JP5823087B2 - 複合材格納ケーシング - Google Patents
複合材格納ケーシング Download PDFInfo
- Publication number
- JP5823087B2 JP5823087B2 JP2008313980A JP2008313980A JP5823087B2 JP 5823087 B2 JP5823087 B2 JP 5823087B2 JP 2008313980 A JP2008313980 A JP 2008313980A JP 2008313980 A JP2008313980 A JP 2008313980A JP 5823087 B2 JP5823087 B2 JP 5823087B2
- Authority
- JP
- Japan
- Prior art keywords
- sandwich structure
- fan
- abradable
- casing
- containment casing
- 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
Links
Images
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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
- F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
- F01D11/122—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with erodable or abradable material
-
- 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
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/603—Composites; e.g. fibre-reinforced
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Medicinal Preparation (AREA)
Description
12 ファンアセンブリ
14 コアエンジン
16 ファンケーシング
17 ファンケーシング本体
18 ブレード
19 ファンケーシングの内部
20 ロータディスク
22 高圧圧縮機
24 燃焼器
26 高圧タービン
28 低圧タービン
30 吸気端
32 排気端
33 表面板
34 一体型アブレイダブルシステム
35 一体型アブレイダブルシステムを有するファンケーシング
36 サンドイッチ構造
37 コア層
38 アブレイダブル層
40 マンドレル
42 ポケット
44 材料
46 プリフォーム
48 音響パネル
W 幅
D 深さ
L ファンブレードの軸方向コード長
T ファンケーシングプリフォームの半径方向厚さ
Claims (6)
- 少なくとも1つのファンブレード(18)を含むガスタービンエンジン(10)のファンアセンブリ(12)用の、半径方向厚さ(T)を有する複合材格納ケーシング(16)であって、
内部(19)を有する本体(17)と、
前記格納ケーシング(16)の前記本体(17)の前記内部(19)に一体的に結合されたアブレイダブルシステム(34)と
を含み、
該アブレイダブルシステム(34)が、
第1表面板(33)と少なくとも1つのコア層(37)の周囲に配置された第2表面板(33)とを含むサンドイッチ構造(36)と、
該サンドイッチ構造(36)に塗布された少なくとも1つのアブレイダブル層(38)とからなっており、
前記サンドイッチ構造(36)が、前記本体(17)の対向する端部の間に位置し、前記本体(17)の前記内部(19)から半径方向内側に突出する円周方向ポケットを形成し、
前記サンドイッチ構造(36)が、該ファンブレード(18)の軸方向コード長(L)の約1〜約3倍の幅(W)と、該ファンケーシング(16)の該半径方向厚さ(T)の約1〜約5倍の深さ(D)を有し、
該少なくとも1つのコア層(37)は、セル構造、円柱構造、またはトラス構造のいずれかからなり、該サンドイッチ構造(36)は、半径方向に強く円周方向に弱いものである格納ケーシング(16)。 - 該サンドイッチ構造(36)が、炭素繊維、黒鉛繊維、ガラス繊維、セラミック繊維、アラミドポリマー繊維、およびそれらの組み合わせからなるグループから選択される材料からなる、請求項1に記載の格納ケーシング(16)。
- 該アブレイダブルシステム(34)が、該ファンアセンブリ(12)の該ファンブレード(18)に隣接して配置される、請求項1又は2に記載の格納ケーシング(16)。
- 該アブレイダブル層(38)が低密度シンタクチックフィルムエポキシからなる、請求項1、2または3のいずれかに記載の格納ケーシング(16)。
- 該サンドイッチ構造(36)が複数のコア層(37)からなる、請求項1、2、3または4のいずれかに記載の格納ケーシング(16)。
- 該アブレイダブルシステム(34)が、約25%の衝突エネルギーを吸収することができる、請求項1、2、3、4または5のいずれかに記載の格納ケーシング(16)。
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/954,878 | 2007-12-12 | ||
US11/954,878 US8061966B2 (en) | 2007-12-12 | 2007-12-12 | Composite containment casings |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2009144712A JP2009144712A (ja) | 2009-07-02 |
JP5823087B2 true JP5823087B2 (ja) | 2015-11-25 |
Family
ID=40266058
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2008313980A Expired - Fee Related JP5823087B2 (ja) | 2007-12-12 | 2008-12-10 | 複合材格納ケーシング |
Country Status (4)
Country | Link |
---|---|
US (1) | US8061966B2 (ja) |
EP (1) | EP2071132A3 (ja) |
JP (1) | JP5823087B2 (ja) |
CA (1) | CA2645375C (ja) |
Families Citing this family (32)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8333558B2 (en) * | 2008-03-05 | 2012-12-18 | General Electric Company | Containment cases and method of manufacture |
US8545167B2 (en) * | 2009-08-26 | 2013-10-01 | Pratt & Whitney Canada Corp. | Composite casing for rotating blades |
GB0917149D0 (en) * | 2009-10-01 | 2009-11-11 | Rolls Royce Plc | Impactor containment |
US8586179B1 (en) * | 2010-04-09 | 2013-11-19 | The Boeing Company | Mechanical attachment for micro-truss actively cooled structural insulation layer |
