WO2011024375A1 - 排熱回収タービンシステム - Google Patents
排熱回収タービンシステム Download PDFInfo
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- WO2011024375A1 WO2011024375A1 PCT/JP2010/004576 JP2010004576W WO2011024375A1 WO 2011024375 A1 WO2011024375 A1 WO 2011024375A1 JP 2010004576 W JP2010004576 W JP 2010004576W WO 2011024375 A1 WO2011024375 A1 WO 2011024375A1
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- medium
- working medium
- turbine
- exhaust heat
- hfe
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01K—STEAM ENGINE PLANTS; STEAM ACCUMULATORS; ENGINE PLANTS NOT OTHERWISE PROVIDED FOR; ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES
- F01K25/00—Plants or engines characterised by use of special working fluids, not otherwise provided for; Plants operating in closed cycles and not otherwise provided for
- F01K25/08—Plants or engines characterised by use of special working fluids, not otherwise provided for; Plants operating in closed cycles and not otherwise provided for using special vapours
- F01K25/10—Plants or engines characterised by use of special working fluids, not otherwise provided for; Plants operating in closed cycles and not otherwise provided for using special vapours the vapours being cold, e.g. ammonia, carbon dioxide, ether
-
- 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
Definitions
- the present invention relates to an exhaust heat recovery turbine system that operates with a working medium whose main medium is an alternative chlorofluorocarbon having excellent environmental performance and handling.
- an exhaust heat recovery turbine system that uses exhaust heat such as hot waste water of less than 100 ° C. generated in a manufacturing process such as steelworks or ceramics as a heat source uses a low boiling point medium other than water as a working medium. It is attracting attention as a means of reducing greenhouse gases in conjunction with energy conservation.
- chlorofluorocarbon (CFC), hydrochlorofluorocarbon (HCFC), and hydrofluorocarbon (HFC) which have a boiling point lower than those of natural media such as ammonia, hydrocarbons, and water, operate. It is used as a medium (see, for example, Patent Document 1).
- chlorofluorocarbon (CFC) and hydrochlorofluorocarbon (HCFC), which are synthetic media, are difficult to use from an environmental point of view because they destroy the ozone layer and have a large global warming potential (GWP).
- Hydrofluorocarbon (HFC) has an ozone depletion potential (ODP) of zero and does not destroy the ozone layer, but has a slightly higher global warming potential. Therefore, in addition to the ozone depletion potential (ODP) being zero, there is a demand for a medium that has a smaller global warming potential and is more environmentally friendly.
- HFE hydrofluoroether
- the present invention has been made based on the above research, and an object of the present invention is to provide an exhaust heat recovery turbine system that operates with a working medium containing an alternative chlorofluorocarbon as a main medium that is excellent in environmental friendliness and is easy to handle.
- an exhaust heat recovery turbine system vaporizes the working medium by heat exchange between a turbine driven by the working medium and exhaust heat from an external heat source, and supplies the turbine to the turbine.
- An evaporator to be supplied and a condenser for liquefying the working medium that has passed through the turbine are included, and the working medium includes, as a main medium, a compound selected from a group of hydrofluoroether (HFE) and fluorinated alcohol.
- HFE hydrofluoroether
- the compound selected from the group of HFE and 3FE since the compound selected from the group of HFE and 3FE has a generally low boiling point at normal pressure, the working medium containing this as a main medium is exchanged with the exhaust heat from the heat source in the evaporator. It can be easily vaporized.
- these compounds since these compounds have a zero ozone depletion coefficient and a small global warming coefficient, they have a low environmental burden, are excellent in environmental properties, and have low toxicity, so that they are easy to handle.
- the main medium is preferably HFE having a boiling point at normal pressure (hereinafter, simply referred to as “boiling point” means a boiling point at normal pressure) of ⁇ 24 to 60 ° C.
- boiling point means a boiling point at normal pressure
- the main medium can be easily vaporized only with a normal exhaust heat level recovered from the heat source.
