BR112017021062A2 - turbina multiestágio preferencialmente para usinas de ciclo rankine orgânico orc - Google Patents
turbina multiestágio preferencialmente para usinas de ciclo rankine orgânico orcInfo
- Publication number
- BR112017021062A2 BR112017021062A2 BR112017021062A BR112017021062A BR112017021062A2 BR 112017021062 A2 BR112017021062 A2 BR 112017021062A2 BR 112017021062 A BR112017021062 A BR 112017021062A BR 112017021062 A BR112017021062 A BR 112017021062A BR 112017021062 A2 BR112017021062 A2 BR 112017021062A2
- Authority
- BR
- Brazil
- Prior art keywords
- turbine
- bearings
- rankine cycle
- shaft
- organic rankine
- Prior art date
Links
Classifications
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/06—Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
- F01D5/066—Connecting means for joining rotor-discs or rotor-elements together, e.g. by a central bolt, by clamps
-
- 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
- F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
-
- 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
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
- F01D25/243—Flange connections; Bolting arrangements
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/04—Blade-carrying members, e.g. rotors for radial-flow machines or engines
- F01D5/043—Blade-carrying members, e.g. rotors for radial-flow machines or engines of the axial inlet- radial outlet, or vice versa, type
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/06—Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
-
- 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
- F01K23/00—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids
- F01K23/02—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled
- F01K23/06—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled combustion heat from one cycle heating the fluid in another cycle
- F01K23/10—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled combustion heat from one cycle heating the fluid in another cycle with exhaust fluid of one cycle heating the fluid in another cycle
-
- 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
-
- 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
- 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
- F05D2210/00—Working fluids
- F05D2210/40—Flow geometry or direction
- F05D2210/43—Radial inlet and axial outlet
-
- 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
- F05D2240/20—Rotors
-
- 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
- F05D2250/00—Geometry
- F05D2250/50—Inlet or outlet
- F05D2250/51—Inlet
Abstract
trata-se de uma turbina de um ciclo de rankine orgânico orc. a turbina compreende um eixo sustentado por pelo menos dois mancais e uma pluralidade de estágios axiais de expansão, definidos por matrizes de pás de estator alternadas com matrizes ou pás de rotor. as pás de rotor são mantidas por discos de sustentação correspondentes. um disco de sustentação principal é acoplado diretamente ao eixo em uma posição externa em relação aos mancais, e os discos de sustentação remanescentes são travados ao disco de sustentação principal, e um ao outro em sucessão, mas não diretamente ao eixo. a solução proposta permite que uma configuração em balanço da turbina seja obtida ao mesmo tempo em que ainda tem uma pluralidade de estágios, até mais do que três, caso desejado. a turbina permite expandir o fluido de trabalho com alto salto de entalpia similar àquele obtenível pelas turbinas axiais multiestágio convencionais, que não são em balanço, ou por duas turbinas axiais acopladas, em que as outras condições são inalteradas. alguns dos discos de sustentação remanescentes são travados ao disco de sustentação principal e se estendem em balanço a partir do mesmo lado dos mancais que sustentam o eixo, para que o centro de gravidade da parte de rotor da turbina seja mais deslocado em direção aos mancais.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT102015902342533 | 2015-04-03 | ||
ITBS20150057 | 2015-04-03 | ||
PCT/IB2016/051581 WO2016157020A2 (en) | 2015-04-03 | 2016-03-21 | Multistage turbine preferably for organic rankine cycle orc plants |
Publications (2)
Publication Number | Publication Date |
---|---|
BR112017021062A2 true BR112017021062A2 (pt) | 2018-07-03 |
BR112017021062B1 BR112017021062B1 (pt) | 2023-02-23 |
Family
ID=53385724
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112017021062-2A BR112017021062B1 (pt) | 2015-04-03 | 2016-03-21 | Turbina multiestágio preferencialmente para usinas de ciclo rankine orgânico orc |
Country Status (11)
Country | Link |
---|---|
US (1) | US10526892B2 (pt) |
EP (1) | EP3277929B1 (pt) |
JP (1) | JP6657250B2 (pt) |
CN (1) | CN107429567B (pt) |
BR (1) | BR112017021062B1 (pt) |
CA (1) | CA2975968C (pt) |
ES (1) | ES2959679T3 (pt) |
HR (1) | HRP20231218T1 (pt) |
PL (1) | PL3277929T3 (pt) |
RU (1) | RU2716932C2 (pt) |
WO (1) | WO2016157020A2 (pt) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
