JP2006242184A5 - - Google Patents
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- Publication number
- JP2006242184A5 JP2006242184A5 JP2006049675A JP2006049675A JP2006242184A5 JP 2006242184 A5 JP2006242184 A5 JP 2006242184A5 JP 2006049675 A JP2006049675 A JP 2006049675A JP 2006049675 A JP2006049675 A JP 2006049675A JP 2006242184 A5 JP2006242184 A5 JP 2006242184A5
- Authority
- JP
- Japan
- Prior art keywords
- assembly
- manifold
- bleed
- compressor case
- channels
- 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
Links
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 (3)
| Publication Number | Publication Date |
|---|---|
| JP2006242184A JP2006242184A (ja) | 2006-09-14 |
| JP2006242184A5 true JP2006242184A5 (enExample) | 2009-04-09 |
| JP5043347B2 JP5043347B2 (ja) | 2012-10-10 |
Family
ID=36615618
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2006049675A Expired - Fee Related JP5043347B2 (ja) | 2005-02-28 | 2006-02-27 | 抽気マニホルドおよびコンプレッサー・ケースアセンブリ |
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)
| 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 |
Family Cites Families (21)
| 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 |
| 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 |
| 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 |
| 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 |
-
2005
- 2005-02-28 US US11/066,167 patent/US7374396B2/en not_active Expired - Fee Related
-
2006
- 2006-02-23 EP EP06250955A patent/EP1696113B1/en not_active Not-in-force
- 2006-02-23 DE DE602006001059T patent/DE602006001059D1/de active Active
- 2006-02-27 JP JP2006049675A patent/JP5043347B2/ja not_active Expired - Fee Related
- 2006-02-27 RU RU2006106172/06A patent/RU2383784C2/ru active
- 2006-02-28 CN CN2006100515094A patent/CN101082345B/zh not_active Expired - Fee Related
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