NZ238185A - Heat pipe with vapour driven turbine. - Google Patents

Heat pipe with vapour driven turbine.

Info

Publication number
NZ238185A
NZ238185A NZ238185A NZ23818591A NZ238185A NZ 238185 A NZ238185 A NZ 238185A NZ 238185 A NZ238185 A NZ 238185A NZ 23818591 A NZ23818591 A NZ 23818591A NZ 238185 A NZ238185 A NZ 238185A
Authority
NZ
New Zealand
Prior art keywords
thermosyphon
vapour
enclosure
section
turbine
Prior art date
Application number
NZ238185A
Inventor
Aliakbar Akbarzadeh
Peter William Johnson
Kevin Arthur Gibson
Original Assignee
Technisearch Ltd
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 Technisearch Ltd filed Critical Technisearch Ltd
Publication of NZ238185A publication Critical patent/NZ238185A/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01KSTEAM ENGINE PLANTS; STEAM ACCUMULATORS; ENGINE PLANTS NOT OTHERWISE PROVIDED FOR; ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES
    • F01K25/00Plants or engines characterised by use of special working fluids, not otherwise provided for; Plants operating in closed cycles and not otherwise provided for
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01KSTEAM ENGINE PLANTS; STEAM ACCUMULATORS; ENGINE PLANTS NOT OTHERWISE PROVIDED FOR; ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES
    • F01K27/00Plants for converting heat or fluid energy into mechanical energy, not otherwise provided for
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D1/00Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D15/00Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies
    • F28D15/02Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D15/00Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies
    • F28D15/02Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes
    • F28D2015/0291Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes comprising internal rotor means, e.g. turbine driven by the working fluid

