EP3314176A1 - Temperiereinheit für ein gasförmiges oder flüssiges medium - Google Patents
Temperiereinheit für ein gasförmiges oder flüssiges mediumInfo
- Publication number
- EP3314176A1 EP3314176A1 EP16735834.0A EP16735834A EP3314176A1 EP 3314176 A1 EP3314176 A1 EP 3314176A1 EP 16735834 A EP16735834 A EP 16735834A EP 3314176 A1 EP3314176 A1 EP 3314176A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- base body
- temperature
- unit according
- cooling
- heat sink
- Prior art date
- Legal status (The legal status 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 status listed.)
- Withdrawn
Links
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B21/00—Machines, plants or systems, using electric or magnetic effects
- F25B21/02—Machines, plants or systems, using electric or magnetic effects using Peltier effect; using Nernst-Ettinghausen effect
- F25B21/04—Machines, plants or systems, using electric or magnetic effects using Peltier effect; using Nernst-Ettinghausen effect reversible
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B21/00—Machines, plants or systems, using electric or magnetic effects
- F25B21/02—Machines, plants or systems, using electric or magnetic effects using Peltier effect; using Nernst-Ettinghausen effect
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M31/00—Apparatus for thermally treating combustion-air, fuel, or fuel-air mixture
- F02M31/02—Apparatus for thermally treating combustion-air, fuel, or fuel-air mixture for heating
- F02M31/12—Apparatus for thermally treating combustion-air, fuel, or fuel-air mixture for heating electrically
- F02M31/125—Fuel
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23K—FEEDING FUEL TO COMBUSTION APPARATUS
- F23K1/00—Preparation of lump or pulverulent fuel in readiness for delivery to combustion apparatus
- F23K1/04—Heating fuel prior to delivery to combustion apparatus
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23K—FEEDING FUEL TO COMBUSTION APPARATUS
- F23K5/00—Feeding or distributing other fuel to combustion apparatus
- F23K5/002—Gaseous fuel
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23K—FEEDING FUEL TO COMBUSTION APPARATUS
- F23K5/00—Feeding or distributing other fuel to combustion apparatus
- F23K5/02—Liquid fuel
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- H—ELECTRICITY
- H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10N—ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10N10/00—Thermoelectric devices comprising a junction of dissimilar materials, i.e. devices exhibiting Seebeck or Peltier effects
- H10N10/10—Thermoelectric devices comprising a junction of dissimilar materials, i.e. devices exhibiting Seebeck or Peltier effects operating with only the Peltier or Seebeck effects
- H10N10/17—Thermoelectric devices comprising a junction of dissimilar materials, i.e. devices exhibiting Seebeck or Peltier effects operating with only the Peltier or Seebeck effects characterised by the structure or configuration of the cell or thermocouple forming the device
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23K—FEEDING FUEL TO COMBUSTION APPARATUS
- F23K2300/00—Pretreatment and supply of liquid fuel
- F23K2300/10—Pretreatment
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23K—FEEDING FUEL TO COMBUSTION APPARATUS
- F23K2400/00—Pretreatment and supply of gaseous fuel
- F23K2400/10—Pretreatment
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B2321/00—Details of machines, plants or systems, using electric or magnetic effects
- F25B2321/003—Details of machines, plants or systems, using electric or magnetic effects by using thermionic electron cooling effects
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B2321/00—Details of machines, plants or systems, using electric or magnetic effects
- F25B2321/02—Details of machines, plants or systems, using electric or magnetic effects using Peltier effects; using Nernst-Ettinghausen effects
- F25B2321/023—Mounting details thereof
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B2321/00—Details of machines, plants or systems, using electric or magnetic effects
- F25B2321/02—Details of machines, plants or systems, using electric or magnetic effects using Peltier effects; using Nernst-Ettinghausen effects
- F25B2321/025—Removal of heat
- F25B2321/0251—Removal of heat by a gas
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B2321/00—Details of machines, plants or systems, using electric or magnetic effects
- F25B2321/02—Details of machines, plants or systems, using electric or magnetic effects using Peltier effects; using Nernst-Ettinghausen effects
- F25B2321/025—Removal of heat
- F25B2321/0252—Removal of heat by liquids or two-phase fluids
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D7/00—Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
- F28D7/04—Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being spirally coiled
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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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Definitions
- the subject invention relates to a temperature control unit for tempering a gaseous or liquid medium by means of a number of thermoelectric modules, which are arranged between a base body and a heat sink, and in the base body a media line is arranged through which flows through the gaseous or liquid medium, wherein the media line is arranged guided in the base body in the form of a catchy spiral from outside to inside.