- the boiling point of HFE as the main medium at normal pressure exceeds 30 ° C.
- the system can be simplified because it can be easily liquefied with water at room temperature (about 15 to 30 ° C.) in the condenser.
- the main medium is preferably HFE having 2 to 4 carbon atoms.
- HFE hydrogen fluoride
- the carbon number of HFE is 2 to 4
- the boiling point at normal pressure is lower than that of water. Therefore, when the exhaust heat from the heat source is warm water, the HFE is easily vaporized by heat exchange with the warm water. be able to.
- HFE include C 3 F 7 OCH 3 (HFE 7000), C 4 F 9 OCH 3 (HFE 7100), C 4 F 9 OC 2 H 5 (HFE 7200) and C 6 F 13 OCH 3 (HFE 7300).
- the HFE may be CHF 2 —CF 2 —O—CH 2 —CF 3 (HFE-S7).
- the working medium is preferably a mixture of the main medium and a lubricating oil compatible with the main medium, for example, fluorine oil.
- a lubricating oil compatible with the main medium for example, fluorine oil.
- the bearing can be lubricated well.
- a lubrication system for supplying lubricating oil to the bearing of the turbine, and a seal portion that seals between the bearing and the turbine on the outer periphery of the rotating shaft of the turbine, and the lubricating system supplies the lubricating oil to the turbine
- the turbine bearing is of a grease lubrication type in which grease is enclosed.
- auxiliary equipment such as an injection pump becomes unnecessary, and maintenance is unnecessary as long as the grease life is long.
- the working medium containing this as the main medium is heated with the exhaust heat from the heat source in the evaporator. It is easily vaporized by exchange and is easily liquefied by a condenser after passing through the turbine. Moreover, since these compounds have a zero ozone depletion coefficient and a small global warming coefficient, they have a low environmental impact, are excellent in environmental properties, and have low toxicity.
- FIG. 1 is a schematic configuration diagram showing an exhaust heat recovery turbine system according to a first embodiment of the present invention.
- FIG. 2 is a characteristic comparison table between the main medium and other medium used in the present invention.
- FIG. 3 is a schematic configuration diagram showing an exhaust heat recovery turbine system according to the second embodiment of the present invention.
- FIG. 4 is a longitudinal sectional view showing details of the injection unit.
- FIG. 5 is a schematic configuration diagram illustrating an exhaust heat recovery turbine system according to a third embodiment of the present invention.
- FIG. 6 is a longitudinal sectional view showing details of the bearing of FIG.
- FIG. 1 shows a schematic configuration of an exhaust heat recovery turbine system according to a first embodiment of the present invention.
- the exhaust heat recovery turbine system shown in FIG. 1 includes a turbine power generation unit U including a generator 10 and a turbine 13 that drives the generator 10, and a falling liquid is supplied to a medium passage 30 that circulates a working medium M that rotates the turbine 13.
- a membrane evaporator 16, a condenser 17 and a medium feed pump 18 are provided.
- the generator 10 includes a generator rotor 11 and a generator stator 12, turbines 13 and 13 are arranged at both ends thereof, and the generator rotor 11 and the turbines 13 and 13 are connected by a single rotating shaft 21.
- the rotary shaft 21 is rotatably supported by two bearings 19, 19 disposed between the generator 10 and the two turbines 13, and an oil tank 25 is provided below each of the bearings 19. Yes.
- the two turbines 13 and 13 are arranged in opposite directions to form a so-called mirror image type, whereby the axial thrust acting on both turbines 13 and 13 is canceled out, and the thrust bearing is omitted or simplified. . Therefore, each bearing 19 bears mainly a radial load of the rotating shaft 21.
- the heat source 15 is, for example, exhaust heat of hot water or the like that is generated in a large amount in a manufacturing process such as an ironworks or a ceramic industry.
- the hot water led out from the heat source 15 is introduced into the heat transfer pipe 16a in the evaporator 16 through the heating fluid supply passage 15a, and then returned to the heat source 15 side from the heat transfer pipe 16a through the heating fluid recovery passage 15b. .