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Description

238185 fiiorily Da:.;. . u..v.»w V CYS^l rh^: F.^O^SIOT-j F2-SOl\o=>; f.Q A Y^lS\ <^0; . <r O\V-2-Tl\ oo. . 2 3 DEC 1993 P.O. Jourrso.. l"SlS" NEW ZEALAND PATENTS ACT, 1953 No.: Date: COMPLETE SPECIFICATION THERMOSYPHON * *T * {($ 2*lt 'AYf99j4 • ■ $ I V Xfwc, TECHNISEARCH LTD., a company incorporated in the State of Victoria, Australia of 449 Swanston Street, Melbourne, Victoria 3000, Australia hereby declare the invention for which/f*/ we pray that a patent may be granted to pa€7us, and the method by which it is to be performed, to be particularly described in and by the following statement: - The present invention relates to gravity assisted heat pipes or thermosyphons.
A heat pipe usually comprises an elongate sealed cylinder containing a vaporisable material having liquid and vapour phases at the temperatures of operation of the heat pipe. Heat applied to one end portion of the cylinder, known as the evaporator section, vaporises the liquid. The vapour then flows 10 in a high speed stream to the other end portion of the cylinder, known as the condenser section, which is maintained at a lower temperature than the evaporator section causing the vapour to condense whereby heat is given off. The heat pipe provides very efficient heat transfer between a higher temperature zone surrounding the evaporator section and a lower temperature 15 zone surrounding the condenser section. The temperature difference between the two sections need not be substantial. The vapour condenses in the condenser section and is returned to the evaporator section by means of the capillary action of a wick structure affixed to the inner surface of the cylinder. The evaporation rate, and consequently the heat transfer rate, is determined by 20 the amount of liquid available for evaporation in the evaporator section. The rate of return of the condensate is thus a limiting factor in the operation of the heat pipe and, in some instances, a fluid pump is required to enhance this return rate. A thermosyphon is a simple form of heat pipe where the return of the condensate from the condenser section to the evaporator section is 25 achieved by gravity. Therefore thermosyphons are also called gravity assisted heat pipes.
Various proposals have been made to convert the thermal energy of the vapour stream into electrical energy by placing a turbine, connected to a 30 generator, in the path of the vapour stream. The higher the kinetic energy of the vapour as it flows through the turbine the greater the electricahpower produced. The present invention seeks to provide a thermosyphon turbine.^ 910517,paw001.techn.spe ,2 2381 system in which the kinetic energy of the vapour is increased so as to obtain a higher electrical (or mechanical) power output.
The present invention seeks also to provide an effective, simple and passive 5 liquid return system from the condenser low pressure environment to the evaporator section which is at a higher pressure.
According to the present invention there is provided a thermosyphon comprising an enclosure containing a vaporisable material, said enclosure 10 comprising an evaporator section at a lower end portion wherein the material is heated and vaporised, an adiabatic section through which the vapour flows, a condenser section at an upper end portion wherein the vapour condenses, collection means to collect the condensate, at least one return pipe to return the condensate from the collection means to the evaporator section, separator 15 means separating the evaporator section from the condenser section to thereby, in use, provide a differential pressure therebetween, the separator means having at least one aperture for flow therethrough of the vapour, and a turbine mounted downstream of the separator means to be driven by the vapour stream flowing through the aperture.
The separator means supports the pressure difference between the evaporator and condenser sections to enable a high velocity flow out of the nozzles.
The thermosyphon finds particular utility in the production of energy, from 25 such diverse low temperature heat sources as solar ponds and geothermal systems and the structure of the enclosure may be rigid or part flexible depending on the particular application.
Alternatively, provided that the portion of the enclosure adjacent the turbine is substantially rigid so as not to interfere with the rotation of the turbine, one or more of the other portions of the enclosure may be flexible. Thus, for example, if the thermosyphon is to be used to produce energy from a non-linear 5 geothermal bore, portions of the enclosure, such as the evaporator and adiabatic sections, may be flexible so as to allow the thermosyphon to be positioned in the bore passage. The return pipe in such cases should also be flexible so as to accomodate the flexibility of the enclosure.
The collection means is preferably an annular channel provided around the periphpery of the interior of the enclosure. The term annular refers not only to a circular formation but also to other formations, such as rectangular.
Advantageously, the aperture either forms or carries a nozzle to increase the 15 kinetic energy of the vapour stream. The nozzle may also be used to direct the vapour stream at an optimum angle onto the blades of the turbine to improve efficiency.
The turbine may be coupled to an electrical generator. If the electrical 20 generator is located outside the enclosure a shaft or similar means associated with the turbine will be required to drive the generator. Difficulties in sealing the enclosure may result due to the pressures within the enclosure and, accordingly, the electrical generator is preferably located within the enclosure. The power produced by the generator may then be easily transferred to the 25 exterior through a sealed gland.
Alternatively, or in addition to electrical power, mechanical power may be transferred out of the enclosure using a magnetic coupling between the turbine and an external device driven by the turbine.
The invention will now be further described by way of example only with reference to the accompanying drawing, the sole figure of which is a cross-.^ T £ !! 7, 910517,patt001.techn.spe,4 ^ 9 \\ 38185 sectional view of a thermosyphon in accordance with a preferred embodiment of the invention.
Referring to the figure, the thermosyphon of the preferred embodiment 5 comprises a substantially vertical elongate enclosure 1 preferably of cylindrical form and comprising an evaporator section A containing a working liquid reservoir 2 at its lower end, a condenser section C at the upper end, and an adiabatic section B disposed between the evaporator section A and the condenser section C. To minimise potential heat losses in the adiabatic 10 section B it may be provided with thermal insulation 3.
An annular condensate collection channel 9 is provided around the inner periphery of the cylinder. A separator plate 5 is disposed below the channel 9 between the condenser section C and the adiabatic section B. The diameter of 15 the separator plate 5 is the same as the diameter of the enclosure 1. The plate 5 has one or more apertures which either form or carry nozzles 7 which provide passageways through which a vapour stream may flow. The separator plate 5 has the effect of supporting the pressure difference between the evaporator section A and the condenser section C and enabling high velocity 20 flow out of the nozzles 7.
A turbine 13, directly coupled to an electrical generator 15, is axially mounted downstream of the separator plate 5. The diameter of the turbine 13 should be such that condensed vapour can drain freely past the turbine 13 into the 25 channel 9.
Extending from the bottom of the channel 9, through the separator plate 5 and terminating in the evaporator section A are one or more liquid return pipes 11. These return pipes 11 transport condensed vapour from the channel 9 to 30 the liquid reservoir 2. " ' ■ 4 t- Heat is supplied to the evaporator section A from a suitable energy source and is absorbed by the working liquid. A solar pond can provide a relatively low cost means of collecting solar energy, and could be used as a heat source for the thermosyphon. Thermal energy generated by other ♦ypes of solar collectors 5 can also be used. Geo-thermal energy and waste heat can also be used as heat sources. As the liquid vaporises the heat is taken up as latent heat of vaporisation. The vapour then expands adiabatically in the nozzles 7 from the high pressure and temperature at the evaporator section A to the lower pressure and temperature at the condenser section C where it cools and 10 condenses. The speed achieved by the vapour stream at the nozzle exit is dependent on the pressure difference between the evaporator section A and the condenser section C, and in some instances may reach the speed of sound.
As the vapour stream expands through the nozzles 7 its kinetic energy, and 15 hence its speed, increases. The shape and size of the nozzles are chosen to maximise the increase in kinetic energy. The vapour, with its speed increased by the passage through the nozzles 7, impinges on the blades of the turbine 13 and provides a force which rotates the turbine, which in turn drives the generator 15. The nozzles 7 are arranged to direct the vapour stream onto the 20 turbine blades at the optimum angle required to produce the maximum electrical power extraction. The generator 15 is located within the thermosyphon, and is provided with conducting wires, which exit the thermosyphon through a sealed gland, to conduct the generated current to the exterior of the thermosyphon. The loss in energy resulting from the work done 25 on the turbine by the vapour stream may cause some of the vapour to condense, and the cyclone action of the turbine 13 separates this liquid from the vapour. This liquid collects in the channel 9 and combines with the liquid draining from the condenser section C. The combined liquid is then returned to the evaporator section A via the return pipe 11, and the cycle is repeated. -ovi 910517, pawd01.techn.spe, 6 ICC K'.' The hydrostatic pressure head in the return pipes 11 must be such that it maintains the flow of liquid from the lower pressure condenser section C to the higher pressure evaporator section A, with the return rate of the liquid matching the evaporation rate. The configuration of the return pipes should be 5 such that vapour or liquid from the evaporator section A is prevented from flowing through the pipes. In the embodiment shown this is provided by a U-shaped portion at the lower end of each pipe. Alternatively, the return pipes may be provided with a non-return valve. The return system is gravity based. The difference in height between the free surface of the returning liquid 10 and the upper surface of liquid reservoir 2 should be greater than the required hydrostatic head in pipe 11 to compensate for the pressure difference between the evaporator section A and the condenser C and also to overcome the fluid friction losses in pipe 11.
The embodiment has been described by way of example only and modifications are possible within the scope of the invention.

