RU2383784C2 - Съемный радиальный отводной коллектор - Google Patents

Съемный радиальный отводной коллектор Download PDF

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Publication number
RU2383784C2
RU2383784C2 RU2006106172/06A RU2006106172A RU2383784C2 RU 2383784 C2 RU2383784 C2 RU 2383784C2 RU 2006106172/06 A RU2006106172/06 A RU 2006106172/06A RU 2006106172 A RU2006106172 A RU 2006106172A RU 2383784 C2 RU2383784 C2 RU 2383784C2
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RU
Russia
Prior art keywords
manifold
compressor
channels
outlet
housing
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Application number
RU2006106172/06A
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English (en)
Russian (ru)
Other versions
RU2006106172A (ru
Inventor
Николас Фрэнсис МАРТИН (US)
Николас Фрэнсис МАРТИН
Джеймс Эдвард СЕНКЬЮЛА (US)
Джеймс Эдвард СЕНКЬЮЛА
Original Assignee
Дженерал Электрик Компани
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.)
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Application filed by Дженерал Электрик Компани filed Critical Дженерал Электрик Компани
Publication of RU2006106172A publication Critical patent/RU2006106172A/ru
Application granted granted Critical
Publication of RU2383784C2 publication Critical patent/RU2383784C2/ru

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    • 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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/06—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
    • F02C6/08—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas the gas being bled from the gas-turbine compressor
    • 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
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/105—Final actuators by passing part of the fluid
    • 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
    • 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
    • F04D29/52—Casings; Connections of working fluid for axial pumps
    • F04D29/54—Fluid-guiding means, e.g. diffusers
    • F04D29/541—Specially adapted for elastic fluid pumps
    • F04D29/545—Ducts

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Compressor (AREA)
  • Supercharger (AREA)
RU2006106172/06A 2005-02-28 2006-02-27 Съемный радиальный отводной коллектор RU2383784C2 (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11/066,167 US7374396B2 (en) 2005-02-28 2005-02-28 Bolt-on radial bleed manifold
US11/066,167 2005-02-28

Publications (2)

Publication Number Publication Date
RU2006106172A RU2006106172A (ru) 2007-09-27
RU2383784C2 true RU2383784C2 (ru) 2010-03-10

Family

ID=36615618

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2006106172/06A RU2383784C2 (ru) 2005-02-28 2006-02-27 Съемный радиальный отводной коллектор

Country Status (6)

Country Link
US (1) US7374396B2 (enExample)
EP (1) EP1696113B1 (enExample)
JP (1) JP5043347B2 (enExample)
CN (1) CN101082345B (enExample)
DE (1) DE602006001059D1 (enExample)
RU (1) RU2383784C2 (enExample)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8240979B2 (en) 2007-10-24 2012-08-14 United Technologies Corp. Gas turbine engine systems involving integrated fluid conduits
EP2189630A1 (de) * 2008-11-19 2010-05-26 Siemens Aktiengesellschaft Gasturbine, Leitschaufelträger für eine solche Gasturbine und Gas- bzw. Dampfturbinenanlage mit einer solchen Gasturbine
US8769954B2 (en) * 2009-12-31 2014-07-08 General Electric Company Frequency-tunable bracketless fluid manifold
WO2014120334A1 (en) 2013-01-29 2014-08-07 Sippel Aaron D Turbine shroud
EP2971577B1 (en) 2013-03-13 2018-08-29 Rolls-Royce Corporation Turbine shroud
US10190434B2 (en) 2014-10-29 2019-01-29 Rolls-Royce North American Technologies Inc. Turbine shroud with locating inserts
CA2915370A1 (en) 2014-12-23 2016-06-23 Rolls-Royce Corporation Full hoop blade track with axially keyed features
CA2915246A1 (en) 2014-12-23 2016-06-23 Rolls-Royce Corporation Turbine shroud
EP3045674B1 (en) 2015-01-15 2018-11-21 Rolls-Royce Corporation Turbine shroud with tubular runner-locating inserts
CA2924855A1 (en) 2015-04-29 2016-10-29 Rolls-Royce Corporation Keystoned blade track
CA2925588A1 (en) 2015-04-29 2016-10-29 Rolls-Royce Corporation Brazed blade track for a gas turbine engine
US10316695B2 (en) 2015-12-10 2019-06-11 General Electric Company Metallic attachment system integrated into a composite structure
US10240476B2 (en) 2016-01-19 2019-03-26 Rolls-Royce North American Technologies Inc. Full hoop blade track with interstage cooling air
US10247040B2 (en) 2016-01-19 2019-04-02 Rolls-Royce North American Technologies Inc. Turbine shroud with mounted full hoop blade track
US10480342B2 (en) 2016-01-19 2019-11-19 Rolls-Royce Corporation Gas turbine engine with health monitoring system
US10287906B2 (en) 2016-05-24 2019-05-14 Rolls-Royce North American Technologies Inc. Turbine shroud with full hoop ceramic matrix composite blade track and seal system
US10415415B2 (en) 2016-07-22 2019-09-17 Rolls-Royce North American Technologies Inc. Turbine shroud with forward case and full hoop blade track