- thermoelectric modules thermoelectric modules
- This device is also aimed specifically at the conditioning of liquid fuels.
- gaseous fuels such as natural gas or hydrogen
- the gaseous fuel is typically under high pressure and, consequently, for use as fuel in an internal combustion engine, it must first be depressurized to a required, lower pressure .
- the gaseous fuel such as natural gas
- the fuel cools down sharply, which can be problematic for subsequent components of the conditioning, for example, by condensation and icing of the gas lines or other components in the gas line. Therefore, the gaseous fuel is usually heated prior to relaxing, so that the relaxation results in a desired temperature of the fuel.
- the temperature control of the gaseous fuel before relaxing must be highly dynamic to the temperature after the relaxation and to be able to keep constant before the flow measurement.
- the required heating power for controlling the temperature of the fuel is also heavily dependent on the current flow, which also makes a highly dynamic temperature control required with rapidly changing flow rates.
- such a highly dynamic temperature control requires a control method which is capable of carrying out highly dynamic (in terms of rapid temperature changes) control interventions and, on the other hand, a temperature control unit which is also able to implement the highly dynamic control interventions. Consequently, such a temperature control unit must be able to impress the required temperature changes on the fuel flowing through in a very short time.
- high temperature stability is also desirable, even if under certain circumstances no high demands are placed on the dynamics of the temperature. be made because of certain applications, a highly accurate and highly stable temperature control is required.
- These requirements require a temperature control unit with a high heating and cooling capacity, which may also be necessary to change quickly between heating and cooling. Apart from that, a precise temperature control must be possible in order to avoid excessive overheating (either overheating or overcooling).
- US 6,502,405 B1 shows a heat exchanger element with Peltier elements for heating or cooling fuel in a vehicle.
- the heat exchanger element consists of a heat conducting block in which a fuel line is inserted meandering and which is thermally insulated on a first side.
- Peltier elements which are thermally connected to a heat sink, are arranged on the second side of the heat-conducting block.
- the heat sink is typically designed with a large surface area and small mass of memory to maximize heat dissipation capacity.
- a fan is still arranged on the heat sink in order to increase the heat dissipation capacity even further.
- 6,502,405 B1 is also designed for a low thermal storage mass in order to be able to dissipate heat quickly to the environment via the heat sink. Due to the meandering guidance of the fuel in the heat exchanger element but it also leads to an uneven heating of the fuel, which makes the temperature control difficult, since the Peltier elements are all driven with the same supply voltage. The uneven heating results in a higher temperature difference between the outlet temperature of the medium and the surface of the Peltier elements, which in turn leads to a lower maximum outlet temperature of the medium, since the Peltier elements can not be heated arbitrarily. Or it results in a lower maximum flow rate for a given outlet target temperature.
- a temperature control unit for the temperature control of a liquid flow which has a main heat exchanger, a heat exchanger and interposed Peltier elements.
- a media line for controlling the temperature of a liquid flow is arranged in the main heat exchanger and is guided spirally from outside to inside. In this case, a pre-tempering takes place in the heat-auxiliary exchanger and the Peltier elements are used for precise and rapid adjustment of a desired temperature.
- thermoelectric modules are arranged in several rows on the base body, wherein the Modulflower subtitle a radially further outer thermoelectric module is greater than the Modulflower exchange a radially further inside thermoelectric module.
- the inflowing medium from the outside can be tempered in the radially outer region with high heat output, which enables strong and rapid temperature changes.
- a module heat output of a thermoelectric module is understood to be both the rated output at a nominal voltage and a nominal current, as well as the output at a specific supply voltage that deviates from the rated voltage or a specific one that deviates from the rated current Supply current sets.