US9482114B2 (en) * | 2010-05-31 | 2016-11-01 | Craig Rookstool | Compressor case lining |
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 |
US9840936B2 (en) * | 2012-02-16 | 2017-12-12 | United Technologies Corporation | Case with ballistic liner |
US9555871B2 (en) * | 2012-03-05 | 2017-01-31 | The Boeing Company | Two-surface sandwich structure for accommodating in-plane expansion of one of the surfaces relative to the opposing surface |
US20140003923A1 (en) | 2012-07-02 | 2014-01-02 | Peter Finnigan | Functionally graded composite fan containment case |
US20140119904A1 (en) * | 2012-11-01 | 2014-05-01 | United Technologies Corporation | In-situ pressure enhanced processing of composite articles |
US10669936B2 (en) | 2013-03-13 | 2020-06-02 | Raytheon Technologies Corporation | Thermally conforming acoustic liner cartridge for a gas turbine engine |
FR3005990B1 (fr) * | 2013-05-23 | 2017-09-01 | Snecma | Procede de raidissement d'un composant d'une turbine a turbomachine |
FR3007064B1 (fr) * | 2013-06-13 | 2018-06-29 | Composite Industrie | Secteur de joint annulaire abradable pour turbomachine et procede de fabrication d'une telle piece |
FR3007063B1 (fr) | 2013-06-13 | 2015-07-03 | Composite Ind | Piece de materiau abradable pour la fabrication d'un secteur de joint annulaire abradable pour turbomachine et procede de fabrication d'une telle piece |
EP2940251B1 (en) | 2014-04-28 | 2019-06-12 | Rolls-Royce Corporation | Fan containment case |
US9915168B2 (en) * | 2014-06-03 | 2018-03-13 | United Technologies Corporation | Flowpath cartridge liner and gas turbine engine including same |
US10113559B2 (en) * | 2014-10-14 | 2018-10-30 | United Technologies Corporation | Gas turbine engine impact liner |
US10125788B2 (en) | 2016-01-08 | 2018-11-13 | General Electric Company | Ceramic tile fan blade containment |
US10907651B2 (en) | 2016-01-12 | 2021-02-02 | Rolls-Royce Corporation | Fan track liner subassembly angled upturn joint |
US10519965B2 (en) * | 2016-01-15 | 2019-12-31 | General Electric Company | Method and system for fiber reinforced composite panels |
US10697470B2 (en) * | 2016-02-15 | 2020-06-30 | General Electric Company | Containment case trench filler layer and method of containing releasable components from rotatable machines |
CN107829980B (zh) * | 2016-09-16 | 2021-05-25 | 通用电气公司 | 沿周向变化厚度的复合风扇壳 |
FR3060438B1 (fr) * | 2016-12-15 | 2021-01-29 | Safran Aircraft Engines | Procede et outillage de mise en forme d'un carter de soufflante |
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 |
US11391297B2 (en) | 2017-11-09 | 2022-07-19 | Pratt & Whitney Canada Corp. | Composite fan case with nanoparticles |
FR3074088B1 (fr) * | 2017-11-30 | 2021-02-12 | Safran Aircraft Engines | Carter en materiau composite renforce et son procede de fabrication |
US20210246807A1 (en) * | 2020-02-11 | 2021-08-12 | Pratt & Whitney Canada Corp. | Fan case for gas turbine engine and associated method of use |
JP2021167577A (ja) * | 2020-04-09 | 2021-10-21 | 三菱重工業株式会社 | 回転機械のハウジング構造体、及び、回転機械のハウジング構造体の製造方法 |
US11549391B2 (en) * | 2021-03-22 | 2023-01-10 | General Electric Company | Component formed from hybrid material |
US20230193827A1 (en) * | 2021-12-21 | 2023-06-22 | Rolls-Royce Deutschland Ltd & Co Kg | Fan case assembly for a gas turbine engine |
