JP2008025578A5 - - Google Patents

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Publication number
JP2008025578A5
JP2008025578A5 JP2007186669A JP2007186669A JP2008025578A5 JP 2008025578 A5 JP2008025578 A5 JP 2008025578A5 JP 2007186669 A JP2007186669 A JP 2007186669A JP 2007186669 A JP2007186669 A JP 2007186669A JP 2008025578 A5 JP2008025578 A5 JP 2008025578A5
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JP
Japan
Prior art keywords
annular
downstream
metal plate
air
impeller
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.)
Granted
Application number
JP2007186669A
Other languages
English (en)
Japanese (ja)
Other versions
JP4956809B2 (ja
JP2008025578A (ja
Filing date
Publication date
Priority claimed from FR0606541A external-priority patent/FR2904036B1/fr
Application filed filed Critical
Publication of JP2008025578A publication Critical patent/JP2008025578A/ja
Publication of JP2008025578A5 publication Critical patent/JP2008025578A5/ja
Application granted granted Critical
Publication of JP4956809B2 publication Critical patent/JP4956809B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2007186669A 2006-07-19 2007-07-18 遠心圧縮機のインペラの下流側空洞の換気システム Active JP4956809B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0606541 2006-07-19
FR0606541A FR2904036B1 (fr) 2006-07-19 2006-07-19 Systeme de ventilation d'une cavite aval de rouet de compresseur centrifuge

Publications (3)

Publication Number Publication Date
JP2008025578A JP2008025578A (ja) 2008-02-07
JP2008025578A5 true JP2008025578A5 (enExample) 2010-08-12
JP4956809B2 JP4956809B2 (ja) 2012-06-20

Family

ID=37770941

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2007186669A Active JP4956809B2 (ja) 2006-07-19 2007-07-18 遠心圧縮機のインペラの下流側空洞の換気システム

Country Status (6)

Country Link
US (1) US7942630B2 (enExample)
EP (1) EP1882826B1 (enExample)
JP (1) JP4956809B2 (enExample)
CA (1) CA2594008C (enExample)
FR (1) FR2904036B1 (enExample)
RU (1) RU2433310C2 (enExample)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8075247B2 (en) * 2007-12-21 2011-12-13 Pratt & Whitney Canada Corp. Centrifugal impeller with internal heating
US8147178B2 (en) * 2008-12-23 2012-04-03 General Electric Company Centrifugal compressor forward thrust and turbine cooling apparatus
US8087249B2 (en) * 2008-12-23 2012-01-03 General Electric Company Turbine cooling air from a centrifugal compressor
US9228497B2 (en) 2010-12-30 2016-01-05 Rolls-Royce Corporation Gas turbine engine with secondary air flow circuit
GB2510004B (en) * 2013-08-19 2015-10-14 Rolls Royce Plc Axial flow machine cooling system
FR3025260B1 (fr) * 2014-08-29 2019-08-30 Safran Aircraft Engines Compresseur centrifuge a resistance amelioree
US10208668B2 (en) * 2015-09-30 2019-02-19 Rolls-Royce Corporation Turbine engine advanced cooling system
US10830144B2 (en) 2016-09-08 2020-11-10 Rolls-Royce North American Technologies Inc. Gas turbine engine compressor impeller cooling air sinks
JP6750998B2 (ja) * 2016-10-07 2020-09-02 パナソニックｉ−ＰＲＯセンシングソリューションズ株式会社 監視システム及び監視方法
FR3062682B1 (fr) * 2017-02-07 2019-04-19 Safran Aircraft Engines Partie de turbomachine comprenant une paroi de separation de deux cavites pourvue de bossages
CN107725479B (zh) * 2017-09-26 2019-09-24 中国科学院工程热物理研究所 一种旋转盘腔内部的转子罩壳结构及包含该结构的发动机
US11049176B1 (en) 2020-01-10 2021-06-29 House Of Skye Ltd Systems/methods for identifying products within audio-visual content and enabling seamless purchasing of such identified products by viewers/users of the audio-visual content
US11525393B2 (en) 2020-03-19 2022-12-13 Rolls-Royce Corporation Turbine engine with centrifugal compressor having impeller backplate offtake
FR3137409A1 (fr) * 2022-07-04 2024-01-05 Safran Helicopter Engines Compresseur pour aéronef
US11773773B1 (en) 2022-07-26 2023-10-03 Rolls-Royce North American Technologies Inc. Gas turbine engine centrifugal compressor with impeller load and cooling control
FR3160436B1 (fr) * 2024-03-19 2026-03-20 Safran Aircraft Engines système de contrôle de la pressurisation d’une cavité aval de rotor de compresseur centrifuge dans une turbomachine
FR3166163A1 (fr) 2024-09-06 2026-03-13 Safran Aircraft Engines Module pour une turbomachine d’aeronef
FR3166178A1 (fr) 2024-09-06 2026-03-13 Safran Aircraft Engines Module pour une turbomachine d’aeronef
FR3166165A1 (fr) 2024-09-06 2026-03-13 Safran Aircraft Engines Module pour une turbomachine d’aeronef
FR3166167A1 (fr) 2024-09-06 2026-03-13 Safran Aircraft Engines Module pour une turbomachine d’aeronef
FR3166164A1 (fr) 2024-09-06 2026-03-13 Safran Aircraft Engines Module pour une turbomachine d’aeronef