- the modules are preferably coordinated so that the temperature spread at maximum flow between module surface and medium outlet temperature is minimal. As has been shown, this is the case when all modules have almost the same surface temperature. Due to the circumferential arrangement, the thermoelectric modules within a row of the house are almost at the same temperature. Only the different rows would have to be adjusted in this respect, which, in contrast to a meandering arrangement of the media line, represents a substantial simplification since it is no longer necessary to adjust all thermoelectric modules for the same result (minimum temperature spread).
- the module heating power can be optimally adapted to the conditions and it can be installed radially inside modules with smaller module heating.
- the heating power in the radially outer region of the basic body is greater than the heating power in the radially inner region of the basic body, as the sum of the modulus heating capacities.
- the temperature of the medium can also be optimized by the arrangement and selection of the Modulflower according to the invention.
- the number of thermoelectric modules is arranged in a plurality of rows on the main body and the module heating power of a radially outer thermoelectric module is set greater than the Modulflower electrode a radially further inside thermoelectric module.
- the adjustability of the module heating power can be achieved both by the choice of modules with different nominal powers and by different supply voltage or current values.
- thermoelectric module can also cover several spiral paths, which improves the efficiency of the temperature control unit and the uniformity of the heating. This allows a particularly highly dynamic, accurate and stable temperature control of the medium can be achieved.
- the mass ratio of the thermal storage mass of the heat sink to the thermal storage mass of base body and disposed therein media line in the range of 0.5 to 1, advantageously in the range of 0.7 to 0.8, and very particularly advantageous with 0 , 75 is chosen. It has been found that for a highly dynamic temperature control of a medium by means of a tempering unit according to the preamble of claim 1, especially when a rapid and frequent change in the direction of the heat flow is required, too low a storage mass, as suggested by the prior art, disadvantageous is. Surprisingly, it has been found that a certain mass ratio between the mass of the heat sink and the mass of the main body together with the media line arranged therein is advantageous for the temperature control.
- a compact embodiment of the temperature control unit is obtained if a groove is provided in the main body into which the media line is pressed.
- the base body is advantageously surrounded by a base body shell, wherein over the circumference of the base body a plurality of radial connecting webs are arranged, which are connected to the base body shell. This also increases the efficiency of the temperature control unit. This can be further improved if the body shell is made partially hollow, since thus an even better thermal insulation between the body and the environment is achieved.
- cooling line in the heat sink, through which, as required, cooling medium flows to cool the heat sink in order to be able to dissipate heat more quickly from the heat sink.
- the cooling line is advantageously arranged spirally again.
- the tempering unit 1 shows a perspective view of the temperature control unit 1 according to the invention.
- the tempering unit 1 consists of a base body 2, to which any fastening elements 3, such as, for example, feet in the exemplary embodiment shown, can be provided for fastening the tempering unit 1.
- a thermal insulation element 4 is arranged and on the opposite second side, a heat sink 5.
- a media line 6 is performed, through which a gaseous or liquid medium, such as fuel, flows in the Temperper 1 is tempered to a desired temperature.
- the media line 6 has for this purpose an input terminal 10 and an output terminal 1 1, whereby the flow direction of the medium is determined by the temperature control unit 1 (indicated in Figure 1 by the arrows).
- thermoelectric module 7 is a semiconductor element which is arranged between a first heating surface 9a (not visible in FIG. 2) facing the main body 2 and a second heating surface 9b (here facing the heat sink). Depending on the polarity of the electrical voltage supplied to the semiconductor element, either the first heating surface 9a is warmer than the second heating surface 9b, or vice versa.
- thermoelectric module 7 depending on the polarity of the supply voltage, which is supplied for example via the terminals 8, both heated and cooled.
- Heating here means that the base body 2 heat is supplied and “cooling” that the main body 2 heat is removed.
- thermoelectric modules 7 are via a first heating surface 9a (not visible in Figure 2) directly or indirectly (for example via a heat transfer element to improve the heat conduction) in thermal contact with the main body 2.
- the heat sink 5 is on the second heating surface 9b of the thermoelectric module and is in thermally conductive contact, again directly or indirectly, with this second heating surface 9b.
