IL81918A - Universal energy turboconverter - Google Patents
Universal energy turboconverterInfo
- Publication number
- IL81918A IL81918A IL8191887A IL8191887A IL81918A IL 81918 A IL81918 A IL 81918A IL 8191887 A IL8191887 A IL 8191887A IL 8191887 A IL8191887 A IL 8191887A IL 81918 A IL81918 A IL 81918A
- Authority
- IL
- Israel
- Prior art keywords
- turbine
- turboconverter
- universal
- mentioned
- blades
- Prior art date
Links
Classifications
-
- 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
- Y02E10/20—Hydro energy
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Description
vi UNIVERSAL ENERGY Noah 2 of the invention power mixer for chemical industry and aerator and disinfector for community Purpose Full pr partial conversion of the energy of circulating pf Consistencies to mechanical or electrical energy vice versar The turbpcpnverter be used as electric mixer for pesticides aerator and disinfector of water in fish ponds kinematic drive element for other electrical or mechanical seyeral functions can be combined in one as electric fertilizer and or p or electric generator with an injector to solar energy converting pf There are varipus knpwn turboconyerters that make use pf energy pf most popular are hydraulic turbines of the Francis turbines and aplan use are the and there are and turbines combined with the rotor of a generator which is fitted on the ends of fixed on the main There are also turbines with stages mo in sequence on a common these have certain advantages and Their main Disadvantages large energy losses at the input large loss pf the energy pf flow in the turbine midsection of turbines the in ΡΓ an abrupt change in the direction of flow centrifugal d centripetal The constructional and technological peculiarities of these turbines do not allow their implementation fpr a partial e of the energy of for in plant irrigation with simultaneous fertilizer or for obtaining electrical energy to charge batteries and tP power automatic irrigation control TP reduce the negative effects of the above disadvantages and broaden the range pf applications pf the energy I am submitting the following Drawings lb Front view of proposed energy turboconverter Turbine without central shaft greater Turbine with central shaft 4 Longitudinal section of energy turboconverter with central shaft and with axial and radial bearings 5 Longitudinal section of energy turboconverter with pump and outward shaft 6 View along arrow A in 5 7 Front view of the energy turboconverter modified for use as turboelectric generator 8 Turboelectric generator for travel in water 9 Front view of energy tuboconverter with turbine with centrifugal pump on outside 10 Turboconverter modified for use as watering machine lib Sections along and in 10 12 Turboconverter modified for use as One of the versions of the energy converter is shown in longitudinal section in It consists of a housing 1 with ends threaded for attaching the input and output Inside the housing are spaces for bearings compression seals and room for for the rotor and stator of an electric or the pump wheel or transducer disc of a flowmeter or of an axial or several of these devices a guide apparatus for a water flow is formed by inside wall of the housing blades la and the neck 11 which at the same time acts as the diffusor of the The turbine 2 has in the first stage 2a 8 in the second stage 2b 4 third stage 2c 2 blades and can to be a or turbine If the work of the turbine 2 must be combined with that of an ejector 7 its inner conical space of the neck 11 causes turbulence in the interior mixing chamber on the front face of the and the neck causes turbulence in the mixing chamber on the back face of the The latter can be used as a receiver of the type for to meet an axial It should be mentioned that the degree of effectiveness of each of the above devices and their power output are designed in accordance with the intended use of the energy In we illustrate our conception with a working draft of a turbine for The turbine 20 consists of a casing 21 that acts at once as support for an axial bearing and as an attachment The external part of the casing is in the shape of a cylinder which serves to mount the turbine in the housing and to hold the parts of the The inner wall of the casing is conical with a contraction in the direction of This allows one to use the turbine in combination with an Depending on its the turbine can be made with a reversed or with contractions at the ends or in the The blades of the turbine 20 are of various lengths and constitute the stages of the The number of blades depends on the purpose of the 2C shows an axial pump A on the external part of the The axial pump sets up a radial water bearing and lightens the load on the axial 2a shows a The first stage has 8 the second stage has 4 and the third stage has 2 The blades of the turbine are with a pitch and their front edges make an angle β with the longitudinal plane of which directs the flow to the The blades are fixed on the periphery and free in the center and do not touch one making an axial passage for the passing of mixtures containing particulate matter and for reducing resistance losses when working with viscous The blades of the guide apparatus are similar to the blades of the turbine but have a different pitch a and are fitted in the opposite If the turboconverter must be used under other for example with an the inner passage of the turbine and of the guide can be replaced by a shaft