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE968742C (de) * 1944-09-22 1958-03-27 Daimler Benz Ag Mehrstufiges Radialgeblaese, vorzugsweise Ladegeblaese fuer Flugmotoren
GB1047014A (en) * 1962-07-03 1966-11-02 English Electric Co Ltd Improvements in or relating to hydraulic pumps, turbines or reversible pump turbines
FR1472085A (fr) * 1965-11-18 1967-03-10 Snecma Perfectionnement aux compresseurs contra-rotatifs
US3469772A (en) * 1967-07-19 1969-09-30 Donald A Mcdonald Air moving apparatus
US4462204A (en) * 1982-07-23 1984-07-31 General Electric Company Gas turbine engine cooling airflow modulator
SU1222900A1 (ru) * 1984-11-22 1986-04-07 Производственное объединение "Невский завод" им.В.И.Ленина Сигнализатор помпажа турбокомпрессора
JPS62143098A (ja) * 1985-12-18 1987-06-26 松下電器産業株式会社 明瞭度評価用単音節の合成方法
DE4225625A1 (de) * 1992-08-03 1994-02-10 Asea Brown Boveri Abgasturbolader
GB2290113B (en) * 1994-05-31 1998-07-15 Ingersoll Dresser Pump Co Centrifugal pump
US5555721A (en) * 1994-09-28 1996-09-17 General Electric Company Gas turbine engine cooling supply circuit
JPH1089291A (ja) * 1996-09-11 1998-04-07 Tochigi Fuji Ind Co Ltd 遠心式コンプレッサ
US5996331A (en) * 1997-09-15 1999-12-07 Alliedsignal Inc. Passive turbine coolant regulator responsive to engine load
US6035627A (en) * 1998-04-21 2000-03-14 Pratt & Whitney Canada Inc. Turbine engine with cooled P3 air to impeller rear cavity
EP0961033B1 (de) * 1998-05-25 2003-10-08 ABB Turbo Systems AG Radialverdichter
JP2001123997A (ja) * 1999-10-21 2001-05-08 Hitachi Ltd 磁気軸受搭載遠心圧縮機
JP4375883B2 (ja) * 2000-06-02 2009-12-02 本田技研工業株式会社 ガスタービンエンジンの軸受へのシールエア供給装置
US6276896B1 (en) * 2000-07-25 2001-08-21 Joseph C. Burge Apparatus and method for cooling Axi-Centrifugal impeller
RU2208177C1 (ru) * 2002-07-15 2003-07-10 Открытое акционерное общество Авиамоторный научно-технический комплекс "Союз" Двухконтурный турбореактивный двигатель
JP4125985B2 (ja) * 2003-03-31 2008-07-30 株式会社山田製作所 ウォーターポンプ
DE10325980A1 (de) * 2003-06-07 2004-12-23 Daimlerchrysler Ag Abgasturbolader

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