IT201800002027A1 (it) * | 2018-01-26 | 2019-07-26 | Turboden Spa | Dispositivo di tenuta di fluido per macchine rotanti |
JP7026520B2 (ja) * | 2018-01-30 | 2022-02-28 | 三菱重工コンプレッサ株式会社 | タービン用の弁装置、タービン、およびそれらの製造方法 |
IT201800021292A1 (it) | 2018-12-28 | 2020-06-28 | Turboden Spa | Turbina assiale a due livelli di alimentazione |
JP7216567B2 (ja) * | 2019-02-25 | 2023-02-01 | 三菱重工コンプレッサ株式会社 | 弁装置及び蒸気タービン |
US11008979B2 (en) * | 2019-05-29 | 2021-05-18 | Raytheon Technologies Corporation | Passive centrifugal bleed valve system for a gas turbine engine |
RU195196U1 (ru) * | 2019-11-21 | 2020-01-17 | Общество с ограниченной ответственностью "Проблемная лаборатория "Турбомашины" | Роторный узел газовой турбины |
RU202366U1 (ru) * | 2020-09-08 | 2021-02-15 | Александр Александрович Стуров | Газотурбинный двигатель Стурова с вращением соосных роторов в противоположных направлениях |
CN113969806B (zh) * | 2021-10-29 | 2024-02-02 | 重庆江增船舶重工有限公司 | 一种大功率多级轴流涡轮膨胀机 |
CN114183210A (zh) * | 2021-12-02 | 2022-03-15 | 中国船舶重工集团公司第七0三研究所 | 一种紧凑汽缸结构 |
CN114876580B (zh) * | 2022-07-12 | 2022-09-27 | 陕西联信材料科技有限公司 | 一种飞机制造用航空发动机涡轮叶片组件及其制备方法 |
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GB310037A (en) * | 1928-04-21 | 1930-02-06 | Ljungstroms Angturbin Ab | Turbine disk for radial flow steam turbines with an axial blade system |
US1896809A (en) * | 1930-03-03 | 1933-02-07 | B F Sturtevant Co | Multistage turbine |
US2115031A (en) * | 1932-03-22 | 1938-04-26 | Meininghaus Ulrich | Disk construction for radial flow machines |
US2020793A (en) * | 1932-03-30 | 1935-11-12 | Meininghaus Ulrich | Turbine |
US2102637A (en) * | 1932-06-01 | 1937-12-21 | Mcininghaus Ulrich | Arrangement of radially traversed blades in rotary machines |
US2081150A (en) * | 1932-09-10 | 1937-05-25 | Meininghaus Ulrich | Disk construction for radial flow machines |
US2145886A (en) * | 1934-04-24 | 1939-02-07 | Meininghaus Ulrich | Steam turbine working with wet steam |
US2430183A (en) * | 1944-12-16 | 1947-11-04 | Moller Ragnar Olov Jacob | Double rotation elastic fluid turbine |
US2614799A (en) * | 1946-10-02 | 1952-10-21 | Rolls Royce | Multistage turbine disk construction for gas turbine engines |
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US2918252A (en) * | 1954-12-24 | 1959-12-22 | Rolls Royce | Turbine rotor disc structure |
NL246286A (pt) * | 1956-01-25 | |||
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US3226085A (en) * | 1962-10-01 | 1965-12-28 | Bachl Herbert | Rotary turbine |
CH491287A (de) * | 1968-05-20 | 1970-05-31 | Sulzer Ag | Zweiwellige Gasturbinenanlage |
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NL8303401A (nl) * | 1982-11-01 | 1984-06-01 | Gen Electric | Aandrijfturbine voor tegengesteld draaiende propellers. |
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EP2952692A4 (en) * | 2013-03-27 | 2016-03-02 | Mitsubishi Heavy Ind Compressor Corp | MULTISOUPAPES TYPE VAPOR VALVE AND STEAM TURBINE |
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-
2016
- 2016-03-21 US US15/562,378 patent/US10526892B2/en active Active
- 2016-03-21 JP JP2017549762A patent/JP6657250B2/ja active Active
- 2016-03-21 CA CA2975968A patent/CA2975968C/en active Active
- 2016-03-21 ES ES16722697T patent/ES2959679T3/es active Active
- 2016-03-21 CN CN201680016506.9A patent/CN107429567B/zh active Active
- 2016-03-21 HR HRP20231218TT patent/HRP20231218T1/hr unknown
- 2016-03-21 WO PCT/IB2016/051581 patent/WO2016157020A2/en active Application Filing
- 2016-03-21 BR BR112017021062-2A patent/BR112017021062B1/pt active IP Right Grant
- 2016-03-21 EP EP16722697.6A patent/EP3277929B1/en active Active
- 2016-03-21 RU RU2017131761A patent/RU2716932C2/ru active
- 2016-03-21 PL PL16722697.6T patent/PL3277929T3/pl unknown
Also Published As
Publication number | Publication date |
---|---|
US10526892B2 (en) | 2020-01-07 |
CN107429567B (zh) | 2021-03-23 |
EP3277929B1 (en) | 2023-08-02 |
JP6657250B2 (ja) | 2020-03-04 |
CA2975968A1 (en) | 2016-10-06 |
CA2975968C (en) | 2024-01-02 |
JP2018513299A (ja) | 2018-05-24 |
WO2016157020A3 (en) | 2016-11-24 |
RU2017131761A (ru) | 2019-05-07 |
RU2716932C2 (ru) | 2020-03-17 |
US20180283177A1 (en) | 2018-10-04 |
RU2017131761A3 (pt) | 2019-10-17 |
EP3277929A2 (en) | 2018-02-07 |
ES2959679T3 (es) | 2024-02-27 |
WO2016157020A2 (en) | 2016-10-06 |
CN107429567A (zh) | 2017-12-01 |
BR112017021062B1 (pt) | 2023-02-23 |
HRP20231218T1 (hr) | 2024-02-02 |
PL3277929T3 (pl) | 2024-04-08 |
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Legal Events
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B06U | Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette] | ||
B09A | Decision: intention to grant [chapter 9.1 patent gazette] | ||
B16A | Patent or certificate of addition of invention granted [chapter 16.1 patent gazette] |
Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 21/03/2016, OBSERVADAS AS CONDICOES LEGAIS |