and also with a transfer of the axial and the radial bearings to that shaft This does not greatly increase the resistance to flow or the other properties of the proposed 5 3 5 shows a longitudinal section of the energ turboconyerter putward To the turboagregate 24 is added the pump 25 by means of A shaft 27 can be utilized as 6 show the cross section along arrow A of The pump 25 connects up with the housing and work together with axial pump through a tube 28 7 Shows a front view of the energ turboconyerter for se as turboelectric It consists of a housing 29 with ends threaded for attaching the input output tubes and a guide inside body are fittings for bearings compression seals 31 and room for installing the rotor 32 on the and stator 33 of an electric V 8 shows the turboelectric generator modified for t r It of a reception pipe 34 and pipe bend This version has applications for sailbpats a blades of the turbine are fixed on the periphery an4 free the center do not touch each creating an passage fpr containing e matter and for reducing resistance turbine is not by seaweeds and other 9 a front view of the energy turboconverter with a turbine with Centrifugal pump 36 on the outside of the casing The same turbine may serve for pumping liquid from the work stream and from the outside required 10 shows a modification of the turboconyerter for use as a watering The turbogenerator together with the turbine stabilizer bearings flange 41 and drum make up the watering 11 shows how the drum 42 revolves together with turbine this Water discharge hoses which are connected to a spring 12 shows a modification of the turboconyerter for as a pump Arrows show the direction of motion of the Signs show the zones pf increased and reduced insufficientOCRQuality
Claims (22)
1. The liquid acts on the peripheral parts of the blades of the turbine at the area where they are held in the casing, with the purpose of achieving the maximum moment, reducing the dimensions of the middle section and reducing the resistance of the axle and of the bushing of the turbine, or alternatively of producing a central opening along the length of the turbine to enable flow of mixtures (for instance, sewage or more viscous liquids) so as to increase the strength of the turbine.
2. To make possible the arrangement described above in (1), the blades are mounted so that the angle β in the cross section of the turbine opens in the direction opposite to the direction of rotation of the turbine;
3. The casing of the turbine has an axial pump (with screw threads) on the outside which sets up a liquid radial bearing, the liquid for work being taken from the work stream or from the outside;
4. Together with the turbine the housing forms a work cavity for the energy converter (gears, rotor and stator of the electrogenerator, centrifugal pump, axial pump and other parts), which can be made hermetically sealed from the channels of liquid. 5. The universal turboconverter can work on ascent and lower gravity feed lines and can keep one's in dissolubility of the stream (presence of a central opening in the turbine). IV. WHAT IS CLAIMED IS 1. An universal turboconverter for exploiting flowing of liquid or gaseous media which comprises from a guide apparatus and a high-moment, single-pass, multistage turbine, mounted in a housing, wherein the guide apparatus, turbine and housing are arranged so that a single-pass axial channel is created, allowing full or partial use of energy of working medium moving through said axial channel, which is bounded by inner edges of turbine blades and a shape of blades forces part of working medium to periphery, thus increasing a torque of turbine and eliminating harmful resistance in said channel and energy-conversion devices are installed beyond of turbine casing, outside of flow, but entirely or partially within of housing. 7 8^918/3 2. An universal turboconverter as mentioned in claim 1, wherein liquid i turbine acts on the peripheral parts of blades where they join up tQ c sing, with p pp e of achieving maximum moment, reducing dimensions of middle section anq" reducing resistance of axle and of bushing of the turbine, or in order to prpcluce 3 central longitudinal opening. 3, An universal turboconverter as mentioned in claim \, wherein blad s are mounted so as to produce in cross sectipn an angle β opening in a direcfipn ppposite to the direction of rotation of the turbine. - An universal turboconverter as mentioned in claim 1, wherein a casing pf turbine has an axial pump with screw threads on outside that sets up a liquid radial bearing a d takes load off the axial bearing and the liquid, for work is tak from t e WPrk-stream or from the outside and returned tp the work-stream pr tp the putside,
5. An universal turboconverter as mentioned in claim 1, wherein a turbine and housing forms a work cavity for the energy converter (gears, rptPr an statpr pf electric generator, centrifugal pump, axial pump and other) which can be made hermetically sealed from the channels of liquid.
6. An universal turboconverter as mentioned in claim I, wherein in cases where liquid, does not contain solid matter or has low viscosity, a turbine can, if necessary, be replaced by a shaft without significantly increasing the losses in efficienpy du fP friction.
7. An universal turboconverter as mentioned in claim 1, wherein energy conversipn devices are placed inside pf sealed hpusing P PUtside pf turbine casing. Which broadens possibilities for use.