- the evaporator 16 evaporates the working medium M by heat exchange with the hot water passing through the heat transfer pipe 16a, that is, heat exchange with the exhaust heat of the heat source 15, and supplies the working medium M in the vapor phase to the gas-phase medium feed.
- the turbine power generation unit U is supplied via the path 30a.
- the evaporator 16 is provided with a circulation pump 27 in a circulation passage 29 disposed so as to communicate between the lower part and the upper part of the evaporator 16, and the liquid phase taken out from the lower part of the evaporator 16 by the circulation pump 27.
- the working medium M is sprayed into the evaporator 16 in a shower form from the outlet of the injection pipe 26 disposed in the evaporator 16 and sprayed onto the heat transfer pipe 16a to promote heat exchange.
- the working medium M after rotating the turbine 13 of the turbine power generation unit U is sent to the condenser 17 via the vapor phase medium recovery path 30b.
- the condenser 17 has a known structure in which a cooling medium C pipe is passed through, and liquefies the gas phase working medium M by cooling it with the cooling medium C.
- a medium passage 30 that is a circulation path is formed by the gas phase medium supply path 30a, the gas phase medium recovery path 30b, and the liquid phase medium supply path 30c.
- An oil tank 25 is provided below each bearing 19.
- a supply passage 20 branched from the circulation passage 29 is formed on the outlet side of the circulation pump 27, and a part of the liquid-phase working medium M taken out from the lower portion of the evaporator 16 by the circulation pump 27 from the supply passage 20. Is supplied to the oil tank 25 below each bearing 19. Therefore, the high-pressure working medium M is supplied from the oil tank 25 to the bearing 19 and lubrication is performed smoothly.
- the supply passage 20 is provided with a pressure reducer 28 such as a throttle such as an orifice or a pressure reducing valve, and by evaporating a part of the liquid-phase working medium M by the pressure reduction, the lubricating oil concentration is improved. The temperature of the working medium M is lowered by the latent heat of evaporation.
- a return passage for returning the liquid-phase working medium M discharged from the bearing 19 to the condenser 17. 23 is connected.
- the liquid-phase working medium M returned to the condenser 17 from the return passage 23 merges in the condenser 17 with the working medium M that has passed through the gas phase medium recovery path 30b.
- HFE hydrofluoroether
- H in the general formula C n H 2n + 1 —O—C m H 2m + 1 is partially substituted with F
- fluorinated alcohol fluorinated alcohol
- HFE having 2 to 4 carbon C is preferable.
- the carbon number of HFE is 2 to 4, the boiling point at normal pressure is lower than that of water. Therefore, even if the exhaust heat from the heat source 15 is warm water having a temperature of 100 ° C. or less, the HFE is exchanged by heat exchange with the warm water. Can be easily vaporized.
- the main medium preferably has a boiling point of ⁇ 24 to 60 ° C., more preferably more than 30 ° C. and 60 ° C. or less. If the boiling point is 60 ° C. or lower, the main medium can be vaporized using the relatively low-temperature exhaust heat recovered from the heat source 15. If it exceeds 30 ° C., it can be condensed with water at normal pressure (atmospheric pressure) and room temperature (about 15 to 30 ° C.) and can be easily liquefied, thereby simplifying the system.
- HFE satisfying the condition of the boiling point of ⁇ 24 to 60 ° C. examples include C 3 F 7 OCH 3 (HFE 7000) and CHF 2 —CF 2 —O—CH 2 —CF 3 .
- C 3 F 7 OCH 3 HFE7000
- Novec 7000 roofing point 34 ° C.
- CHF 2 —CF 2 —O—CH 2 —CF 3 Daikin Industries There are trade names HFE-S7 from Asahi Glass Co., Ltd.
- Such main media include C 4 F 9 OCH 3 (HFE 7100) with a boiling point of 61 ° C., C 4 F 9 OC 2 H 5 (HFE 7200) at 76 ° C. and C 6 F 13 OCH 3 (HFE 7300) at 98 ° C. .
