BR112012027246A2 - turbina dotada de sistema de válvula de ar de vedação - Google Patents

turbina dotada de sistema de válvula de ar de vedação

Info

Publication number
BR112012027246A2
BR112012027246A2 BR112012027246A BR112012027246A BR112012027246A2 BR 112012027246 A2 BR112012027246 A2 BR 112012027246A2 BR 112012027246 A BR112012027246 A BR 112012027246A BR 112012027246 A BR112012027246 A BR 112012027246A BR 112012027246 A2 BR112012027246 A2 BR 112012027246A2
Authority
BR
Brazil
Prior art keywords
air
air valve
valve system
turbine
sealing air
Prior art date
Application number
BR112012027246A
Other languages
English (en)
Inventor
Christopher Sidney
Trevor Milne
Original Assignee
Siemens Ag
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 Siemens Ag filed Critical Siemens Ag
Publication of BR112012027246A2 publication Critical patent/BR112012027246A2/pt

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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/18—Lubricating arrangements
    • F01D25/183—Sealing means
    • 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
    • F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
    • F01D11/04—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type using sealing fluid, e.g. steam
    • F01D11/06—Control thereof
    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/28—Arrangement of seals
    • 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
    • F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth 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
    • F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
    • F01D11/04—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type using sealing fluid, e.g. steam
    • 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
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/09—Purpose of the control system to cope with emergencies
    • 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
    • F05D2270/00—Control
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/304—Spool rotational speed

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Magnetic Bearings And Hydrostatic Bearings (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)

Abstract

turbina dotada de sistema de válvula de ar de vedação. a presente invenção refere-se a uma turbina (1), compreendendo: um rotor (2); um mancal de fluido (31) de modo a suportar o rotor de forma rotativa; um sistema de condutos de suprimento de ar (45, 47) para suprimento de ar na direção do mancal de fluido; um sistema de condutos de descarga (57, 59,61,63) para a descarga de uma porção do ar suprido; um sistema de controle (67, 71) disposto de modo a modificar uma quantidade de ar que é descarregado através do sistema de condutos de descarga com base em uma condição de funcionamento de turbina.
BR112012027246A 2010-04-28 2011-03-30 turbina dotada de sistema de válvula de ar de vedação BR112012027246A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP10161310A EP2383440A1 (en) 2010-04-28 2010-04-28 Turbine including seal air valve system
PCT/EP2011/054929 WO2011134730A2 (en) 2010-04-28 2011-03-30 Turbine including seal air valve system

Publications (1)

Publication Number Publication Date
BR112012027246A2 true BR112012027246A2 (pt) 2016-07-26

Family

ID=42752032

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112012027246A BR112012027246A2 (pt) 2010-04-28 2011-03-30 turbina dotada de sistema de válvula de ar de vedação

Country Status (6)

Country Link
US (1) US9429037B2 (pt)
EP (2) EP2383440A1 (pt)
CN (1) CN103026004B (pt)
BR (1) BR112012027246A2 (pt)
RU (1) RU2562682C2 (pt)
WO (1) WO2011134730A2 (pt)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9617916B2 (en) 2012-11-28 2017-04-11 Pratt & Whitney Canada Corp. Gas turbine engine with bearing buffer air flow and method
US20160003142A1 (en) * 2014-06-11 2016-01-07 United Technologies Corporation Geared turbofan with gearbox seal
US9944399B2 (en) 2014-08-07 2018-04-17 Pratt & Whitney Canada Corp. Seal assembly for a bearing assembly in a gas turbine engine
EP3054089A1 (de) 2015-02-05 2016-08-10 Siemens Aktiengesellschaft Turbomaschinen-Hohlwelle mit Hitzeschild
GB201517770D0 (en) 2015-10-08 2015-11-25 Birmingham High Performance Turbomachinery Ltd Improvements in or relating to gas bearings
US10550724B2 (en) * 2016-10-11 2020-02-04 General Electric Company System and method for the pressurization of a sump of a gas turbine engine
US10520035B2 (en) 2016-11-04 2019-12-31 United Technologies Corporation Variable volume bearing compartment
US10458267B2 (en) * 2017-09-20 2019-10-29 General Electric Company Seal assembly for counter rotating turbine assembly
EP4127434A4 (en) * 2020-04-03 2024-04-17 Technion Research & Development Foundation Ltd. ADDITIVELY MANUFACTURED GAS TURBINE ENGINE AND FAN
US20220162993A1 (en) * 2020-11-23 2022-05-26 Raytheon Technologies Corporation Starter turbine bearing compartment buffer air

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB702931A (en) 1951-04-18 1954-01-27 Bristol Aeroplane Co Ltd Improvements in or relating to rotary machines comprising fluid compressing means
US4156342A (en) * 1976-06-11 1979-05-29 Westinghouse Canada Limited Cooling apparatus for a bearing in a gas turbine
US4193603A (en) * 1978-12-21 1980-03-18 Carrier Corporation Sealing system for a turbomachine
GB2111607B (en) 1981-12-08 1985-09-18 Rolls Royce Bearing chamber pressurisation system for a machine
US4433539A (en) * 1982-05-13 1984-02-28 United Technologies Corporation Means for controlling air scavenge pressure in the bearing compartment of gas turbines
DE3826217A1 (de) 1988-08-02 1990-02-08 Mtu Muenchen Gmbh Gasturbine mit einer verdichterseitigen lagerkammer
FR2698406B1 (fr) 1992-11-25 1994-12-23 Snecma Procédé de pressurisation d'enceintes lubrifiées d'une turbomachine.
DE4435322B4 (de) * 1994-10-01 2005-05-04 Alstom Verfahren und Vorrichtung zur Wellendichtung und zur Kühlung auf der Abgasseite einer axialdurchströmten Gasturbine
US6142672A (en) * 1998-06-22 2000-11-07 Bently Nevada Corporation Fluid flow and control system for a hydrostatic bearing supporting rotating equipment: method and apparatus
RU2167322C2 (ru) 1999-06-25 2001-05-20 Открытое акционерное общество "Авиадвигатель" Газотурбинная установка
IT1318065B1 (it) * 2000-06-29 2003-07-21 Nuovo Pignone Spa Sistema di tenuta e di pressurizzazione per il cuscino portante di una turbina a gas
RU2211936C2 (ru) 2001-05-04 2003-09-10 Открытое акционерное общество "Авиадвигатель" Газотурбинный двигатель
US20030097872A1 (en) * 2001-11-29 2003-05-29 Granitz Charles Robert System for reducing oil consumption in gas turbine engines
JP4773804B2 (ja) 2005-11-17 2011-09-14 三菱重工業株式会社 ガスタービン
UA87670C2 (ru) * 2006-06-05 2009-08-10 Государственное Предприятие "Научно-Производственный Комплекс Газотурбостроения "Заря"- "Машпроект" Газотурбинный двигатель с валом отбора мощности от силовой турбины в направлении, противоположном течению воздуха

Also Published As

Publication number Publication date
CN103026004B (zh) 2015-12-16
RU2012150811A (ru) 2014-06-10
EP2383440A1 (en) 2011-11-02
US20130039739A1 (en) 2013-02-14
WO2011134730A2 (en) 2011-11-03
WO2011134730A3 (en) 2015-06-25
RU2562682C2 (ru) 2015-09-10
CN103026004A (zh) 2013-04-03
US9429037B2 (en) 2016-08-30
EP2529084A2 (en) 2012-12-05

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Legal Events

Date Code Title Description
B08F Application fees: application dismissed [chapter 8.6 patent gazette]
B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]
B350 Update of information on the portal [chapter 15.35 patent gazette]