SI9600085A - Fluid planet turbine, engine propeller, vane - Google Patents
Fluid planet turbine, engine propeller, vane Download PDFInfo
- Publication number
- SI9600085A SI9600085A SI9600085A SI9600085A SI9600085A SI 9600085 A SI9600085 A SI 9600085A SI 9600085 A SI9600085 A SI 9600085A SI 9600085 A SI9600085 A SI 9600085A SI 9600085 A SI9600085 A SI 9600085A
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- Prior art keywords
- planetary
- fluid
- wings
- turbine
- propeller
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03B—MACHINES OR ENGINES FOR LIQUIDS
- F03B17/00—Other machines or engines
- F03B17/06—Other machines or engines using liquid flow with predominantly kinetic energy conversion, e.g. of swinging-flap type, "run-of-river", "ultra-low head"
- F03B17/062—Other machines or engines using liquid flow with predominantly kinetic energy conversion, e.g. of swinging-flap type, "run-of-river", "ultra-low head" with rotation axis substantially at right angle to flow direction
- F03B17/065—Other machines or engines using liquid flow with predominantly kinetic energy conversion, e.g. of swinging-flap type, "run-of-river", "ultra-low head" with rotation axis substantially at right angle to flow direction the flow engaging parts having a cyclic movement relative to the rotor during its rotation
- F03B17/067—Other machines or engines using liquid flow with predominantly kinetic energy conversion, e.g. of swinging-flap type, "run-of-river", "ultra-low head" with rotation axis substantially at right angle to flow direction the flow engaging parts having a cyclic movement relative to the rotor during its rotation the cyclic relative movement being positively coupled to the movement of rotation
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- Y—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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/30—Energy from the sea, e.g. using wave energy or salinity gradient
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- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Wind Motors (AREA)
- Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
Abstract
Description
FLUIDNA PLANETNA TURBINA, MOTOR, PROPELER, VETRNICAFLUID PLANET TURBINE, ENGINE, PROPELLER, WINDOW
Predmet izuma sta turbina oziroma motor, ki spreminjata fotonsko energijo raznih elementov in energijo fluidov v mehansko delo in obratno v izvedbi propelerja ali črpalke.The subject of the invention are a turbine or engine, which convert the photonic energy of various elements and the energy of the fluid into mechanical work and vice versa in the design of a propeller or pump.
Izum sodi po mednarodni patentni klasifikaciji v F03D 7/06 v F04B ...The invention belongs to the international patent classification in F03D 7/06 in F04B ...
Tehnični problem, ki ga rešuje izum, je konstrukcija turbine, ki omogoča izkoriščanje malih in zelo velikih energetskih potencialov pogonskih medijev fotonov ali fluidov. Osebno vidim vsestransko uporabno vrednost izuma, vse od turbine, ki izkorišča plimo in oseko morja. Postavljena sme biti v pregradno steno kjer se morje ali drugi fluidi pretakajo. Postavljena sme biti na dno kjer so večji ali manši vodni tokovi. Uporabimo jo lahko za pogon elektro generatorjev na rekah. Postaviti jo smemo na dno reke, v pretočne jaške ali v že obstoječe objekte za odvzem energije vodnega toka.A technical problem solved by the invention is the construction of a turbine that allows the exploitation of small and very large energy potentials of photonic or fluid propulsion media. Personally, I see the versatile utility of the invention, everything from a turbine that takes advantage of the tide and the ebb of the sea. It may be placed in a bulkhead where the sea or other fluids flow. It may be placed at the bottom where there are larger or smaller watercourses. It can be used to drive electric generators on rivers. It may be placed at the bottom of the river, in the wells or in existing facilities for the abstraction of water flow.