- a fluorinated alcohol can also be used as the main medium.
- 3FE trifluorinated alcohol in which H other than OH in the general formula C n H 2n + 1- OH is partially substituted with F is preferable.
- 3FE has a boiling point of 74 ° C. at normal pressure and weak flammability, the ozone depletion coefficient ODP is zero and the global warming potential GWP is also small.
- the main medium is a medium that has an ozone depletion potential ODP of zero and a low global warming potential GWP, which has a low environmental load, is environmentally friendly, has no toxicity, and has good handleability. Since it is used, it can be easily vaporized by heat exchange with the exhaust heat in the evaporator 16, and can be easily liquefied by the condenser 17 after passing through the turbine 13.
- FIG. 2 illustrates CFC (chlorofluorocarbon), HCFC (hydrochlorofluorocarbon), HFC (hydrofluorocarbon), HFE, and 3FE (trifluorinated alcohol).
- HFE7000 has a boiling point of 60 ° C. or less, and is extremely excellent in that it is easily vaporized (marked with ⁇ ).
- HFO hydrofluoroolefin
- HFE hydrofluoroolefin
- HFO-1234yf chemical formula CF 3 CF ⁇ CH 2 .
- HFE used as a main medium is an excellent medium that has a small warming potential and does not destroy the ozone layer, but has no lubricity. Therefore, in this embodiment, lubricity is imparted to the working medium M by mixing lubricating oil made of fluorine oil into HFE.
- Examples of the lubricating oil to be mixed with the main medium include a fluorine oil represented by the following chemical formula having a polymer structure in which the terminal of the base oil or additive of the lubricating oil is partially or entirely blocked with fluorine. .
- the former is, for example, the product name Krytox manufactured by DuPont.
- This fluorine oil has good compatibility with the main medium such as HFE described above, and the main medium and the fluorine oil are not separated in a liquid phase state.
- Hot water derived from the heat source 15 as exhaust heat is introduced into the evaporator 16 from the heating fluid supply passage 15a, and the working medium M in the evaporator 16 exchanges heat with the introduced hot water, that is, from the heat source 15. It is vaporized by receiving the heat and becomes a high-pressure gas phase of, for example, about 4 atm.
- the lubricating oil is difficult to evaporate, it remains as a liquid-phase working medium M with a high lubricating oil concentration at the lower part of the evaporator 16.
- the working medium M in the gas phase is taken out from the upper part of the evaporator 16 and supplied to the pair of turbines 13 and 13 of the turbine power generation unit U through the gas phase medium feeding path 30a. To drive. Thereby, the generator 10 connected with the turbine 13 and the rotating shaft 21 is driven, and electric power generation is performed.
- the working medium M that has released the energy by the turbine 13 enters the condenser 17 through the gas phase medium recovery path 30b, and is cooled and condensed by heat exchange with the cooling medium C.
- the working medium M that has become a liquid phase passes through the liquid-phase medium feed path 30c, is pressurized by the medium feed pump 18, and returns to the evaporator 16.
- the liquid-phase working medium M having a high lubricating oil concentration left in the lower portion of the evaporator 16 is supplied to the oil tank 25 of the bearing 19 of the turbine power generation unit U through the supply passage 20.
- the working medium M is cooled by the decompressor 28 provided in the supply passage 20.
- the supply passage 20 in this embodiment may be provided with a cooler instead of or in addition to the decompressor 28.
- the liquid-phase working medium M supplied to the oil tank 25 from the outlet side of the circulation pump 27 of the circulation passage 29 is a working medium having a high lubricating oil concentration containing a large amount of lubricating oil.
- the bearing 19 When the turbine generator rotates, the bearing 19 Is always well lubricated by the liquid-phase working medium M having a high lubricating oil concentration. As described above, since the bearing 19 can be lubricated by the working medium M having a high lubricating oil concentration, it is not necessary to mix a large amount of lubricating oil with the working medium in order to improve lubricity. There is no hindrance to heat.