Family Cites Families (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4149824A (en) * | 1976-12-23 | 1979-04-17 | General Electric Company | Blade containment device |
US4500252A (en) * | 1981-12-21 | 1985-02-19 | United Technologies Corporation | Beam for a containment structure |
US4452565A (en) * | 1981-12-21 | 1984-06-05 | United Technologies Corporation | Containment structure |
US4598449A (en) * | 1981-12-21 | 1986-07-08 | United Technologies Corporation | Beam for a containment structure |
US4534698A (en) * | 1983-04-25 | 1985-08-13 | General Electric Company | Blade containment structure |
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 |
GB9307288D0 (en) * | 1993-04-07 | 1993-06-02 | Rolls Royce Plc | Gas turbine engine casing construction |
WO1995003170A1 (en) | 1993-05-04 | 1995-02-02 | Foster-Miller, Inc. | Truss reinforced foam core sandwich structure |
US5344280A (en) * | 1993-05-05 | 1994-09-06 | General Electric Company | Impact resistant fan case liner |
US5451448A (en) | 1993-07-01 | 1995-09-19 | The United States Of America As Represented By The United States National Aeronautics And Space Administration | Flexible ceramic thermal protection system resistant to high aeroacoustic noise comprising a three-dimensional woven-fiber structure having a multilayer top fabric layer, a bottom fabric layer and an intermediate rib fabric layer |
US5486086A (en) | 1994-01-04 | 1996-01-23 | General Electric Company | Blade containment system |
US5431532A (en) | 1994-05-20 | 1995-07-11 | General Electric Company | Blade containment system |
US6059524A (en) | 1998-04-20 | 2000-05-09 | United Technologies Corporation | Penetration resistant fan casing for a turbine engine |
US6290455B1 (en) * | 1999-12-03 | 2001-09-18 | General Electric Company | Contoured hardwall containment |
DK1265744T3 (en) | 1999-12-28 | 2016-03-29 | Milliken & Co | Fibre reinforced composite cores |
US6742547B2 (en) | 2000-09-20 | 2004-06-01 | Bally Ribbon Mills | Three-dimensional woven forms with integral bias fibers and bias weaving loom |
US6814541B2 (en) | 2002-10-07 | 2004-11-09 | General Electric Company | Jet aircraft fan case containment design |
GB0300999D0 (en) | 2003-01-16 | 2003-02-19 | Rolls Royce Plc | A gas turbine engine blade containment assembly |
WO2005018926A2 (en) | 2003-03-28 | 2005-03-03 | Webcore Technologies, Inc. | Fiber reinforced composite cores and panels |
GB0408825D0 (en) * | 2004-04-20 | 2004-05-26 | Rolls Royce Plc | A rotor blade containment assembly for a gas turbine engine |
US7335012B2 (en) | 2004-12-22 | 2008-02-26 | General Electric Company | Apparatus for fabricating reinforced composite materials |
US7246990B2 (en) * | 2004-12-23 | 2007-07-24 | General Electric Company | Composite fan containment case for turbine engines |
GB2426287B (en) | 2005-05-18 | 2007-05-30 | Rolls Royce Plc | Blade containment structure |
-
2007
- 2007-12-12 US US11/954,878 patent/US8061966B2/en active Active
-
2008
- 2008-11-27 CA CA2645375A patent/CA2645375C/en not_active Expired - Fee Related
- 2008-12-03 EP EP08170597.2A patent/EP2071132A3/en not_active Withdrawn
- 2008-12-10 JP JP2008313980A patent/JP5823087B2/ja not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
EP2071132A3 (en) | 2015-03-11 |
CA2645375C (en) | 2016-07-05 |
US20090155065A1 (en) | 2009-06-18 |
JP2009144712A (ja) | 2009-07-02 |
US8061966B2 (en) | 2011-11-22 |
CA2645375A1 (en) | 2009-06-12 |
EP2071132A2 (en) | 2009-06-17 |
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