V obliki - izvedbi fluidnega planetnega propelerja le tega namestimo pod dno ladje oz. čolna tik ob gredlju. Postavljen sme biti tako, da so planetna krila paralelna z gladino fluida vendar potopljena v fluid, na samo dno plovila. Druga postavitev je pravokotna na fluidno gladino (vodo). V tem primeru planetna krila gledajo čelno na dno, kot je to primer pri VVoith - Schneider - jevem propelerju. Vse do sedaj znane rešitve uporabljajo drugačen princip - način zajemanja energije. Znane so rešitve po patentih DE 386469, DE 59005308, IT 408992,In the form of a fluid planetary propeller, it is placed under the bottom of the ship or. boats just off the shaft. It may be positioned so that the planetary wings are parallel to the fluid surface but submerged in the fluid at the very bottom of the vessel. The second layout is perpendicular to the fluid surface (water). In this case, the planetary wings face the bottom, as is the case with the VVoith - Schneider propeller. All known solutions so far use a different principle - the way energy is captured. Patent solutions known in DE 386469, DE 59005308, IT 408992,
US 9501328, PL 300373, BE, FR 539273, CN 1029379, DE 534936.US 9501328, PL 300373, BE, FR 539273, CN 1029379, DE 534936.
Po izumu je problem rešen na način, s sistemom fotonske - fluidne planetne turbine, katero je možno izdelati in izkoriščati kot fluidno planetno turbino, planetno vetrnico ali fluidni planetni propeler in kot fotonski planetni turbo motor, propeler ali vetrnico.According to the invention, the problem is solved by a photon-fluid planetary turbine system that can be manufactured and used as a fluid planetary turbine, planetary windmill or fluid planetary propeller, and as a photonic planetary turbo engine, propeller or windmill.
Izum je opisan na poenostavljenem izvedbenem primeru in slikah, ki prikazujejo:The invention is described in the simplified embodiment and in the drawings showing:
Fig. 1a, 1 b fluidna planetna turbina po izumu v aksonometrični projekcijiFIG. 1a, 1b is a fluid planetary turbine according to the invention in axonometric projection
Fig. 2 fluidni planetni propeler po izumu v prerezuFIG. 2 is a cross-sectional view of a fluid planetary propeller of the invention
Fig. 3 radialni prerez fluidne planetne turbineFIG. 3 radial cross section of a fluid planetary turbine
Fig. 4 orisni delovni krog fotonske - fluidne planetne turbine, fluidnega planetnega propelerja in planetne vetrnice.FIG. 4 is an outline view of a photonic - fluid planetary turbine, fluid planetary propeller and planetary windmill.
Fluidna planetna turbina je sestavljena iz pogonskih ali gnanih planetnih kril 1, 2,3,4,5,6, zunanjih planetnih zobnikov 8,9,10,11,12,13, vmesnih zobnikov 14,15,16 in centralnega regulacijskega zobnika 17. Fluidna planetna turbina je vstavljena v okvir, ki ga sestavljajo ohišje reduktorja 46, podporna plošča 41 jedro 38 in dve zapiralni stranici 52 in 55.Fluid planetary turbine consists of propulsion or driven planetary wings 1, 2,3,4,5,6, outer planetary gears 8,9,10,11,12,13, intermediate gears 14,15,16 and central control gear 17 A fluid planetary turbine is inserted into a frame consisting of a gearbox housing 46, a support plate 41, a core 38, and two closing sides 52 and 55.
Planetna krila 1,2,3, 4, 5, 6 fluidne planetne turbine so z osjo 64, 65, 66, 67, 68, 69 vstavljena skozi iežajno ploščo 7. Na podaljšan del osi planetnih kril 64, 65,66,67, 68,69 nasadimo planetne zobnike 8, 9,10,11,12,13 nad Iežajno ploščo 7. Planetna krila 1, 2, 3, 4, 5, 6 fluidne planetne turbine so medsebojno postavljena v zakonito lego - položaj. Osnovno planetno krilo 1 fluidne planetne turbine je postavljeno soosno v smeri pretoka fluida oziroma paralelno z zapiralno stranico 55. Pravokotno na osnovno planetno krilo 1 fluidne planetne turbine je postavljeno četrto planetno krilo 4. Vsa ostala planetna krila 2, 3, 5, 6 so postavljena tako, da prečna os planetnega krila 2, 3, 5, 6 meri povsem matematično natančno v vzdolžno os osnovnega planetnega krila 1 fluidne planetne turbine. Vsi planetni zobniki 8, 9,10,11,12,13 so po parih v oprijemu z vmesnimi zobniki 14, 15, 16. Možne so izvedbe fluidnih planetnih turbin s še več ali manj planetnih kril kar osnovne zakonitosti postavitve (usmeritve) in regulacije rotacije planetnih kril ne poruši.The planetary wings 1,2,3, 4, 5, 6 of the fluid planetary turbine, with the axis 64, 65, 66, 67, 68, 69, are inserted through the bearing plate 7. On the extended part of the axis of the planetary wings 64, 65,66,67, 68,69 Plant planetary gears 8, 9,10,11,12,13 above the bearing plate 7. The planetary wings 1, 2, 3, 4, 5, 6 of the fluid planetary turbine are positioned in a legal position with one another. The basic planetary wing 1 of the fluid planetary turbine is positioned coaxially in the direction of fluid flow, or in parallel with the closing side 55. Perpendicular to the basic planetary wing 1 of the fluid planetary turbine is positioned the fourth planetary wing 4. All other planetary wings 2, 3, 5, 6 are erected so that the transverse axis of the planetary wing 2, 3, 5, 6 measures perfectly mathematically precisely in the longitudinal axis of the basic planetary wing 1 of the fluid planetary turbine. All planetary gears 8, 9,10,11,12,13 are in pairs in contact with intermediate gears 14, 15, 16. Fluid planetary turbines with even more or less planetary wings are possible, which is the basic regularity of layout (regulation) and regulation rotation of planetary wings does not break.