- the oil tank 25 It is sufficient for the oil tank 25 to have an amount of the working medium M necessary for lubricating the bearing 19, and the surplus is discharged from the oil tank 25 to the return passage 23 and returned to the condenser 17 from the return passage 23. Therefore, the working medium M is not discharged out of the system and does not affect the surrounding environment, and is circulated and used in the closed system. A part of the working medium M may be in a gas phase due to the temperature rise in the bearing 19. In this case, the working medium M in which the liquid phase and the gas phase are mixed enters the condenser 17 through the return passage 23. .
- the inlet of the condenser 17 is about normal pressure, the working medium M is smoothly recovered from the oil tank 25 having a slightly high pressure to the condenser 17.
- the circulation pump 27 is operated at a constant flow rate unlike the medium feed pump 18 in which the flow rate varies according to the liquid level in the evaporator 16.
- a liquid phase working medium M having a high lubricating oil concentration can be supplied to the bearing 19 in a stable amount from the branched supply passage 20.
- the downstream end of the return passage 23 may be connected to the medium recovery path 30 b instead of the inlet of the condenser 17.
- the decompressor 28 provided in the supply passage 20 evaporates part of the working medium M to increase the lubricating oil concentration of the working medium M, and in the working medium M due to a temperature drop due to latent heat of evaporation. Since the viscosity of the lubricating oil increases, good lubricating performance is maintained.
- the lubricating working medium M is used for driving the turbine, it is directly supplied from the supply passage 20 to the bearing 19 of the turbine 13, so that the bearing 19 is well lubricated. Is done.
- the generator 10 is driven by the turbine 13, but the present invention can also be applied to a system in which another load such as a pump of a plant is driven by the turbine 13.
- FIG. 3 shows an exhaust heat recovery turbine system according to a second embodiment of the present invention.
- the supply passage 20 for supplying the working medium M mixed with the lubricating oil L to the bearing 19 of the turbine 13 is provided.
- a lubricating system 40 that stores lubricating oil L in the bearing 19 of the turbine 13 is newly provided in place of the supply passage 20 using the working medium M1 that does not contain lubricating oil.
- the lubricating system 40 includes a lubricating oil reservoir 41 that stores the lubricating oil L, and a lubricating oil supply passage 42 that connects the lubricating oil reservoir 41 and the injection unit 33 that injects the lubricating oil L to the bearings 19 and 19. And an injection pump 43 that pressurizes the lubricating oil L and sends it to the injection unit 33.
- the lubricating oil L injected from the injection unit 33 to the bearings 19 and 19 is returned to the lubricating oil reservoir 41 through the return passage 35 and is used repeatedly.
- FIG. 4 shows details of the injection unit 33.
- an inner ring spacer 36 fixed to the rotary shaft 21 and an outer ring spacer 37 fixed to the housing H are disposed between the pair of left and right bearings 19, 19.
- An injection nozzle 38 is provided on the seat 37.
- the injection nozzle 38 has a central inlet 38a and an injection passage 38b branched from the inlet 38a and directed to the left and right bearings 19, 19.
- the tip of the injection passage 38b is connected to the inner ring 19a and the outer ring of the bearing 19.
- the lubricating oil L is directed to the bearing space 19c between the rolling element 19d and the rolling element 19d through the bearing space 19c.
- the housing H is formed with a downstream portion of the lubricating oil supply passage 42 for supplying the lubricating oil L to the injection portion 33 and an upstream portion of the return passage 35 for the lubricating oil L.
- One or two injection nozzles 38 are provided for each of the bearings 19 and 19.
- seal portion 39 that seals between the parts 19 and 13, and similarly on the outer periphery of the rotor 11 of the generator 10 (FIG. 3).
- a seal portion 39 is also provided between the bearing 19 and the generator 10.
- the seal portion 39 is configured by a seal ring that is fixed to the housing H and forms a labyrinth seal with the outer peripheral surface of the rotary shaft 14.