Claims (14)

J I -8- TIIE CLAIMS- WHAT#WE CLAIM IS
1. A thermosyphon comprising an enclosure containing a vaporisable material, said enclosure comprising an evaporator section at a lower end portion wherein the material is heated and vaporised, an adiabatic section through which the vapour flows, a condenser section at an upper end portion wherein the vapour condenses, collection means to collect the condensate, at least one return pipe to return the condensate from the collection means to the evaporator section, separator means separating the evaporator section from the condenser section to thereby, in use, provide a differential pressure therebetween, the separator means having at least one aperture for flow therethrough of the vapour, and a turbine mounted downstream of the separator means to be driven by the vapour stream flowing through the aperture.
2. A thermosyphon according to claim 1, wherein the enclosure is substantially rigid.
3. A thermosyphon according to claim 1, wherein at least a portion of the enclosure other than that adjacent the turbine is flexible.
4. A thermosyphon according to any one of the preceding claims, wherein the collection means is adjacent the separator means.
5. A thermosyphon according to any one of the preceding claims, wherein the separator means is above the adiabatic section.
6. A thermosyphon according to any one of the preceding claims, wherein the collection means comprises an annular channel open towards the condenser section provided around the periphery of the interior of the enclosure. -9 -
7. A thermosyphon according to claim 5 or claim 6, wherein in separator means is of plate like form.
8. A thermosyphon according to any one of the preceding claims, wherein the aperture either forms or carries a nozzle to increase the kinetic energy of the vapour stream.
9. A thermosyphon according to any one of the preceding claims, wherein the return pipe is configured so as to prevent the vapour or liquid from the evaporator section from flowing therethrough.
10. A thermosyphon according to claim 8, wherein the lower end of the return pipe is U-shaped.
11. A thermosyphon according to any one of claims 1 to 8, wherein the return pipe is provided with a non-return valve so as to prevent the vapour or liquid from the evaporator section from flowing therethrough.
12. A thermosyphon according to any one of the preceding claims further comprising an electrical generator located within the enclosure and coupled to the turbine.
13. A thermosyphon according to any one of the preceding claims, wherein the turbine is magnetically coupled to an external device to transfer mechanical power out of the enclosure. 910517, paw001.techn.spe, 9 238185 - 10
14. A thermosyphon subtsantially as hereinbefore described with reference to Che accompanying drawing. MTED THK pfejh CAy 0F _A.J. PARK & SON PER AGbW ici rOR THE APPLICANTS | -:T OFFICE j ; 2 r-Cf 1833 | 910M7,pro<)0l.u!clnL3perlfl' * : I
NZ238185A 1990-05-18 1991-05-17 Heat pipe with vapour driven turbine. NZ238185A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
AUPK020190 1990-05-18

Publications (1)

Publication Number Publication Date
NZ238185A true NZ238185A (en) 1993-12-23

Family

ID=3774692

Family Applications (1)

Application Number Title Priority Date Filing Date
NZ238185A NZ238185A (en) 1990-05-18 1991-05-17 Heat pipe with vapour driven turbine.

Country Status (2)

Country Link
AU (1) AU644873B2 (en)
NZ (1) NZ238185A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1993005348A1 (en) * 1991-08-30 1993-03-18 Robert Kenneth Prudhoe Vacuum panel heat exchangers (vphe)
CN102759142A (en) * 2011-04-29 2012-10-31 姚福来 Heat-pipe heating and heat-pipe power generation method for cold regions

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU571769B2 (en) * 1985-03-26 1988-04-21 Fujikura Ltd. Heat pipe with inbuilt turbine

Also Published As

Publication number Publication date
AU644873B2 (en) 1993-12-23
AU7716991A (en) 1991-11-21

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