Regulacija je izvedena s pomočjo vmesnih zobnikov 14,15,16, ki so v oprijemu s centralnim regulacijskim zobnikom 17 in planetnimi zobniki 8, 9, 10, 11, 12,The regulation is made by means of intermediate gears 14,15,16 which are in contact with the central control gear 17 and the planetary gears 8, 9, 10, 11, 12,
13. V sistemu je prvi vmesni zobnik 14 v oprijemu s centralnim regulacijskim zobnikom 17, ki miruje in z dvema zunanjima planetnima zobnikoma 8,9. Drugi vmesni zobnik 15 je prav tako v oprijemu s centralnim regulacijskim zobnikom 17 in naslednjim parom zunanjih planetnih zobnikov 10,11. Tretji vmesni zobnik 16 je v oprijemu s centralnim regulacijskim zobnikom 17 in se tako vsi trije vmesni zobniki 14, 15, 16 obračajo okoli stoječega - mirujočega centralnega regulacijskega zobnika 17, s tem da je tretji vmesni zobnik 16 v oprijemu z zadnjim parom zunanjih planetnih zobnikov 12,13, ki jih poganja. Vsi zunanji planetni zobniki 8, 9,10,11,12,13, so nasajeni na osi 64, 65, 66, 67, 68, 69 planetnih kril 1,2,3,4,5,6. Regulacijski sistem je postavljen v ohišje regulacije 23 fluidne planetne turbine, ki je istočasno osnovna vodilna os (puša) na katero je tesno nasajen pogonski zobnik 19. Pogonski zobnik 19 je v oprijemu z gnanim zobnikom 20, ki je vležajen v ohišju reduktorja 46. S pomočjo gnanega zobnika 20 in njegove osi 21 v uležajenem ležišču 50 se energija iz planetnih kril 1,2,3, 4, 5, 6 fluidne planetne turbine prenaša k porabniku. Odvzem energije fluidne planetne turbine nam omogočata prileg jermenice - zobnika - verižnega kolesa in zagozda 22 v osi 21 gnanega zobnika 20. Ves sistem deluje tudi v obratni smeri kot fluidna planetna črpalka ali fluidni planetni propeler.13. In the system, the first intermediate gear 14 is in contact with the central control gear 17 which is stationary and with two outer planetary gears 8.9. The second intermediate gear 15 is also in contact with the central control gear 17 and the next pair of outer planetary gears 10.11. The third intermediate gear 16 is in contact with the central control gear 17, and thus all three intermediate gears 14, 15, 16 rotate around the standing-stationary central control gear 17, with the third intermediate gear 16 in contact with the last pair of outer planetary gears 12.13 driven by. All outer planetary gears 8, 9,10,11,12,13 are mounted on the axes 64, 65, 66, 67, 68, 69 of the planetary wings 1,2,3,4,5,6. The control system is mounted in the control housing 23 of the fluid planetary turbine, which is at the same time the basic guiding axis (bushing) to which the drive gear 19 is tightly fitted. The drive gear 19 is in contact with the driven gear 20 which is mounted in the gear housing 46. S by means of the driven pinion 20 and its axis 21 in the roller bearing 50, the energy from the planetary wings 1,2,3, 4, 5, 6 of the fluid planetary turbine is transmitted to the consumer. The energy recovery of the fluid planetary turbine allows us to fit the pulley - sprocket - chain wheel and wedge 22 in the axis 21 of the driven sprocket 20. The entire system also acts in the opposite direction as a fluid planetary pump or fluid planetary propeller.