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2642603A1 (de) * 1975-09-25 1977-03-31 Rolls Royce 1971 Ltd Kompressorgehaeuse fuer ein gasturbinentriebwerk
SU688717A1 (ru) * 1978-04-10 1979-09-30 Ордена Ленина И Ордена Трудового Красного Знамени Производственное Объединение "Невский Завод" Им. В.И.Ленина Система отбора воздуха из осевого компрессора
US4246274A (en) * 1978-05-10 1981-01-20 Bayer Aktiengesellschaft Antimycotic hydroxypropyl-imidazoles
SU1744311A1 (ru) * 1989-08-22 1992-06-30 Ленинградский Политехнический Институт Им.М.И.Калинина Входное или выходное устройство лопаточной турбомашины
RU2033563C1 (ru) * 1992-03-16 1995-04-20 Акционерное общество открытого типа "Авиадвигатель" Компрессор высокого давления двухконтурного турбореактивного двигателя
SU1080566A1 (ru) * 1982-07-01 1996-04-10 Производственное Объединение "Турбомоторный Завод" Им.К.Е.Ворошилова Система отбора воздуха из осевого компрессора

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE488010A (enExample) * 1947-03-11 1900-01-01
US2837270A (en) * 1952-07-24 1958-06-03 Gen Motors Corp Axial flow compressor
US3365124A (en) * 1966-02-21 1968-01-23 Gen Electric Compressor structure
US3945759A (en) * 1974-10-29 1976-03-23 General Electric Company Bleed air manifold
FR2452600A1 (fr) * 1979-03-28 1980-10-24 United Technologies Corp Moteur a turbine a gaz avec un carter de compresseur divise longitudinalement et comportant des collecteurs s'etendant circonferentiellement autour du carter
GB2192229B (en) * 1986-07-04 1990-05-02 Rolls Royce Plc A compressor and air bleed system
US5203162A (en) * 1990-09-12 1993-04-20 United Technologies Corporation Compressor bleed manifold for a gas turbine engine
AU648833B2 (en) * 1990-10-30 1994-05-05 Carrier Corporation Centrifugal compressor with pipe diffuser and collector
US6027304A (en) 1998-05-27 2000-02-22 General Electric Co. High pressure inlet bleed heat system for the compressor of a turbine
US6585482B1 (en) 2000-06-20 2003-07-01 General Electric Co. Methods and apparatus for delivering cooling air within gas turbines
US6438941B1 (en) 2001-04-26 2002-08-27 General Electric Company Bifurcated splitter for variable bleed flow
US6783324B2 (en) * 2002-08-15 2004-08-31 General Electric Company Compressor bleed case
US7596954B2 (en) * 2004-07-09 2009-10-06 United Technologies Corporation Blade clearance control
US7090462B2 (en) * 2004-08-18 2006-08-15 General Electric Company Compressor bleed air manifold for blade clearance control
FR2875866B1 (fr) * 2004-09-30 2006-12-08 Snecma Moteurs Sa Procede de circulation d'air dans un compresseur de turbomachine, agencement de compresseur le mettant en oeuvre , etage de compression et compresseur comportant un tel agencement, et moteur d'aeronef equipe d'un tel compresseur

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2642603A1 (de) * 1975-09-25 1977-03-31 Rolls Royce 1971 Ltd Kompressorgehaeuse fuer ein gasturbinentriebwerk
SU688717A1 (ru) * 1978-04-10 1979-09-30 Ордена Ленина И Ордена Трудового Красного Знамени Производственное Объединение "Невский Завод" Им. В.И.Ленина Система отбора воздуха из осевого компрессора
US4246274A (en) * 1978-05-10 1981-01-20 Bayer Aktiengesellschaft Antimycotic hydroxypropyl-imidazoles
SU1080566A1 (ru) * 1982-07-01 1996-04-10 Производственное Объединение "Турбомоторный Завод" Им.К.Е.Ворошилова Система отбора воздуха из осевого компрессора
SU1744311A1 (ru) * 1989-08-22 1992-06-30 Ленинградский Политехнический Институт Им.М.И.Калинина Входное или выходное устройство лопаточной турбомашины
RU2033563C1 (ru) * 1992-03-16 1995-04-20 Акционерное общество открытого типа "Авиадвигатель" Компрессор высокого давления двухконтурного турбореактивного двигателя

Also Published As

Publication number Publication date
JP2006242184A (ja) 2006-09-14
EP1696113A1 (en) 2006-08-30
CN101082345A (zh) 2007-12-05
DE602006001059D1 (de) 2008-06-19
US20060193719A1 (en) 2006-08-31
CN101082345B (zh) 2010-12-08
EP1696113B1 (en) 2008-05-07
JP5043347B2 (ja) 2012-10-10
US7374396B2 (en) 2008-05-20
RU2006106172A (ru) 2007-09-27

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