- the heat sink 5 and the main body 2 are not arranged adjacent to each other in order to avoid a direct thermally conductive contact between the heat sink 5 and the main body 2 (as shown in Figure 1).
- the basic body 2 is shown in detail in FIGS. 3 and 4, which show different views of the main body 2. 3 shows the side of the main body 2, on which the thermoelectric modules 7 are arranged.
- the main body 2 is essentially formed from a base plate 20, which is surrounded along its circumference by a main body shell 21.
- the main body shell 21 is connected via radial connecting webs 22 with the base plate 20, wherein the connecting webs 22 are arranged distributed over the circumference of the base plate 20.
- cavities 23 are formed, which act as thermal insulation between the base plate 2 and the main body shell 21.
- the main body shell 21 may additionally be made partially hollow by 21 circumferential slots 24 are incorporated in the main body shell, which also form cavities for additional thermal insulation.
- the other side of the base body 2 is shown.
- a preferably spiral groove 25 is formed, in the assembled state, the media line 6 is pressed.
- the groove 25 forms in the base body 2 a catchy planar spiral (Archimedean spiral, logarithmic spiral).
- the media line 6 is preferably guided spirally inwards from the outside and emerges from the temperature control unit 1 in the central inner region of the base plate 20, the media line 6 being deflected out of the plane of the spiral when exiting, preferably by about 90 ° the media line 6 easy to be able to lead out of the temperature control unit 1. In principle, however, any other guidance of the media line 6 in the main body 20 is conceivable.
- the medium is thus supplied radially on the outside via the input terminal 10 and discharged radially outside via the output terminal 1 1.
- the double-flighted spiral has the advantage that the media line 6 does not have to be deflected out of the plane of the spiral, which is easier to manufacture.
- the double-flighted spiral has the disadvantage that the inflowing medium cools the outflowing medium, which requires a little more power and a less uniform heating is feasible. The temperature spread gets bigger, but the thermoelectric modules of a series, in the case of tuned modules, are still at approximately the same temperature.
- the catchy or double-flighted spiral need not necessarily be designed as a circular spiral, but may also have other shapes, such as rectangular, square, etc., have. Due to the spiral shape, the temperature control unit 1 can be made very compact, since the spiral passages can be arranged close to each other. This can be accommodated in a small space a lot of meters on the media line 6, which increases the available surface for temperature control of the medium flowing through the media line 6 medium.
- a meandering guide the media line would be disadvantageous in this regard, since the required bending radii for a dense packing are considerably smaller than in a spiral course. With increasing pressure requirements on the part of the media line 6 increases due to the required wall thickness increase usually also the minimum bending radius. A meander-shaped guide therefore has a particularly disadvantageous effect on high pressure requirements, as in the present case.
- thermo insulation element 4 shows still the thermal insulation element 4 with the advantageous catchy spiral-shaped media line 6, which is pressed into the base body 20 in the assembled state.
- the thermal insulation element 4 ensures that the heat introduced by the thermoelectric modules 7 into the base plate 20 remains concentrated therein and is not released via the end face of the temperature control unit 1 to the environment.
- thermoelectric modules 7 are preferably circular, or adapted to the spiral shape, and arranged in several rows (ie at different radial distances) on the base plate 20 ( Figure 2). As a result, more thermoelectric modules 7 can be arranged radially on the outside due to the resulting larger circumference.
- the inflowing medium is thus tempered in the radially outer region with high heating power (sum of the module heat outputs of the radially outer modules 7 involved), which enables strong and rapid changes in temperature. It is further advantageous if a thermoelectric module 7, which is arranged radially further inwards, has a lower module heating power than a thermoelectric module 7, which is arranged radially further outward.
- thermoelectric modules 7 After the media line 6 is preferably guided in a spiraling manner inwards, fewer and weaker (in the sense of less module heating power) thermoelectric modules 7 extend radially inwards for temperature control of the medium.
- the radially inward necessary heating power (sum of the module heat outputs of the participating radially inner modules 7) is thus lower than the heating power in the radially outer region. This allows the temperature of the medium can also be optimized by the arrangement and selection of the module heating power of the individual thermoelectric modules 7 and it can be a very uniform heating of the medium can be achieved.