Okvir fluidne planetne turbine je sestavljen iz ohišja reduktorja 46, ki je izdelan tako, da je zagotovljena pravilna medosna razdalja in vležajenje ohišja regulacije 23 in gnanega zobnika 20 z izstopno osjo 21. Ohišje reduktorja 46 je centralnemu regulacijskemu zobniku 17 s pomočjo vodilne puše 49 in osi zobnika 18 osnovno vodilo. Precizno regulacijo - nastavitev položaja planetnih kril 1,2,3, 4, 5, 6 vršimo s pomočjo regulacjskega utora 51 na centralnem regulacijskem zobniku 17. Na ohišje reduktorja 46 s pomočjo sponskih vijakov privijemo podporno ploščo 41. Za distanco nam služita dve zapiralni stranici 52 in 55. Montaža je sledeča: Sponski vijak potisnemo skozi izvrtino 42 podporne plošče 41, skozi izvrtino 53 v levi zapiralni stranici 52 in izvrtino 47 v ohišju reduktoija 46. Drugi sponski vijak potisnemo skozi izvrtino 43 podporne plošče 41, skozi izvrtino 54 v levi zapiralni stranici 52 v izvrtino 48 v ohišje reduktorja 46. Potrebujemo še dva sponska vijaka za desno zapiralno stranico 55. Postopek je enak le zapiralna stranica in izvrtine so druge.The fluid planetary turbine frame consists of a gear housing 46 designed to provide the correct wheelbase and mounting of the control housing 23 and the driven sprocket 20 with the output axis 21. The gear housing 46 is provided to the central control gear 17 by a guide sleeve 49 and sprocket axles 18 basic guide. Precision control - adjust the position of the planetary wings 1,2,3, 4, 5, 6 by means of the control groove 51 on the central control gear 17. Screw the support plate 41 onto the gearbox housing 46 with the help of clamping screws. 52 and 55. The mounting is as follows: The clamp screw is pushed through the hole 42 of the support plate 41, through the hole 53 in the left closure side 52 and the hole 47 in the gear housing 46. The second clamp screw is pushed through the hole 43 of the support plate 41, through the hole 54 in the left closing side 52 into bore 48 into gear housing 46. We need two more fastening screws for right closing side 55. The procedure is only the closing side and the holes are different.
Pri uporabi sistema fluidne planetne turbine kot fluidni planetni propeler, ni potrebno montirati elementov okvirja fluidne planetne turbine, kot so podporna plošča 41, leva zapiralna stranica 52 in desna zapiralna stranica 55. Planetna krila 1, 2, 3, 4, 5, 6 so na zunanjem delu v tem primeru zaobljena. Pogonsko energijo dovajamo na pogonsko os 21 in nato prek pogonskega zobnika 20 na gnani zobnik 19 s katerim sta v oprijemu. Iz gnanega zobnika 19 se energija pogona prenese prek ohišja regulacije 23 na ležajno ploščo 7 in od tod na podaljšane osi 64, 65, 66, 67, 68, 69 planetnih kril 1,2, 3, 4, 5, 6 fluidnega planetnega propelerja. Regulacijski sistem zobnikov 8,9,10,11,12,13 -14,15, 16-17 je povsem identičen - enak, kot pri fluidni planetni turbini. Tudi v tej izvedbi morajo biti planetna krila 1,2, 3, 4, 5, 6 fluidnega planetnega propelerja postavljena v zakonito lego - položaj. Osnovno planetno krilo 1 fluidnega planetnega propelerja je postavljeno soosno v smeri pretoka fluida oziroma paralelno z dnom vodnega plovila. Pravokotno na to osnovno planetno krilo 1 fluidnega planetnega propelerja je postavljeno četrto planetno krilo 4. Vsa ostala planetna krila 2, 3, 5,6 fluidnega planetnega propelerja so postavljena tako, da prečna os planetnih kril 2,3,5,6 fluidnega planetnega propelerja merijo povsem matematično točno v vzdolžno os osnovnega planetnega krila 1 fluidnega planetnega propelerja.When using a fluid planetary turbine system as a fluid planetary propeller, it is not necessary to mount the elements of the fluid