- the lubricating oil L from the lubricating oil reservoir 41 is injected as a high-speed jet from the injection unit 33 through the lubricating oil supply passage 42 and lubricates the bearings 19 and 19. Is done. Therefore, the bearing 19 can be effectively lubricated and cooled even when high-speed rotation is required and the heat generation of the bearing is large. Further, since the seal portions 39 are provided on both sides of the bearing 19, there is no possibility that the lubricating oil L used for lubricating the bearing 19 leaks to the turbine 13 side and the rotor 11 side, and the lubricating oil L is recovered with a high yield. Can do. Further, it can be avoided that the lubricating oil L is mixed into the working medium M of the turbine 13 to lower the thermal efficiency of the turbine 13.
- FIG. 5 shows an exhaust heat recovery turbine system according to a third embodiment of the present invention.
- a grease lubricated bearing 19B in which grease G is enclosed is used.
- FIG. 6 shows details of the bearing 19B.
- a rolling element 19Bd is rotatably held by a cage 19Bc between a bearing outer ring 19Ba and a bearing inner ring 19Bb, and a pair of seals are provided outside the cage 19Bc in the axial direction.
- Plates 19Be and 19Be are provided.
- the upper end of the sealing plate 19Be is engaged with a groove provided on the inner peripheral surface of the bearing outer ring 19Ba, and the lower end of the sealing plate 19Be is such that the rotation of the bearing inner ring 19Bb rotating integrally with the rotary shaft 21 is not hindered.
- Two bearings 19B may be arranged similarly to the second embodiment shown in FIG. Similarly to the second embodiment, a seal portion is provided for sealing between the bearing 19B of FIG. 5 and the turbine 13 and the generator 10 so that the grease G leaks to the turbine 13 side or the generator 10 side. It may not be possible.
- the supply passage 20 used in the first embodiment and the auxiliary machinery such as the lubricating oil supply passage 42 and the injection pump 43 used in the second embodiment are not required. Simplification is possible, and maintenance is unnecessary as long as the grease life is long.
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Abstract
Description
G グリース
M 作動媒体
L 潤滑油
U タービン発電ユニット
10 発電機
13 タービン
15 熱源
16 蒸発器
16a 伝熱管
17 凝縮器
18 媒体送給ポンプ
19 軸受
19B グリース封入型軸受
20 供給通路
26 噴射管
27 循環ポンプ
28 減圧器
29 循環通路
30 媒体通路
30a 気相媒体送給路
30b 気相媒体回収路
30c 液相媒体送給路
35 戻し通路
39 シール部
40 潤滑系統
41 潤滑油溜まり
42 潤滑油供給通路
43 噴射ポンプ
Claims (11)
- 作動媒体により駆動されるタービンと、
外部の熱源からの排熱との熱交換により前記作動媒体を蒸気化して前記タービンに供給する蒸発器と、前記タービンを通過した作動媒体を液化する凝縮器とを備え、
前記作動媒体が、ハイドロフルオロエーテル(HFE)およびフッ化アルコールの一群から選択された化合物を主媒体として含む排熱回収タービンシステム。 - 請求項1において、前記主媒体は、沸点が-24~60℃のHFEである排熱回収タービンシステム。
- 請求項2において、前記主媒体であるHFEの常圧における沸点が30℃を超えている排熱回収タービンシステム。
- 請求項1から3のいずれか一項において、前記主媒体は、炭素数が2~4のHFEである排熱回収タービンシステム。
- 請求項1において、HFEは、C3F7OCH3,C4F9OCH3,C4F9OC2H5,およびC6F13OCH3よりなる群から選択された化合物である排熱回収タービンシステム。
