TR201819956T4 - Radyal turbo maki̇ne. - Google Patents

Radyal turbo maki̇ne. Download PDF

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Publication number
TR201819956T4
TR201819956T4 TR2018/19956T TR201819956T TR201819956T4 TR 201819956 T4 TR201819956 T4 TR 201819956T4 TR 2018/19956 T TR2018/19956 T TR 2018/19956T TR 201819956 T TR201819956 T TR 201819956T TR 201819956 T4 TR201819956 T4 TR 201819956T4
Authority
TR
Turkey
Prior art keywords
rotor
annular segments
housing
segments
protruding
Prior art date
Application number
TR2018/19956T
Other languages
English (en)
Inventor
Spadacini Claudio
Rizzi Dario
Original Assignee
Exergy Spa
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Exergy Spa filed Critical Exergy Spa
Publication of TR201819956T4 publication Critical patent/TR201819956T4/tr

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
    • F01D5/04—Blade-carrying members, e.g. rotors for radial-flow machines or engines
    • F01D5/041—Blade-carrying members, e.g. rotors for radial-flow machines or engines of the Ljungström 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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/001—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between stator blade and rotor
    • 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
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/003—Arrangements for testing or measuring
    • 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
    • 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
    • F01D5/12—Blades
    • 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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/026—Scrolls for radial machines or engines
    • 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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/001—Testing thereof; Determination or simulation of flow characteristics; Stall or surge detection, e.g. condition monitoring
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/08—Sealings
    • F04D29/083—Sealings especially adapted for elastic fluid pumps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/284—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for compressors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/4206—Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/44—Fluid-guiding means, e.g. diffusers
    • F04D29/441—Fluid-guiding means, e.g. diffusers especially adapted for elastic fluid pumps
    • F04D29/444—Bladed diffusers
    • 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
    • F05D2260/00—Function
    • F05D2260/83—Testing, e.g. methods, components or tools therefor

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

Mevcut buluş, bir radyal turbo makine ile ilgili olup, şunları içermektedir: bir sabit mahfaza (6); mahfazada (6) kurulan ve bunun bir ön yüzünde (4, 4', 4&#8221#&) monte edilen rotor kanatlarına (3, 3', 3&#8221#&) sahip en az bir rotor disk (2, 2', 2&#8221#&); mahfazadan (6) çıkıntı yapan ve rotor diskin (2, 2', 2&#8221#&) yakınında sona erken birden çok eleman (25, 35), burada çıkıntı yapan elemanlar (25, 35), rotor diskin (2, 2', 2") bir arka yüzünde (9, 9', 9&#8221#&) işlevsel olarak aktif olan rotor diske (2, 2', 2&#8221#&) karşı işlev gösteren sızdırmazlık elemanları (34) veya rotor diskin (2) rotor kanatları (3) arasında radyal olarak yerleştirilen stator kanatları (13) içermektedir; çıkıntı yapan elemanları (25, 35) taşıyan ve mahfazada (6) kurulan en az bir destek plakası (17, 37). Destek plakası (17, 37), rotor diskten (2, 2', 2&#8221#&) radyal olarak karşıya uzanmaktadır ve rotor diskin (2) dönüş ekseni (X-X) ile eş merkezli birden çok birinci dairesel bölüm (29) ile ve birinci dairesel bölümler (29) arasında radyal olarak yerleştirilen birden çok ikinci dairesel bölüm (30) içermektedir. Birinci dairesel bölümlerin (29) en azından birkaçı, çıkıntı yapan elemanları (25, 35) taşımaktadır ve ikinci dairesel bölümler (30), destek plakası (17, 37), termal gradyanların eylemine tabi tutulduğunda birinci dairesel bölümler (29) arasında ilgili hareketlere imkân tanıyacak bir şekilde birinci dairesel bölümlere (29) göre radyal yönler boyunca daha fazla biçim değiştirebilmektedir.
TR2018/19956T 2014-03-21 2015-03-17 Radyal turbo maki̇ne. TR201819956T4 (tr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ITMI20140488 2014-03-21

Publications (1)

Publication Number Publication Date
TR201819956T4 true TR201819956T4 (tr) 2019-02-21

Family

ID=50981686

Family Applications (1)

Application Number Title Priority Date Filing Date
TR2018/19956T TR201819956T4 (tr) 2014-03-21 2015-03-17 Radyal turbo maki̇ne.

