JP2010031871A - ガスタービンエンジン用のファンケーシング - Google Patents
ガスタービンエンジン用のファンケーシング Download PDFInfo
- Publication number
- JP2010031871A JP2010031871A JP2009176047A JP2009176047A JP2010031871A JP 2010031871 A JP2010031871 A JP 2010031871A JP 2009176047 A JP2009176047 A JP 2009176047A JP 2009176047 A JP2009176047 A JP 2009176047A JP 2010031871 A JP2010031871 A JP 2010031871A
- Authority
- JP
- Japan
- Prior art keywords
- fan
- casing
- blade
- fan casing
- blades
- 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.)
- Ceased
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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
- F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
- F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
- F01D21/045—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of rotor
-
- 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
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
- F04D27/02—Surge control
- F04D27/0292—Stop safety or alarm devices, e.g. stop-and-go control; Disposition of check-valves
-
- 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
- F04D29/02—Selection of particular materials
- F04D29/023—Selection of particular materials especially adapted for elastic fluid pumps
-
- 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
- F04D29/522—Casings; Connections of working fluid for axial pumps especially adapted for elastic fluid pumps
- F04D29/526—Details of the casing section radially opposing blade tips
-
- 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
- F05D2240/00—Components
- F05D2240/10—Stators
- F05D2240/12—Fluid guiding means, e.g. vanes
- F05D2240/121—Fluid guiding means, e.g. vanes related to the leading edge of a stator vane
-
- 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
- F05D2240/00—Components
- F05D2240/20—Rotors
- F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
- F05D2240/303—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the leading edge of a rotor blade
-
- 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
- F05D2250/00—Geometry
- F05D2250/20—Three-dimensional
- F05D2250/28—Three-dimensional patterned
- F05D2250/283—Three-dimensional patterned honeycomb
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
【解決手段】 ガスタービンエンジン用ファンケーシングは、ファンブレードの上流部分だけに亘って延びる、ファントラックライナを有している。ケーシングの局所的剛性及び内部形状は、外れたファンブレードの破壊を促進すると同時に、ブレードの前縁領域がファントラックライナを貫通でき、ファンケーシングによって捕捉されるように構成されている。この構成は、前縁領域の剛性及び圧縮強度がブレードの残りの領域におけるよりもかなり高いファンブレード、例えば金属製中空ファンブレード又は金属製前縁キャップを持つ複合ファンブレードに特に適している。
【選択図】図4
Description
外れたファンブレード423がケーシングと接触したとき、複合材料の強度を越える大きな圧縮負荷が(ブレードの長さ方向に)発生する。圧縮力に良好に耐えることができる比較的剛性の前縁キャップは、例外であり、比較的長期に亘って残り、従って、捕捉ケーシングに多くの脅威を与える。従って、この特徴は、公知の構成で使用されたのと異なる捕捉戦略を必要とする。
11 インテーク
12 ファン
13 中圧コンプレッサ
14 高圧コンプレッサ
15 燃焼器
16 高圧タービン
17 中圧タービン
18 低圧タービン
19 排気ノズル
20、21、22 駆動シャフト
23 ファンブレード
24 ファンディスク
25 ファンケーシング
223 スウェプトファンブレード
226 後縁
228 ブレード先端
Claims (9)
- ガスタービンエンジン用のファンケーシングであって、
前記エンジンは、使用時に前記エンジンの軸線を中心として回転する複数のファンブレードを備えており、
前記ケーシングは、前記ファンブレードの半径方向外方の環状構造を備えており、
この環状構造は、前記ファンブレードの上流及び下流の両方で軸線方向に延び、使用時にファンブレードがほぼ半径方向外方に外れて前記ケーシングに衝突する可能性があり、
前記ケーシングは、使用時に、外れたファンブレードの一部が貫通できるファントラックライナを備えた、ファンケーシングにおいて、
前記ファントラックライナは、前記ファンブレードの上流部分だけに亘って延びている、ことを特徴とするファンケーシング。 - 請求項1に記載のファンケーシングにおいて、
前記ファントラックライナは、前記ファンブレードの前縁領域だけに亘って延びている、ファンケーシング。 - 請求項1に記載のファンケーシングにおいて、
前記ファンケーシングの半径方向内面は、研磨性層を備えている、ファンケーシング。 - 請求項3に記載のファンケーシングにおいて、
前記研磨性層は、前記ファンブレードの軸線方向全長に亘って延びている、ファンケーシング。 - 請求項4に記載のファンケーシングにおいて、
前記ファントラックライナの下流の前記研磨性層は、前記ファンケーシングの半径方向内面に直接的に取り付けられている、ファンケーシング。 - 請求項1に記載のファンケーシングにおいて、
前記ファントラックライナは、複数の別体のライナパネルを備えている、ファンケーシング。 - 請求項6に記載のファンケーシングにおいて、
前記ライナパネルは、前記ファンケーシングにクリップで取り付けられている、ファンケーシング。 - ガスタービンエンジン用のファンケーシングであって、
前記ファンケーシングの内部形状及び高い局所的剛性により、使用時に、外れたファンブレードの破壊が促進される、ことを特徴とするファンケーシング。 - 請求項8に記載のファンケーシングにおいて、
外れたファンブレードの前記前縁領域を捕捉するように構成されている、ファンケーシング。
