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MX2017016039A - Turbomaquina de capa limite, unidad de rotor y particion correspondientes. - Google Patents

Turbomaquina de capa limite, unidad de rotor y particion correspondientes.

Info

Publication number
MX2017016039A
MX2017016039A MX2017016039A MX2017016039A MX2017016039A MX 2017016039 A MX2017016039 A MX 2017016039A MX 2017016039 A MX2017016039 A MX 2017016039A MX 2017016039 A MX2017016039 A MX 2017016039A MX 2017016039 A MX2017016039 A MX 2017016039A
Authority
MX
Mexico
Prior art keywords
rotor assembly
boundary layer
partition
layer turbomachine
corresponding rotor
Prior art date
Application number
MX2017016039A
Other languages
English (en)
Inventor
W Helton Billy
W Jones Mark
Original Assignee
Green Frog Turbines Uk Ltd
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
Priority claimed from EP15171531.5A external-priority patent/EP3103962A1/en
Priority claimed from EP15171530.7A external-priority patent/EP3103961B1/en
Application filed by Green Frog Turbines Uk Ltd filed Critical Green Frog Turbines Uk Ltd
Publication of MX2017016039A publication Critical patent/MX2017016039A/es

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
    • F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/34—Non-positive-displacement machines or engines, e.g. steam turbines characterised by non-bladed rotor, e.g. with drilled holes
    • F01D1/36—Non-positive-displacement machines or engines, e.g. steam turbines characterised by non-bladed rotor, e.g. with drilled holes using fluid friction
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D17/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
    • F04D17/08—Centrifugal pumps
    • F04D17/16—Centrifugal pumps for displacing without appreciable compression
    • F04D17/161—Shear force 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
    • F04D23/00—Other rotary non-positive-displacement 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
    • 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
    • F04D29/445—Fluid-guiding means, e.g. diffusers especially adapted for liquid pumps
    • F04D29/448—Fluid-guiding means, e.g. diffusers especially adapted for liquid pumps bladed diffusers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D5/00—Pumps with circumferential or transverse flow
    • F04D5/001—Shear force pumps
    • 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
    • F05D2210/44—Flow geometry or direction bidirectional, i.e. in opposite, alternating directions
    • 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
    • F05D2250/20—Three-dimensional
    • F05D2250/29—Three-dimensional machined; miscellaneous
    • F05D2250/292—Three-dimensional machined; miscellaneous tapered
    • 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
    • F05D2250/52—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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603—Composites; e.g. fibre-reinforced
    • 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
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

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

Abstract

Una turbomáquina de capa límite (100) puede incluir un alojamiento (110) que define un espacio interior (115) y que incluye una abertura de entrada (112) y una abertura de salida (113) para facilitar el movimiento de un fluido a través del alojamiento (110). La turbomáquina de capa límite (100) puede incluir, además, una unidad de rotor (120) dispuesta en la cámara del rotor (117) y configurada para girar alrededor de un eje de rotación (101). La unidad de rotor (120) puede tener una pluralidad de discos (121) separados a lo largo del eje de rotación (101) y que definen una abertura interior a lo largo del eje de rotación (101). El fluido puede pasar a través de las separaciones entre los discos (121) y la abertura interior conforme el fluido se mueve a través del alojamiento (110). Se proporcionan, además, la unidad de rotor y la partición correspondientes.
MX2017016039A 2015-06-10 2016-06-10 Turbomaquina de capa limite, unidad de rotor y particion correspondientes. MX2017016039A (es)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
EP15171531.5A EP3103962A1 (en) 2015-06-10 2015-06-10 Rotor for a boundary layer turbomachine and boundary layer turbomachine
EP15171530.7A EP3103961B1 (en) 2015-06-10 2015-06-10 Boundary layer turbomachine and corrresponding operating method
US14/991,228 US11208890B2 (en) 2015-01-09 2016-01-08 Boundary layer turbomachine
PCT/IB2016/001360 WO2016198962A2 (en) 2015-06-10 2016-06-10 Boundary layer turbomachine

Publications (1)

Publication Number Publication Date
MX2017016039A true MX2017016039A (es) 2018-12-06

Family

ID=56850322

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2017016039A MX2017016039A (es) 2015-06-10 2016-06-10 Turbomaquina de capa limite, unidad de rotor y particion correspondientes.

Country Status (9)

Country Link
US (2) US11208890B2 (es)
JP (1) JP2018521268A (es)
KR (1) KR20180098215A (es)
CN (1) CN109983202A (es)
AU (1) AU2016276259A1 (es)
CA (1) CA2989093A1 (es)
MX (1) MX2017016039A (es)
PH (1) PH12018500094A1 (es)
WO (1) WO2016198962A2 (es)

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US10766544B2 (en) 2017-12-29 2020-09-08 ESS 2 Tech, LLC Airfoils and machines incorporating airfoils
US20210290986A1 (en) * 2020-03-18 2021-09-23 TruBlue LLC Line dispensing devices
KR20230027999A (ko) * 2021-08-20 2023-02-28 유성훈 디스크형 터빈 증기 원동소
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DE102021005466A1 (de) 2021-11-04 2023-05-04 Truma Gerätetechnik GmbH & Co. KG Vorrichtung zum Erhitzen einer Flüssigkeit und/oder zum Erwärmen von Luft sowie Seitenkanalgebläse

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Also Published As

Publication number Publication date
CN109983202A (zh) 2019-07-05
US11208890B2 (en) 2021-12-28
WO2016198962A2 (en) 2016-12-15
CA2989093A1 (en) 2016-12-15
US20200256191A1 (en) 2020-08-13
PH12018500094A1 (en) 2018-07-09
KR20180098215A (ko) 2018-09-03
JP2018521268A (ja) 2018-08-02
WO2016198962A3 (en) 2017-02-09
US20160258442A1 (en) 2016-09-08
AU2016276259A1 (en) 2018-01-25

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