- 請求項4において、HFEは、CHF2-CF2-O-CH2-CF3である排熱回収タービンシステム。
- 請求項1から6のいずれか一項において、前記作動媒体は、前記主媒体に、この主媒体と相溶性のある潤滑油が混合されたものである排熱回収タービンシステム。
- 請求項7において、前記潤滑油はフッ素油である排熱回収タービンシステム。
- 請求項7において、さらに、前記作動媒体を前記タービンの軸受に供給する供給通路を備えている排熱回収タービンシステム。
- 請求項1から6のいずれか一項において、前記タービンの軸受に潤滑油を供給する潤滑系統と、前記タービンの回転軸の外周における前記軸受とタービンとの間をシールするシール部とを備え、前記潤滑系統が潤滑油を前記軸受に噴射する噴射部を有する排熱回収タービンシステム。
- 請求項1から6のいずれか一項において、前記タービンの軸受が、グリースを封入したグリース潤滑型である排熱回収タービンシステム。
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KR1020127003197A KR101317038B1 (ko) | 2009-08-24 | 2010-07-14 | 배열회수 터빈 시스템 |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
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ITCO20130070A1 (it) * | 2013-12-18 | 2015-06-19 | Nuovo Pignone Srl | Apparato per realizzare una tenuta di fluido in un ambiente interno di una turbomacchina |
JP2016037852A (ja) * | 2014-08-05 | 2016-03-22 | トヨタ自動車株式会社 | 内燃機関の冷却装置 |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS63144737A (ja) * | 1986-12-08 | 1988-06-16 | Fuji Electric Co Ltd | 配管内蔵形発電装置 |
JP2005264863A (ja) * | 2004-03-19 | 2005-09-29 | Ebara Corp | 発電装置 |
JP2007503546A (ja) * | 2003-08-27 | 2007-02-22 | ティーティーエル ダイナミクス リミッテッド | エネルギ回収システム |
JP2008542629A (ja) * | 2005-06-10 | 2008-11-27 | シティ ユニヴァーシティ | ポンプ |
-
2010
- 2010-07-14 CN CN2010800352180A patent/CN102472122A/zh active Pending
- 2010-07-14 KR KR1020127003197A patent/KR101317038B1/ko active IP Right Grant
- 2010-07-14 WO PCT/JP2010/004576 patent/WO2011024375A1/ja active Application Filing
- 2010-07-29 TW TW099125250A patent/TWI443255B/zh not_active IP Right Cessation
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS63144737A (ja) * | 1986-12-08 | 1988-06-16 | Fuji Electric Co Ltd | 配管内蔵形発電装置 |
JP2007503546A (ja) * | 2003-08-27 | 2007-02-22 | ティーティーエル ダイナミクス リミッテッド | エネルギ回収システム |
JP2005264863A (ja) * | 2004-03-19 | 2005-09-29 | Ebara Corp | 発電装置 |
JP2008542629A (ja) * | 2005-06-10 | 2008-11-27 | シティ ユニヴァーシティ | ポンプ |
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ITCO20130070A1 (it) * | 2013-12-18 | 2015-06-19 | Nuovo Pignone Srl | Apparato per realizzare una tenuta di fluido in un ambiente interno di una turbomacchina |
WO2015091434A1 (en) * | 2013-12-18 | 2015-06-25 | Nuovo Pignone Srl | Apparatus for sealing an internal environment of a turbomachine |
US11220926B2 (en) | 2013-12-18 | 2022-01-11 | Nuovo Pignone Srl | Apparatus for sealing an internal environment of a turbomachine |
JP2016037852A (ja) * | 2014-08-05 | 2016-03-22 | トヨタ自動車株式会社 | 内燃機関の冷却装置 |
US10294849B2 (en) | 2014-08-05 | 2019-05-21 | Toyota Jidosha Kabushiki Kaisha | Cooling device having a refrigerant supply part of a condenser arranged higher than a shaft part of a turbine in a gravity direction |
Also Published As
Publication number | Publication date |
---|---|
KR101317038B1 (ko) | 2013-10-11 |
TWI443255B (zh) | 2014-07-01 |
CN102472122A (zh) | 2012-05-23 |
KR20120042934A (ko) | 2012-05-03 |
TW201111617A (en) | 2011-04-01 |
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