- thermoelectric module heat output of a thermoelectric module 7 is generally understood to mean the rated output at a rated current / nominal voltage, as well as the power which occurs at a specific current / voltage deviating from the rated current / nominal voltage. Accordingly, according to the invention, on the one hand, thermoelectric modules 7 with different power ratings, differently adjustable thermoelectric modules 7 with different or the same power ratings or combinations thereof can be used.
- thermoelectric module 7 If an electrical supply voltage is applied to a thermoelectric module 7, as is known, one of the heating surfaces 9a, 9b of the thermoelectric module 7 is cooled, while at the same time the opposing heating surface 9a, 9b is heated.
- the maximum temperature spread between the heating surfaces 9 a, 9 b depends on the operating temperature (temperature at the warmer heating surface) of the thermoelectric module 7. The higher the operating temperature, the higher the maximum achievable temperature spread between cold and hot heating surface 9a, 9b. Thus, with available thermoelectric modules 7 temperatures of up to 200 ° C can be achieved on the hot heating surface, the cold heating surface does not exceed 100 ° C. By simply reversing the supply voltage, a highly dynamic control of the temperature is made possible.
- This control is supported in the temperature control unit 1 according to the invention by the heat sink 5 in the heating mode, so when the medium is to be heated in the media line 6, is used as a buffer memory.
- the thermal storage mass is not as small as possible, as suggested in the prior art, but a certain storage mass is desired in order to be able to realize this.
- the mass ratio of the thermal storage mass of the heat sink 5 to the thermal storage mass of the base body 2 and disposed therein media line 6 in the range of 0.5 to 1, advantageously 0.7 to 0.8, is selected.
- a particularly advantageous temperature controllability of the temperature control unit 1 was found at a mass ratio in the range of 0.75, or at a mass ratio of 0.75.
- a tempering unit 1 that was tested had a thermal storage mass of the heat sink 5 of 5.4 kg and a thermal storage mass of the base body 2 and the media line 6 arranged therein of 7.2 kg, which resulted in a mass ratio of 0.75.
- the mass of the base body shell 21 is not calculated to the thermal storage mass of the body.
- the insulation element 4 is not part of the thermal storage mass of the main body 2.
- This cached thermal energy is the temperature control or the temperature control unit 1 as a support available when more thermal energy is required to control the temperature of the medium again. In this case, the supply voltage would be raised again, whereby the temperature spread at the thermoelectric modules 7 increases again.
- the temperature at the heating surface 9b, against which the heat sink 5 abuts decreases with respect to the temperature of the heat sink 5.
- thermoelectric modules 7 Due to the thermal storage mass of the heat sink 5 can thus be reacted very quickly and accurately with the temperature control unit 1 to load changes or temperature changes and a typical overheating can be largely avoided.
- the thermal storage mass of the heat sink 5 with respect to the thermal storage mass of the base body 2 and disposed therein media line 6 but not too large or too small.
- the total surface of the heat sink 5 should be designed as a function of the expected operating temperature so that the heat stored in the heat sink 5 is not released too quickly to the surface, but remains sufficiently long stored in the heat sink 5.
- the surface is thus not as large as possible and optimized to dissipate the heat as in conventional heat sinks, but on the contrary so that the heat is stored in the heat sink 5.
- a complete thermal insulation of the heat sink 5 from the environment would also be disadvantageous because in the case of frequent reversals, the temperature could heat up in the heat sink 5.
- the material of the media line 6 and the heating power of the thermoelectric modules 7 or the module heating powers of the thermoelectric modules 7 are to be adapted.
- the general basic principle with the heat sink 5 as a storage mass to support the temperature control unit 1 remains untouched.
- the tempering unit 1 generally only needs to preheat the gaseous medium. Cooling of these gases by the temperature control unit 1 is usually not required. Thus, it is usually sufficient for these applications to work only with the temperature spread of the thermoelectric modules 7. A reversal to change from heating to cooling is rather unnecessary. Other gaseous media such as hydrogen, do not show this pronounced effect of strong cooling by the necessary pressure release. On the contrary, it may also come to a warming by the pressure release. When tempering liquid media often no pressure release is necessary because the liquid medium is already present with the right pressure.
