DE102006004836A1 - Organic rankine cycle-turbo-generator, has generator section with stator housing that includes rotor chamber, which opens in direction of exhaust chamber of turbine section, where generator is provided between generator and turbine sections - Google Patents
Organic rankine cycle-turbo-generator, has generator section with stator housing that includes rotor chamber, which opens in direction of exhaust chamber of turbine section, where generator is provided between generator and turbine sections Download PDFInfo
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- DE102006004836A1 DE102006004836A1 DE102006004836A DE102006004836A DE102006004836A1 DE 102006004836 A1 DE102006004836 A1 DE 102006004836A1 DE 102006004836 A DE102006004836 A DE 102006004836A DE 102006004836 A DE102006004836 A DE 102006004836A DE 102006004836 A1 DE102006004836 A1 DE 102006004836A1
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- generator
- section
- turbine
- condensate
- stator
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Links
- 238000001816 cooling Methods 0.000 claims abstract description 12
- 239000012530 fluid Substances 0.000 claims abstract description 12
- 239000002826 coolant Substances 0.000 claims description 20
- 239000002244 precipitate Substances 0.000 abstract 1
- 238000004804 winding Methods 0.000 description 5
- 239000000314 lubricant Substances 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 238000013461 design Methods 0.000 description 3
- 238000012423 maintenance Methods 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- 230000001419 dependent effect Effects 0.000 description 2
- 239000012535 impurity Substances 0.000 description 2
- 238000013021 overheating Methods 0.000 description 2
- 125000006850 spacer group Chemical group 0.000 description 2
- 239000012808 vapor phase Substances 0.000 description 2
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000004821 distillation Methods 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000001704 evaporation Methods 0.000 description 1
- 230000008020 evaporation Effects 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 230000001050 lubricating effect Effects 0.000 description 1
- 238000005461 lubrication Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
- 238000005192 partition Methods 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
- 238000012549 training Methods 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K7/00—Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
- H02K7/08—Structural association with bearings
- H02K7/083—Structural association with bearings radially supporting the rotary shaft at both ends of the rotor
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K5/00—Casings; Enclosures; Supports
- H02K5/04—Casings or enclosures characterised by the shape, form or construction thereof
- H02K5/20—Casings or enclosures characterised by the shape, form or construction thereof with channels or ducts for flow of cooling medium
- H02K5/203—Casings or enclosures characterised by the shape, form or construction thereof with channels or ducts for flow of cooling medium specially adapted for liquids, e.g. cooling jackets
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
- F01D1/02—Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines
- F01D1/06—Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines traversed by the working-fluid substantially radially
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
- F01D15/10—Adaptations for driving, or combinations with, electric generators
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/18—Lubricating arrangements
- F01D25/22—Lubricating arrangements using working-fluid or other gaseous fluid as lubricant
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C1/00—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid
- F02C1/04—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid the working fluid being heated indirectly
- F02C1/05—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid the working fluid being heated indirectly characterised by the type or source of heat, e.g. using nuclear or solar energy
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K1/00—Details of the magnetic circuit
- H02K1/06—Details of the magnetic circuit characterised by the shape, form or construction
- H02K1/22—Rotating parts of the magnetic circuit
- H02K1/32—Rotating parts of the magnetic circuit with channels or ducts for flow of cooling medium
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/50—Bearings
- F05D2240/53—Hydrodynamic or hydrostatic bearings
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K7/00—Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
- H02K7/14—Structural association with mechanical loads, e.g. with hand-held machine tools or fans
Landscapes
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Life Sciences & Earth Sciences (AREA)
- High Energy & Nuclear Physics (AREA)
- Sustainable Development (AREA)
- Sustainable Energy (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Motor Or Generator Cooling System (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
Abstract
Description
Die Erfindung betrifft einen Organic Rankine Zyklus (ORC)-Turbogenerator in einer axialen Anordnung zwischen einem Turbinen-Dampfgehäuse und einem Generatorabschnitt nach dem Oberbegriff des Anspruchs 1.The This invention relates to an Organic Rankine Cycle (ORC) Turbogenerator in an axial arrangement between a turbine-steam housing and a Generator section according to the preamble of claim 1.