planetary turbine frame, such as support plate 41, left closing side 52 and right closing side 55. Planetary wings 1, 2, 3, 4, 5, 6 are on the outer part in this case rounded. The drive energy is fed to the drive axle 21 and then via the drive sprocket 20 to the driven sprocket 19 with which they are gripped. From the driven gear 19, the energy of the drive is transmitted through the control housing 23 to the bearing plate 7 and then to the extended axes 64, 65, 66, 67, 68, 69 of the planetary wings 1,2, 3, 4, 5, 6 of the fluid planetary propeller. The gear system 8,9,10,11,12,13 -14,15, 16-17 is completely identical - the same as that of a fluid planetary turbine. Also in this embodiment, the planetary wings 1,2, 3, 4, 5, 6 of the fluid planetary propeller must be in a legal position. The basic planetary wing 1 of the fluid planetary propeller is positioned coaxially in the direction of fluid flow or parallel to the bottom of the water craft. Perpendicular to this basic planetary wing 1 of the fluid planetary propeller is positioned the fourth planetary wing 4. All other planetary wings 2, 3, 5,6 of the fluid planetary propeller are positioned such that the transverse axis of the planetary wings 2,3,5,6 of the fluid planetary propeller they measure exactly mathematically exactly in the longitudinal axis of the basic planetary wing 1 of a fluid planetary propeller.
Andrej Plešivčnik—Andrej Plešivčnik—
Claims (2)
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SI9600085A SI9600085A (en) | 1996-03-12 | 1996-03-12 | Fluid planet turbine, engine propeller, vane |
| AU21110/97A AU2111097A (en) | 1996-03-12 | 1997-03-11 | Fluid flow turbine with planetary linked paddles |
| PCT/SI1997/000007 WO1997034082A2 (en) | 1996-03-12 | 1997-03-11 | Fluid flow turbine with planetary linked paddles |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SI9600085A SI9600085A (en) | 1996-03-12 | 1996-03-12 | Fluid planet turbine, engine propeller, vane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| SI9600085A true SI9600085A (en) | 1997-10-31 |
Family
ID=20431806
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| SI9600085A SI9600085A (en) | 1996-03-12 | 1996-03-12 | Fluid planet turbine, engine propeller, vane |
Country Status (3)
| Country | Link |
|---|---|
| AU (1) | AU2111097A (en) |
| SI (1) | SI9600085A (en) |
| WO (1) | WO1997034082A2 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2454523B (en) * | 2007-11-10 | 2011-12-14 | Neil Andrew Blackett Caldwell | Pump for fluids |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1396515A (en) * | 1964-03-12 | 1965-04-23 | Motor with vertical axis and adjustable wings driven by a streamline flow | |
| US4411632A (en) * | 1978-06-28 | 1983-10-25 | Wuenscher Hans F | Waterbound facility powered by cycloidal fluid flow engines |
| DE2862346D1 (en) * | 1978-09-01 | 1983-12-22 | Friedrich Friedl | Turbo-machine |
| DE2927956C2 (en) * | 1979-07-11 | 1981-10-29 | J.M. Voith Gmbh, 7920 Heidenheim | Wind or hydropower device |
| GB8327663D0 (en) * | 1983-10-15 | 1983-11-16 | Dunn S | Deriving energy from fluids in flows |
| US5324164A (en) * | 1991-06-13 | 1994-06-28 | Doering John N | Fluid active device |
-
1996
- 1996-03-12 SI SI9600085A patent/SI9600085A/en unknown
-
1997
- 1997-03-11 AU AU21110/97A patent/AU2111097A/en not_active Abandoned
- 1997-03-11 WO PCT/SI1997/000007 patent/WO1997034082A2/en active Application Filing
Also Published As
| Publication number | Publication date |
|---|---|
| WO1997034082A2 (en) | 1997-09-18 |
| AU2111097A (en) | 1997-10-01 |
| WO1997034082A3 (en) | 1997-12-11 |
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