge 26 of the gap 25.
[0077] In particular, the extension 17 may be unitary with the coating 24 or simply juxtaposed thereto by means of any type of connecting means to be in each case continuous therewith.
[0078] The extension 17 may extend only for part of the width of the coating 24, normally corresponding to the width of the facade F of the building, or for the whole width.
[0079] In this case it will also be possible to install more wind turbines 4 independent of each other or fitted with impellers with common axis of rotation.
[0080] The heat exchanger 11 may be installed at the base of the gap 25 or at a different height, depending on the needs.
[0081] Suitably, the gap 25 or the possible conduit 2 will have at the base, in correspondence of the heat exchanger 11, a slot to allow the creation of an air flow from outside toward the inside.
[0082] According to a second variant, not shown, the gap 25 may be divided into one or more shaped vertical conduits to accelerate the flow of air towards the conveyor 5, for example with a cross-section decreasing upwards to generate a Venturi effect.
[0083] According to yet another variant, the gap 25 may house thereinside the first conduit 2, possibly divided in more shaped ducts having an inlet section close to the heat exchanger 11 and an outlet section facing the supplying mouth 16 of the conveyor 5.
[0084] The ducts may have any sectional shape, for example circular or rectangular, and may also be insulated or perforated in correspondence of the heat exchanger 11.
[0085] According to yet an alternative variant, one or more of the vertical ducts that branch off from the heat exchanger 11 may be at least partially external to the ventilated wall 22.
[0086] The first conduit 2 for the circulation of hot air may be either open or closed, even with the ventilated wall 22.
[0087]
[0088]
[0089] When the system is applied to a water pipeline, the turbine 4 will also comprise an acceleration duct 40 connected to the first conduit 2 downstream of the impeller 6 and designed to accelerate the flow outcoming therefrom.
[0090]
[0091] The turbine 4 comprises a stator 28 having a plurality of first radial channels 29 for ejecting the flow, each having an inlet 30 connected to the first conduit 2 upstream of the stator 28 and an outlet 31 facing a respective blade 15 of the impeller 6.
[0092] Furthermore, the stator 28 also comprises a plurality of second radial channels 32 connected to an auxiliary duct 34 open to the outside and having a plurality of inlets 35 for the entry of an air current, for example of the wind, and an output 36 facing a respective blade 15 of the impeller 6.
[0093] Preferably, the inlets 35 will be transverse with respect to the air flow to be intercepted. According to the preferred but not exclusive embodiment of the figure the first radial channels 29 are alternated with second radial channel 32 and also the respective outputs 31, 36 are equally angularly spaced.
[0094] Moreover, the outputs 31, 36 of the first and second radial channels 29, 32 are facing respective blades 15 of the impeller 6 with such inclination as to produce a respective output fluid jet incident the respective blade with an angle between 80 and 100
[0095] As visible from
[0096] In addition, it also appears evident that the turbine thus configured may also be used in systems different from the one object of the present invention because in any case will have the advantage of being able to recover energy from two different flows intercepted by the first radial channels 29 and the second radial channels 32.
[0097] From above it is clear that the system according to the invention reaches the intended objects and in particular it recovers the energy associated with the convective motions created inside the heated fluid, being able to transform, in a particular configuration, the ventilated wall in an active power generation system.
[0098] The system according to the invention is susceptible of numerous modifications and variations, all falling within the inventive concept expressed in the accompanying claims. All the details may furthermore be replaced with other technically equivalent elements, and the materials may be different according to requirements, without departing from the scope of protection of the present invention.
[0099] Although the system has been described with particular reference to the attached figures, the 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 to the scope of protection claimed.