Der Organic Rankine Zyklus (ORC für engl. organic rankine cycle) ist ein thermodynamisches Verfahren zum Betrieb von Dampfturbinen mit einem anderen Arbeitsmittel als Wasser bzw. Wasserdampf. Als Arbeitsmedium werden bei diesem Kreisprozess meist organische Flüssigkeiten mit einer niedrigen Verdampfungstemperatur verwendet. Ein solches Verfahren wird vor allem dann eingesetzt, wenn das zur Verfügung stehende Temperaturgefälle zwischen Wärmequelle und Wärmesenke zu niedrig für eine mit Wasserdampf angetriebene Turbine ist. Ein derartiger Zyklus wird daher vorwiegend zur Stromerzeugung mit Hilfe der Geothermie, einer Kraft-Wärme-Kopplung, bei Solarteichkraftwerken oder Meereswärmekraftwerken eingesetzt.Of the Organic Rankine cycle (ORC for Engl. organic rankine cycle) is a thermodynamic process to operate steam turbines with a working fluid other than Water or water vapor. As a working medium in this cycle usually organic liquids used with a low evaporation temperature. Such a procedure is used especially when the available temperature gradient between heat source and heat sink too low for is a steam driven turbine. Such a cycle is therefore mainly used to generate electricity using geothermal energy, a cogeneration, used in solar power plants or marine thermal power plants.
Bei kleinen Anlagen mit einer Leistung von weniger als 500 kW sind die spezifischen Kosten einer Turbinen-Generatoreinheit in einer herkömmlichen Bauform zu groß. Im Gegensatz zu Dampfturbinen laufen die entsprechenden thermodynamischen Kreisprozesse bei einer wesentlich niedrigeren Temperatur ab. Dadurch besteht die Möglichkeit, die Turbine und den Generator zu einer Einheit zusammen zufassen. Dazu wird in einer bekannten Ausführungsform auf eine axiale Anordnung aus Turbine und Generator zurückgegriffen. Dabei ist das Schaufelrad der Turbine direkt auf der Generatorwelle befestigt. Die Befestigung wird bevorzugt als eine sich selbst zentrierende Befestigung, z.B. eine Hirtverzahnung ausgeführt. Die Turbinenwelle wird hierbei mittels einer Gleitringdichtung nach außen hin abgedichtet und führt direkt in den dahinter angekoppelten Generator.at small plants with a capacity of less than 500 kW are the specific cost of a turbine generator unit in a conventional Design too big. In contrast to steam turbines, the corresponding thermodynamic cycles take place at a much lower temperature. This exists the possibility, to combine the turbine and the generator into one unit. This is in a known embodiment to an axial Arrangement of turbine and generator used. That's it Paddle wheel of the turbine mounted directly on the generator shaft. The attachment is preferred as a self-centering Attachment, e.g. executed a shepherd toothing. The turbine shaft will sealed by means of a mechanical seal to the outside and leads directly in the generator connected behind it.
Derartige Ausführungsformen weisen jedoch das Problem auf, dass das Arbeitsmedium vor allem bei hohen Drehzahlen der Turbine durch die Gleitringdichtung an der Verbindungsstelle zwischen Turbine und Generator infolge von Materialermüdungen und daraus resultierenden Lecks der Gleitringdichtung nach außen dringen kann. Derartige Turbogeneratoren erfordern somit einen erhöhten Wartungsaufwand und damit einhergehende größere Unterhaltungskosten.such embodiments However, have the problem that the working medium especially in high speeds of the turbine through the mechanical seal at the Junction between turbine and generator due to material fatigue and resulting leaks of the mechanical seal penetrate to the outside can. Such turbogenerators thus require increased maintenance and associated greater maintenance costs.
Es besteht somit die Aufgabe, einen Turbogenerator zum Einsatz in einem ORC-Kreisprozess anzugeben, der einen robusten, wartungsarmen und auch bei sehr hohen Drehzahlen leckagesicheren Aufbau aufweist. Der geforderte Turbogenerator soll außerdem eine optimale innere Kühlung bei einem möglichst kompakten und platzsparenden Aufbau aufweisen.It Thus, the task is a turbogenerator for use in a ORC circular process specify a robust, low maintenance and also has leak-proof construction at very high speeds. The required Turbogenerator should also an optimal internal cooling at one possible have compact and space-saving design.
Die Aufgabe wird mit einem ORC-Turbogenerator mit den Merkmalen des Anspruchs 1 gelöst, wobei die Unteransprüche zweckmäßige bzw. vorteilhafte Ausführungsformen enthalten.The Task is with an ORC turbo generator with the characteristics of the Claim 1 solved, wherein the dependent claims appropriate or advantageous embodiments contain.
Erfindungsgemäß ist der ORC-Turbogenerator dadurch gekennzeichnet, dass der Generatorabschnitt ein zur Umgebung hin dichtes und druckfest ausgebildetes Statorgehäuse in Verbindung mit einem in Richtung des Abdampfraumes des Turbinenabschnittes offenen Läuferraum aufweist.According to the invention ORC turbogenerator characterized in that the generator section a close to the environment dense and pressure-resistant trained stator housing in conjunction with a in the direction of Abdampfraumes the turbine section open runner room having.
