CN101082345B - 螺栓固定的径向排气管 - Google Patents

螺栓固定的径向排气管 Download PDF

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Publication number
CN101082345B
CN101082345B CN2006100515094A CN200610051509A CN101082345B CN 101082345 B CN101082345 B CN 101082345B CN 2006100515094 A CN2006100515094 A CN 2006100515094A CN 200610051509 A CN200610051509 A CN 200610051509A CN 101082345 B CN101082345 B CN 101082345B
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CN
China
Prior art keywords
compressor
assembly
pipe
outlet pipe
discharge
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Fee Related
Application number
CN2006100515094A
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English (en)
Chinese (zh)
Other versions
CN101082345A (zh
Inventor
N·F·马丁
J·E·森库拉
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General Electric Co
Original Assignee
General Electric Co
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Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Publication of CN101082345A publication Critical patent/CN101082345A/zh
Application granted granted Critical
Publication of CN101082345B publication Critical patent/CN101082345B/zh
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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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)
CN2006100515094A 2005-02-28 2006-02-28 螺栓固定的径向排气管 Expired - Fee Related CN101082345B (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11/066167 2005-02-28
US11/066,167 US7374396B2 (en) 2005-02-28 2005-02-28 Bolt-on radial bleed manifold

Publications (2)

Publication Number Publication Date
CN101082345A CN101082345A (zh) 2007-12-05
CN101082345B true CN101082345B (zh) 2010-12-08

Family

ID=36615618

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2006100515094A Expired - Fee Related CN101082345B (zh) 2005-02-28 2006-02-28 螺栓固定的径向排气管

Country Status (6)

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

Families Citing this family (18)

* 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
CA2896500A1 (en) 2013-01-29 2014-08-07 Rolls-Royce Corporation 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
CA2924866A1 (en) 2015-04-29 2016-10-29 Daniel K. Vetters Composite 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
US10247040B2 (en) 2016-01-19 2019-04-02 Rolls-Royce North American Technologies Inc. Turbine shroud with mounted full hoop blade track
US10240476B2 (en) 2016-01-19 2019-03-26 Rolls-Royce North American Technologies Inc. Full hoop blade track with interstage cooling air
US10480342B2 (en) 2016-01-19 2019-11-19 Rolls-Royce Corporation Gas turbine engine with health monitoring 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
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
US12595762B2 (en) 2023-02-17 2026-04-07 Rtx Corporation Gas turbine engine with bleed diffuser baffles

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
US5203162A (en) * 1990-09-12 1993-04-20 United Technologies Corporation Compressor bleed manifold for a gas turbine engine
CN1022854C (zh) * 1990-10-30 1993-11-24 运载器有限公司 带有管道扩压器和集气器的离心压缩机

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE488010A (https=) * 1947-03-11 1900-01-01
GB1518293A (en) * 1975-09-25 1978-07-19 Rolls Royce Axial flow compressors particularly for gas turbine engines
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
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
SU1080566A1 (ru) * 1982-07-01 1996-04-10 Производственное Объединение "Турбомоторный Завод" Им.К.Е.Ворошилова Система отбора воздуха из осевого компрессора
GB2192229B (en) * 1986-07-04 1990-05-02 Rolls Royce Plc A compressor and air bleed system
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
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 (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
US5203162A (en) * 1990-09-12 1993-04-20 United Technologies Corporation Compressor bleed manifold for a gas turbine engine
CN1022854C (zh) * 1990-10-30 1993-11-24 运载器有限公司 带有管道扩压器和集气器的离心压缩机

Also Published As

Publication number Publication date
CN101082345A (zh) 2007-12-05
EP1696113B1 (en) 2008-05-07
DE602006001059D1 (de) 2008-06-19
US7374396B2 (en) 2008-05-20
US20060193719A1 (en) 2006-08-31
RU2383784C2 (ru) 2010-03-10
JP2006242184A (ja) 2006-09-14
JP5043347B2 (ja) 2012-10-10
RU2006106172A (ru) 2007-09-27
EP1696113A1 (en) 2006-08-30

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SE01 Entry into force of request for substantive examination
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CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20101208

Termination date: 20160228

CF01 Termination of patent right due to non-payment of annual fee