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GBGB0813820.8A GB0813820D0 (en) | 2008-07-29 | 2008-07-29 | A fan casing for a gas turbine engine |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2010031871A true JP2010031871A (ja) | 2010-02-12 |
JP2010031871A5 JP2010031871A5 (ja) | 2012-09-13 |
Family
ID=39747089
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2009176047A Ceased JP2010031871A (ja) | 2008-07-29 | 2009-07-29 | ガスタービンエンジン用のファンケーシング |
Country Status (4)
Country | Link |
---|---|
US (1) | US8231328B2 (ja) |
EP (1) | EP2149679B2 (ja) |
JP (1) | JP2010031871A (ja) |
GB (1) | GB0813820D0 (ja) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2012062049A (ja) * | 2010-09-15 | 2012-03-29 | Ge Aviation Systems Ltd | 疎氷性コーティングを施したプロペラブレード |
JP2013155741A (ja) * | 2012-01-31 | 2013-08-15 | United Technologies Corp <Utc> | ターボファンエンジンファンケースカートリッジ、ターボファンエンジンファンケースカートリッジの製造方法、およびターボファンエンジンファンケースカートリッジの製造用固定具 |
US9249681B2 (en) | 2012-01-31 | 2016-02-02 | United Technologies Corporation | Fan case rub system |
US10669936B2 (en) | 2013-03-13 | 2020-06-02 | Raytheon Technologies Corporation | Thermally conforming acoustic liner cartridge for a gas turbine engine |
Families Citing this family (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2013102171A2 (en) * | 2011-12-31 | 2013-07-04 | Rolls-Royce Corporation | Blade track assembly, components, and methods |
GB2498194A (en) * | 2012-01-05 | 2013-07-10 | Rolls Royce Plc | Ice impact panel for a gas turbine engine |
US9644493B2 (en) | 2012-09-07 | 2017-05-09 | United Technologies Corporation | Fan case ballistic liner and method of manufacturing same |
GB201302492D0 (en) * | 2013-02-13 | 2013-03-27 | Rolls Royce Plc | A Fan Containment System with Temporarily Deformable Panel |
GB201302493D0 (en) | 2013-02-13 | 2013-03-27 | Rolls Royce Plc | A Fan Containment System |
US10077671B2 (en) | 2013-03-13 | 2018-09-18 | United Technologies Corporation | Thermally conformable liner for reducing system level fan blade out loads |
DE102013207452A1 (de) * | 2013-04-24 | 2014-11-13 | MTU Aero Engines AG | Gehäuseabschnitt einer Turbomaschinenverdichter- oder Turbomaschinenturbinenstufe |
US9683490B2 (en) * | 2013-11-21 | 2017-06-20 | Rolls-Royce Plc | Pivoting fan track liner for blade retainment |
US10094242B2 (en) | 2014-02-25 | 2018-10-09 | United Technologies Corporation | Repair or remanufacture of liner panels for a gas turbine engine |
US9737930B2 (en) | 2015-01-20 | 2017-08-22 | United Technologies Corporation | Dual investment shelled solid mold casting of reticulated metal foams |
US9789534B2 (en) | 2015-01-20 | 2017-10-17 | United Technologies Corporation | Investment technique for solid mold casting of reticulated metal foams |
US9789536B2 (en) | 2015-01-20 | 2017-10-17 | United Technologies Corporation | Dual investment technique for solid mold casting of reticulated metal foams |
US10215056B2 (en) | 2015-06-30 | 2019-02-26 | Rolls-Royce Corporation | Turbine shroud with movable attachment features |
US9884363B2 (en) | 2015-06-30 | 2018-02-06 | United Technologies Corporation | Variable diameter investment casting mold for casting of reticulated metal foams |
US9731342B2 (en) | 2015-07-07 | 2017-08-15 | United Technologies Corporation | Chill plate for equiax casting solidification control for solid mold casting of reticulated metal foams |
US10830136B2 (en) | 2015-11-19 | 2020-11-10 | General Electric Company | Fan case for use in a turbofan engine, and method of assembling a turbofan engine |
US10260522B2 (en) | 2016-05-19 | 2019-04-16 | Rolls-Royce Corporation | Liner system |
US10487684B2 (en) | 2017-03-31 | 2019-11-26 | The Boeing Company | Gas turbine engine fan blade containment systems |
US10550718B2 (en) | 2017-03-31 | 2020-02-04 | The Boeing Company | Gas turbine engine fan blade containment systems |