Im Gegensatz zu den aus dem Stand der Technik bekannten Ausführungsformen, bei denen der Turbinenabschnitt und der Generatorabschnitt strikt voneinander getrennt sind, bildet bei dem erfindungsgemäßen ORC-Turbogenerator der Stator des Generatorabschnittes zusammen mit der Außenhülle des Turbinenabschnitts eine durchgängige und zur Umgebung hin drucksichere und absolut dichte Hülle, während der Läuferraum im Inneren des Stators mit dem Abdampfraum in Verbindung steht.in the In contrast to the embodiments known from the prior art, in which the turbine section and the generator section strictly are separated from each other forms in the ORC turbogenerator according to the invention the stator of the generator section together with the outer shell of the generator section Turbine section a continuous and the environment pressure-resistant and absolutely tight shell, while the runners room inside the stator is in communication with the Abdampfraum.
Damit entfällt einerseits die Gleitlagerdichtung vollständig, wobei sich der Dichtungsaufwand an der Turbinenwelle beträchtlich verringert und höhere Drehzahlen des Turbogenerators erreicht werden können. Die Luftreibung im Läuferinnenraum zwischen Läufer und Stator wird durch den im Abdampfraum des Turbinenabschnitts herrschenden Unterdruck minimiert, wodurch sich die Laufleistung des Turbogenerators zusätzlich erhöht.In order to deleted on the one hand, the plain bearing seal completely, with the sealing effort the turbine shaft considerably decreased and higher Speeds of the turbo generator can be achieved. The air friction in the runner interior between runner and stator is through the in the Abdampfraum the turbine section minimized prevailing negative pressure, which increases the mileage of the Turbogenerators in addition elevated.
Die Lagerung einer Generatorwelle ist zweckmäßigerweise in Form mindestens eines durch das Kondensat des ORC-Arbeitsmittels geschmierten Gleitlagers ausgebildet. Das Gleitlager dient zur Lagerung sowohl des Läufers im Generatorabschnitt, als auch des im Turbinenabschnitt angeordneten Turbinenläufers. Durch den Einsatz des kondensierten und sich in der Dampfphase wieder selbst von Verunreinigungen scheidenden ORC-Arbeitsmediums als Schmiermittel wird ein auch nach längeren Benutzungszeiten hochreiner und ein autark wirkender Schmiermittelkreislauf geschaffen.The Storage of a generator shaft is expediently in the form of at least a lubricated by the condensate of the ORC working fluid plain bearing educated. The plain bearing serves for the storage of both the runner in Generator section, as well as arranged in the turbine section Turbine rotor. Through the use of the condensed and in the vapor phase again even impurity-separating ORC working fluid as a lubricant even after longer Useful periods of highly clean and self-sufficient lubricant circulation created.
Die Kühlung des Generatorabschnittes ist in Form einer durch das Kondensat des ORC-Arbeitsmediums durchströmten Kanalanordnung innerhalb des Läufers und/oder Stators ausgebildet. Dadurch wird zusätzlich ein hochreiner Kühlmittelkreislauf gebildet.The cooling the generator section is in the form of a condensate of the ORC working medium flowed through Channel arrangement within the rotor and / or stator formed. As a result, in addition a highly pure coolant circuit educated.
Der Läufer weist bei einer vorteilhaften Ausführungsform eine innerhalb der Generatorwelle eingebrachte zentrische Bohrung mit einem innerhalb der Bohrung stehenden, das Kondensat einleitenden Kühlrohr auf. Durch diese vorteilhafte Ausgestaltung wird ein Heißlaufen des Läufers durch eine Wärmeabfuhr durch das innerhalb des Läufers strömende ORC-Kondensat verhindert.In an advantageous embodiment, the rotor has a central bore introduced within the generator shaft with a condensate inside the bore Cooling tube on. This advantageous embodiment prevents overheating of the rotor due to heat dissipation by the ORC condensate flowing inside the rotor.
Zusätzlich dazu ist bei einer vorteilhaften Ausgestaltung mindestens eine, die zentrische Bohrung im Läufer mit der Gleitfläche des Gleitlagers verbindende und das Kondensat von der zentrischen Bohrung in das Gleitlager zuführende Gleitlagerbohrung vorgesehen. Die Schmierung des Gleitlagers wird durch diese Ausbildung mit dem Kühlmittelkreislauf innerhalb des Läufers gekoppelt, wobei der Läufer gekühlt und das Gleitlager gezielt geschmiert wird.Additionally is in an advantageous embodiment, at least one, the centric Bore in the runner with the sliding surface connecting the plain bearing and the condensate from the central bore in the plain bearing feeding Sliding bearing hole provided. The lubrication of the plain bearing is through this training with the coolant circuit within the runner coupled, the runner chilled and the plain bearing is lubricated targeted.