Country Status (9)

Country Link
US (2) US10876406B2 (tr)
EP (1) EP3119992B1 (tr)
JP (1) JP2017519156A (tr)
CN (1) CN106255805B (tr)
CA (1) CA2943409A1 (tr)
MX (1) MX2016012187A (tr)
RU (1) RU2016140620A (tr)
TR (1) TR201819956T4 (tr)
WO (1) WO2015140711A1 (tr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ITUA20162125A1 (it) * 2016-03-30 2017-09-30 Exergy Spa Turbomacchina radiale con compensazione della spinta assiale
ITUA20162126A1 (it) * 2016-03-30 2017-09-30 Exergy Spa Metodo per la costruzione di dischi palettati per turbomacchine radiali e disco palettato ottenuto tramite tale metodo
FR3085409B1 (fr) * 2018-08-29 2020-12-11 Safran Aircraft Engines Accouplement pour turbomachine de type curvic avec verrouillage
FR3093533B1 (fr) * 2019-03-06 2022-04-15 Safran Aircraft Engines dispositif d’amortissement pour rotor de turbomachine
WO2020216854A1 (en) * 2019-04-24 2020-10-29 Single Buoy Moorings Inc. Swivel stack for transfer of fluid across a rotary interface and method for manufacturing such a swivel stack.
FR3106153B1 (fr) * 2020-01-10 2022-01-28 Safran Aircraft Engines Dispositif pour le désengagement de turbine en survitesse de turbomachine

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB191024137A (en) * 1909-11-12 1911-03-16 Ljungstroms Angturbin Ab Improvements in Gas or Steam-turbines.
FR428778A (fr) 1910-03-26 1911-09-07 Ljungstroems Angturbin Ab Garniture en labyrinthe pour turbines à vapeur ou à gaz
GB191424137A (en) 1914-12-16 1915-01-21 Albion Motor Car Co Ltd Improvements in Mechanism for Operating Tipping Waggons and the like.
US1468694A (en) * 1921-09-19 1923-09-25 Bonom Alfred Flexible and insulating, supporting, and reenforcing rings for crown blades of turbins
US1925148A (en) * 1930-03-24 1933-09-05 Milo Ab High temperature turbine
US2081148A (en) * 1931-03-25 1937-05-25 Meininghaus Ulrich Disk construction for radial flow machines
US2020793A (en) * 1932-03-30 1935-11-12 Meininghaus Ulrich Turbine
GB396352A (en) * 1932-05-09 1933-08-03 Asea Ab Improvements in radial flow steam or gas turbines having axially displaced bladings
US2200288A (en) * 1937-02-02 1940-05-14 Meininghaus Ulrich Bladed disk for radial flow rotary machines
US2374671A (en) * 1941-06-24 1945-05-01 Dupont Emile Turbine
DE3235585C2 (de) * 1982-09-01 1985-11-14 Christian O. 7590 Achern Schön Hochleistungsgebläse oder -verdichter für aggressive und/oder heiße Medien
GB2221259A (en) * 1988-07-30 1990-01-31 John Kirby Turbines pumps & compressors
ES2132243T3 (es) * 1992-08-10 1999-08-16 Dow Deutschland Inc Procedimiento y dispositivo para vigilar y controlar un compresor.
CN1193686A (zh) * 1997-03-13 1998-09-23 张春智 透平膨胀喷射汽轮机
DE112005002547A5 (de) * 2004-11-02 2007-09-13 Alstom Technology Ltd. Optimierte Turbinenstufe einer Turbinenanlage sowie Auslegungsverfahren
ITMI20110684A1 (it) * 2011-04-21 2012-10-22 Exergy Orc S R L Impianto e processo per la produzione di energia tramite ciclo rankine organico
ITBS20120008A1 (it) 2012-01-20 2013-07-21 Turboden Srl Metodo e turbina per espandere un fluido di lavoro organico in un ciclo rankine

Also Published As

Publication number Publication date
CA2943409A1 (en) 2015-09-24
CN106255805A (zh) 2016-12-21
RU2016140620A (ru) 2018-04-23
US20170107819A1 (en) 2017-04-20
CN106255805B (zh) 2018-02-09
US20210071532A1 (en) 2021-03-11
RU2016140620A3 (tr) 2018-10-18
MX2016012187A (es) 2017-05-04
EP3119992B1 (en) 2018-09-26
WO2015140711A1 (en) 2015-09-24
US10876406B2 (en) 2020-12-29
JP2017519156A (ja) 2017-07-13
US11339661B2 (en) 2022-05-24
EP3119992A1 (en) 2017-01-25

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