GB201805006D0 (en) | 2018-03-28 | 2018-05-09 | Rolls Royce Plc | A containment assembly |
FR3100561B1 (fr) * | 2019-09-10 | 2023-01-20 | Safran Aircraft Engines | Fixation d’une virole acoustique a une enveloppe de carter pour une turbomachine d’aeronef |
EP3885539A1 (en) | 2020-03-26 | 2021-09-29 | Unison Industries LLC | Air turbine starter and method of containing a turbine of an air turbine starter |
Citations (2)
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JPH1089150A (ja) * | 1996-07-03 | 1998-04-07 | United Technol Corp <Utc> | タービンエンジン用閉込め容器 |
JP2003269398A (ja) * | 2002-02-15 | 2003-09-25 | General Electric Co <Ge> | ファンケーシングの吸音処理 |
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US4534698A (en) † | 1983-04-25 | 1985-08-13 | General Electric Company | Blade containment structure |
US4734007A (en) * | 1987-03-03 | 1988-03-29 | Rolls-Royce Plc | Fan casing and fan blade loading/unloading |
US5160248A (en) * | 1991-02-25 | 1992-11-03 | General Electric Company | Fan case liner for a gas turbine engine with improved foreign body impact resistance |
DE4310104C2 (de) | 1993-03-27 | 1997-04-30 | Deutsche Forsch Luft Raumfahrt | Verfahren zur Reduzierung der Schallemission sowie zur Verbesserung der Luftleistung und des Wirkungsgrads bei einer axialen Strömungsmaschine und Strömungsmaschine |
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GB2406615B (en) * | 2003-10-03 | 2005-11-30 | Rolls Royce Plc | A gas turbine engine blade containment assembly |
GB2418957B (en) * | 2003-10-22 | 2006-07-05 | Rolls Royce Plc | A liner for a gas turbine engine casing |
GB2407343B (en) † | 2003-10-22 | 2006-04-19 | Rolls Royce Plc | An acoustic liner for a gas turbine engine casing |
GB0403941D0 (en) * | 2004-02-21 | 2004-03-24 | Rolls Royce Plc | A gas turbine engine blade containment assembly |
GB0408825D0 (en) * | 2004-04-20 | 2004-05-26 | Rolls Royce Plc | A rotor blade containment assembly for a gas turbine engine |
GB2435904B (en) | 2006-03-10 | 2008-08-27 | Rolls Royce Plc | Compressor Casing |
GB0609632D0 (en) * | 2006-05-16 | 2006-06-28 | Rolls Royce Plc | An ice impact panel |
GB0610271D0 (en) * | 2006-05-24 | 2006-07-05 | Rolls Royce Plc | A gas turbine engine casing |
-
2008
- 2008-07-29 GB GBGB0813820.8A patent/GB0813820D0/en not_active Ceased
-
2009
- 2009-06-17 EP EP09251578.2A patent/EP2149679B2/en not_active Not-in-force
- 2009-06-18 US US12/457,691 patent/US8231328B2/en active Active
- 2009-07-29 JP JP2009176047A patent/JP2010031871A/ja not_active Ceased
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
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JPH1089150A (ja) * | 1996-07-03 | 1998-04-07 | United Technol Corp <Utc> | タービンエンジン用閉込め容器 |
JP2003269398A (ja) * | 2002-02-15 | 2003-09-25 | General Electric Co <Ge> | ファンケーシングの吸音処理 |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2012062049A (ja) * | 2010-09-15 | 2012-03-29 | Ge Aviation Systems Ltd | 疎氷性コーティングを施したプロペラブレード |
JP2013155741A (ja) * | 2012-01-31 | 2013-08-15 | United Technologies Corp <Utc> | ターボファンエンジンファンケースカートリッジ、ターボファンエンジンファンケースカートリッジの製造方法、およびターボファンエンジンファンケースカートリッジの製造用固定具 |
US9200531B2 (en) | 2012-01-31 | 2015-12-01 | United Technologies Corporation | Fan case rub system, components, and their manufacture |
US9249681B2 (en) | 2012-01-31 | 2016-02-02 | United Technologies Corporation | Fan case rub system |
US10669936B2 (en) | 2013-03-13 | 2020-06-02 | Raytheon Technologies Corporation | Thermally conforming acoustic liner cartridge for a gas turbine engine |
Also Published As
Publication number | Publication date |
---|---|
EP2149679A2 (en) | 2010-02-03 |
US20100028129A1 (en) | 2010-02-04 |
EP2149679A3 (en) | 2013-10-02 |
US8231328B2 (en) | 2012-07-31 |
GB0813820D0 (en) | 2008-09-03 |
EP2149679B2 (en) | 2022-03-09 |
EP2149679B1 (en) | 2018-06-06 |
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