Zusätzlich dazu ist eine thermische Entkoppelung mindestens zwischen dem Stator und dem Dampfgehäuse des Turbinenabschnittes in Form mindestens eines radial von einem Kühlmittel durchströmten, im Statorgehäuse vorgesehenen Hohlraumes zweckmäßig. Diese Ausgestaltung dient der Kühlung des Stators, insbesondere der nahe dem Dampfraum des Turbinenabschnittes gelegenen Statorabschnitte und einer Verhinderung einer thermischen Überlastung des Stators und damit des Generatorabschnittes.Additionally is a thermal decoupling at least between the stator and the steam housing the turbine section in the form of at least one radially of a coolant perfused, in the stator housing provided cavity expedient. These Design serves for cooling the stator, in particular the near the steam space of the turbine section located stator sections and prevention of thermal overload of the stator and thus of the generator section.
Das den Hohlraum durchströmende Kühlmittel kann ebenfalls das Kondensat des ORC-Arbeitsmittels sein. In diesem Fall wird das Arbeitsmittel in dem Arbeitsmittelkreislauf zum Antreiben der Turbine und in dem Kühl- und Schmiermittelkreislauf ungetrieben werden.The flowing through the cavity coolant may also be the condensate of the ORC working fluid. In this Case becomes the working fluid in the working fluid circuit for driving the turbine and in the cooling and lubricating circuit are driven.
Der erfindungsgemäße ORC-Turbogenerator soll nachfolgend anhand eines Ausführungsbeispiels in Verbindung mit einer Figur näher erläutert werden. Es werden für gleiche bzw. gleich wirkende Teile die selben Bezugszeichen verwendet.Of the ORC turbo-generator according to the invention will be described below using an embodiment in conjunction closer with a figure be explained. It will be for the same or equivalent parts use the same reference numerals.
Für eine verständlichere Darstellung wird der Turbogenerator bei der folgenden Erläuterung in einen Generatorabschnitt A und einen Turbinenabschnitt B unterteilt. Der gesamte Turbogenerator weist jedoch einen kompakten und integrierten Aufbau auf, wobei die Abschnitte A und B zusammen eine in sich geschlossene Vorrichtung bilden.For a more understandable Representation will be the turbo-generator in the following explanation divided into a generator section A and a turbine section B. However, the entire turbogenerator has a compact and integrated Structure on, wherein the sections A and B together a self-contained Form device.
Der
Turbinenabschnitt besteht aus einem Turbinengehäuse
Bei
dem hier gezeigten Beispiel wird das Turbinenlaufrad tangential
angetrieben, während
das Arbeitsmedium den Turbinenabschnitt in axialer Richtung verläßt. Die
Zuführung
des Arbeitsmediums erfolgt über
eine Zudampföffnung
Der
Generatorabschnitt A schließt
sich über ein
Lagerschild
Die
Generatorwelle
Das
Kondensat wird nach dem Durchlaufen des Gleitlagers
In
dem hier dargestellten Ausführungsbeispiel
ist der Generatorabschnitt als ein permanent erregter Synchrongenerator
ausgebildet. Der Läufer des
Generators besteht dabei aus einer Reihe von auf die Welle
Das
Ständergehäuse
Die
zentrische Bohrung
Der
Generator weist weiterhin die üblichen elektrischen
Kabelanschlüsse
auf. In dem gezeigten Beispiel sind diese aus der Statorwicklung über eine Kabelsabschottung
Es ist klar, dass im Rahmen fachmännischen Handelns an dem gezeigten Ausführungsbeispiel eine Reihe von Änderungen erfolgen können, ohne den erfindungsgemäßen Grundgedanken zu verlassen. Weitere Ausführungsformen ergeben sich aus den Unteransprüchen.It It is clear that in the context of expert action in the embodiment shown a Set of changes can be done without the inventive idea to leave. Further embodiments emerge from the dependent claims.