8. A universal turboconverter as mentioned in claim I, wherein it can be fitted, ¾ via connecting devices, directly onto a ma n pipe line or can be provided with input and output devices that supply the working med um-
9. An universal turboconverter as mentioned in claim 1, wherein it can be cpnnected o large diameter pipe lines either in parallel or in series or both and i is also possible to install several units as a block. 8 81918/3 }Q.
10. An universal turboconverter as mentioned jn cl im , wherein it can act a§ a pump and be fitted with an electric motor or other drive by installing blades with the appropriate pitch.
11. Π· An universal turboconverter as mentioned in claim. \> wherein it can he fitted i a ejector stream with mixing chambers on front and back ends of turbine and a neck of outlet can be used as a "Ventury" element, to simplify sealing devices a^d to create a vacuum at site where an energy converter is installed?
12. An universal turboconverter as mentioned in claim 1, wherein a guide apparatus has blades mounted on the periphery that cre e a free i l ss ge y for t e flow of particulate suspensions and the angles of the surfaces and edges of the blade§ assure an optimal direction for the flow velocity vectors over Its, . peripheral part, to create maximum torque.
13. An universal turboconverter as mentioned in claim 1, wherein a gujcl§ apparatus is such that in cases where liquid does not contain solid matter qr has low Viscosity, the free axial passage through a guide apparatus can he replaced by a shaft without considerably increasing the losses in efficiency due to friction. 1 .
14. An universal turboconverter as mentioned in claim X, wherein the high-mpmen†, single-pass, multi-stage turbine has blades mounted on t e inner aP of . ' the casing o as to form an axial passage for the flow of p rticulate suspensions an4 " thereby diminish losses due to factional resistance and the angles of their working * surfaces and edges assure an optimal direction for the vecfpr pf the force applied o , -the liquid at the maximum radius.
15. An universal turboconverter as mentioned in claim 1, wherein the high-moment/ single-pass, multi-stage turbine has, blades inst lled inside o e Pf several adjoining conical cavities to ensure an effective contact of a liquid i h entire lengt ; of blades and this ca allow a change of an angle of sides pf c nes rna e with the direction of flow, so the cones can be almost cylinders, depending on the purpose and order of arrangement of parts of turbine.
16. An universal turboconverter as mentioned in claim 1, wherein in prcjer to increase the efficiency of one or many stages pf high-moment, single-pass, multi- 9 81918/3 stage turbine it is ppssible to install blades of various lengths, where blades of a lower stage enter into structure of a higher stage without interruption.
17. An universal turboconverter as mentioned in claim 1, wherein a high-moment, single-pass, multi-stage turbine stages can he arranged i the direction of th flow frpm the lower to the higher stage or vice versa and in addition, a higher stage can be placed in the middle and the lower stage at the ends or Yice versa.
18. An universal turboconverter as mentioned in claim \, wherein in a Wgh-moment, single-pass, multi-stage turbine an effective length Pan be fi ed according tp the mber of stages or vice versa and this means that working blades can be mounted ith a length of turbine right up to a stage with one blade and it- is alsp possible to use only part of length of a stage. ^
19. An universal turboconverter as mentioned in claim 1, wherein a stabilizing device can haye blades mounted on the periphery to m ke a free axial pass ge for the flow of particulate suspensions and viscous media.
20. An universal turboconverter as mentioned in claim 1/ wherein an axial an radial supports are long-lived and reliable thanks to effect pf the axial ump
21. An u iversal turboconverter s mentioned in claim X, wherein it can wprk pn condensations liquids and the degree of the condensation depending pn pressures i the circulating liquid media.
22. An universal turboconverter as mentioned in claim I, wherein it can work on ascent r> lower gravity feed lines.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IL8191887A IL81918A (en) | 1987-03-17 | 1987-03-17 | Universal energy turboconverter |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IL8191887A IL81918A (en) | 1987-03-17 | 1987-03-17 | Universal energy turboconverter |
Publications (2)
Publication Number | Publication Date |
---|---|
IL81918A0 IL81918A0 (en) | 1987-10-20 |
IL81918A true IL81918A (en) | 1994-11-11 |
Family
ID=11057634
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IL8191887A IL81918A (en) | 1987-03-17 | 1987-03-17 | Universal energy turboconverter |
Country Status (1)
Country | Link |
---|---|
IL (1) | IL81918A (en) |
-
1987
- 1987-03-17 IL IL8191887A patent/IL81918A/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
IL81918A0 (en) | 1987-10-20 |
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