- the temperature control unit 1 For gases without pronounced Joules Thomson effect or liquid media, the temperature control unit 1 must therefore often switch between heating and cooling the gaseous medium in order to keep the temperature constant depending on the pressure and the flow. In particular, during cooling, it may be that due to the lower surface of the heat sink 5, the resulting heat, especially the waste heat of the thermoelectric modules 7, can not be dissipated quickly enough. Therefore, when using the temperature control unit 1 with such gaseous or liquid media, it may also be provided to additionally cool the heat sink 5 as required. For this purpose, a cooling line 12 may be introduced into the heat sink 5, is passed through the cooling liquid for additional cooling of the heat sink 5. Such an embodiment is indicated in Fig.7.
- the cooling line 12 can again be arranged in the heat sink 5 in the form of a catchy or double-flighted spiral, as described above with respect to the media line 6.
- the heat sink 5 can also be designed in several parts in order to be able to introduce the cooling line 12.
- other embodiments of the cooling line 12 are conceivable.
- grooves 31 are incorporated in a heat sink main body 30, for example milled in to form the cooling line 12.
- the grooves 31 are vorzugswiese as described spirally incorporated.
- the heat sink main body 30 with the grooves 31 is covered with a heat sink cover 32 to form the heat sink 5.
- cooling line 12 would also be part of the thermal storage mass of the heat sink fifth
- ademediumzu semiconductoran gleich 34 and ademediumab technologicalan gleich 33 may be provided on the heat sink.
- the cooling medium is supplied from the inside and discharged centrally outside.
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- 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)
- Control Of Temperature (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| ATA50532/2015A AT516611B1 (de) | 2015-06-23 | 2015-06-23 | Temperiereinheit für ein gasförmiges oder flüssiges Medium |
| PCT/EP2016/064300 WO2016207153A1 (de) | 2015-06-23 | 2016-06-21 | Temperiereinheit für ein gasförmiges oder flüssiges medium |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| EP3314176A1 true EP3314176A1 (de) | 2018-05-02 |
Family
ID=56320661
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP16735834.0A Withdrawn EP3314176A1 (de) | 2015-06-23 | 2016-06-21 | Temperiereinheit für ein gasförmiges oder flüssiges medium |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US20180164003A1 (de) |
| EP (1) | EP3314176A1 (de) |
| JP (1) | JP2018520331A (de) |
| KR (1) | KR20180020240A (de) |
| CN (1) | CN107995946A (de) |
| AT (1) | AT516611B1 (de) |
| WO (1) | WO2016207153A1 (de) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| AT516385B1 (de) * | 2015-06-23 | 2016-05-15 | Avl List Gmbh | Temperiereinheit für ein gasförmiges oder flüssiges Medium |
| AT524204B1 (de) | 2021-01-05 | 2022-04-15 | Avl List Gmbh | Temperiervorrichtung für ein gasförmiges Medium |
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-
2015
- 2015-06-23 AT ATA50532/2015A patent/AT516611B1/de not_active IP Right Cessation
-
2016
- 2016-06-21 KR KR1020187001839A patent/KR20180020240A/ko not_active Withdrawn
- 2016-06-21 CN CN201680036272.4A patent/CN107995946A/zh not_active Withdrawn
- 2016-06-21 JP JP2017566852A patent/JP2018520331A/ja active Pending
- 2016-06-21 US US15/739,521 patent/US20180164003A1/en not_active Abandoned
- 2016-06-21 WO PCT/EP2016/064300 patent/WO2016207153A1/de not_active Ceased
- 2016-06-21 EP EP16735834.0A patent/EP3314176A1/de not_active Withdrawn
Also Published As
| Publication number | Publication date |
|---|---|
| US20180164003A1 (en) | 2018-06-14 |
| WO2016207153A1 (de) | 2016-12-29 |
| KR20180020240A (ko) | 2018-02-27 |
| CN107995946A (zh) | 2018-05-04 |
| AT516611B1 (de) | 2016-07-15 |
| JP2018520331A (ja) | 2018-07-26 |
| AT516611A4 (de) | 2016-07-15 |
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