- AA
- Generatorabschnittgenerator section
- BB
- Turbinenabschnittturbine section
- 11
- Turbinengehäuseturbine housing
- 22
- LaufradunterteilWheel base
- 33
- Laufradschaufelnimpeller blades
- 44
- LaufraddeckbandImpeller shroud
- 55
- DüsengrundkörperNozzle body
- 66
- Düsenöffnungnozzle opening
- 77
- DüsenabstandshalterDie spacer
- 88th
- Befestigungsbolzenmounting bolts
- 99
- ZudampföffnungZudampföffnung
- 1010
- ZudampfkanalZudampfkanal
- 1111
- AbdampfdiffusorAbdampfdiffusor
- 1212
- Lagerschildend shield
- 1313
- DruckausgleichsbohrungPressure compensating bore
- 1414
- Gleitlagerbearings
- 14b14b
- zweites Gleitlagersecond bearings
- 1515
- Gleitlagerbohrungplain bearing bore
- 15b15b
- zweite Gleitlagerbohrungsecond plain bearing bore
- 1616
- zentrische Bohrungcentric drilling
- 1717
- Generatorwellegenerator shaft
- 1818
- Permanentmagnetpermanent magnet
- 1919
- Ständerwicklungstator winding
- 2020
- Vergussgrouting
- 2121
- StändergehäuseThe stator frame
- 2222
- Läuferraumrunners room
- 2323
- Hohlraumcavity
- 2424
- StatorkühlungStator
- 2525
- KühlmittelvorlaufCoolant supply
- 2626
- KühlmittelrücklaufCoolant return
- 2727
- Kühlrohrcooling pipe
- 2828
- Rücklaufreturns
- 2929
- KühlmittelablaufCoolant flow
- 3030
- TurbineabdampföffnungTurbineabdampföffnung
- 3131
- Kabelabschottungcable insulation
- 3232
- Klemmkastenterminal box
Claims (7)
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102006004836A DE102006004836A1 (en) | 2005-11-17 | 2006-02-02 | Organic rankine cycle-turbo-generator, has generator section with stator housing that includes rotor chamber, which opens in direction of exhaust chamber of turbine section, where generator is provided between generator and turbine sections |
EP15189987.9A EP3000994B1 (en) | 2006-02-02 | 2007-02-02 | Organic rankine cycle (orc) - turbogenerator |
DE202007018540U DE202007018540U1 (en) | 2006-02-02 | 2007-02-02 | Organic Rankine Cycle (ORC) - Turbogenerator |
EP07726279.8A EP1984602B1 (en) | 2006-02-02 | 2007-02-02 | Organic rankine cycle (orc) turbogenerator |
PCT/EP2007/051002 WO2007088194A2 (en) | 2006-02-02 | 2007-02-02 | Organic rankine cycle (orc) turbogenerator |
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE202005018010.6 | 2005-11-17 | ||
DE202005018010 | 2005-11-17 | ||
DE102006004836A DE102006004836A1 (en) | 2005-11-17 | 2006-02-02 | Organic rankine cycle-turbo-generator, has generator section with stator housing that includes rotor chamber, which opens in direction of exhaust chamber of turbine section, where generator is provided between generator and turbine sections |
Publications (1)
Publication Number | Publication Date |
---|---|
DE102006004836A1 true DE102006004836A1 (en) | 2007-05-24 |
Family
ID=37989619
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE102006004836A Withdrawn DE102006004836A1 (en) | 2005-11-17 | 2006-02-02 | Organic rankine cycle-turbo-generator, has generator section with stator housing that includes rotor chamber, which opens in direction of exhaust chamber of turbine section, where generator is provided between generator and turbine sections |
Country Status (1)
Country | Link |
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DE (1) | DE102006004836A1 (en) |
Cited By (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102007027349A1 (en) * | 2007-06-14 | 2008-12-24 | Conpower Energieanlagen Gmbh & Co Kg. | Device and method for generating electricity from heat |
EP2110572A1 (en) * | 2008-04-16 | 2009-10-21 | Siemens Aktiengesellschaft | Cooling of the rotor lamination of a magnetic bearing |
US7638892B2 (en) * | 2007-04-16 | 2009-12-29 | Calnetix, Inc. | Generating energy from fluid expansion |
US8102088B2 (en) | 2008-01-25 | 2012-01-24 | Calnetix Technologies, L.L.C. | Generating electromagnetic forces with flux feedback control |
US8169118B2 (en) | 2008-10-09 | 2012-05-01 | Calnetix Technologies, L.L.C. | High-aspect-ratio homopolar magnetic actuator |
US8183854B2 (en) | 2008-11-07 | 2012-05-22 | Calnetix Technologies, L.L.C. | Measuring linear velocity |
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US9683601B2 (en) | 2013-03-14 | 2017-06-20 | Calnetix Technologies, Llc | Generating radial electromagnetic forces |
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