JP4883834B2 - 後縁ブロックが冷却されるセラミックタービン翼形部 - Google Patents
後縁ブロックが冷却されるセラミックタービン翼形部 Download PDFInfo
- Publication number
- JP4883834B2 JP4883834B2 JP2000381168A JP2000381168A JP4883834B2 JP 4883834 B2 JP4883834 B2 JP 4883834B2 JP 2000381168 A JP2000381168 A JP 2000381168A JP 2000381168 A JP2000381168 A JP 2000381168A JP 4883834 B2 JP4883834 B2 JP 4883834B2
- Authority
- JP
- Japan
- Prior art keywords
- trailing edge
- airfoil
- cooling air
- block
- edge block
- 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 - Lifetime
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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/187—Convection cooling
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/186—Film cooling
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/187—Convection cooling
- F01D5/188—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall
- F01D5/189—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall the insert having a tubular cross-section, e.g. airfoil shape
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/284—Selection of ceramic materials
-
- 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
- F05D2250/30—Arrangement of components
- F05D2250/32—Arrangement of components according to their shape
- F05D2250/323—Arrangement of components according to their shape convergent
-
- 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
- F05D2300/20—Oxide or non-oxide ceramics
- F05D2300/22—Non-oxide ceramics
- F05D2300/226—Carbides
- F05D2300/2261—Carbides of silicon
-
- 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)
- Chemical & Material Sciences (AREA)
- Ceramic Engineering (AREA)
- Materials Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Ceramic Products (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US09/507,407 US6325593B1 (en) | 2000-02-18 | 2000-02-18 | Ceramic turbine airfoils with cooled trailing edge blocks |
| US09/507407 | 2000-02-18 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2001227302A JP2001227302A (ja) | 2001-08-24 |
| JP2001227302A5 JP2001227302A5 (https=) | 2008-02-07 |
| JP4883834B2 true JP4883834B2 (ja) | 2012-02-22 |
Family
ID=24018525
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2000381168A Expired - Lifetime JP4883834B2 (ja) | 2000-02-18 | 2000-12-15 | 後縁ブロックが冷却されるセラミックタービン翼形部 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US6325593B1 (https=) |
| EP (1) | EP1126135B1 (https=) |
| JP (1) | JP4883834B2 (https=) |
| DE (1) | DE60028529T2 (https=) |
Families Citing this family (124)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6543993B2 (en) * | 2000-12-28 | 2003-04-08 | General Electric Company | Apparatus and methods for localized cooling of gas turbine nozzle walls |
| US6398489B1 (en) * | 2001-02-08 | 2002-06-04 | General Electric Company | Airfoil shape for a turbine nozzle |
| GB0127902D0 (en) | 2001-11-21 | 2002-01-16 | Rolls Royce Plc | Gas turbine engine aerofoil |
| US6648597B1 (en) | 2002-05-31 | 2003-11-18 | Siemens Westinghouse Power Corporation | Ceramic matrix composite turbine vane |
| US6709230B2 (en) | 2002-05-31 | 2004-03-23 | Siemens Westinghouse Power Corporation | Ceramic matrix composite gas turbine vane |
| US9068464B2 (en) * | 2002-09-17 | 2015-06-30 | Siemens Energy, Inc. | Method of joining ceramic parts and articles so formed |
| US7093359B2 (en) | 2002-09-17 | 2006-08-22 | Siemens Westinghouse Power Corporation | Composite structure formed by CMC-on-insulation process |
| US6808363B2 (en) * | 2002-12-20 | 2004-10-26 | General Electric Company | Shroud segment and assembly with circumferential seal at a planar segment surface |
| US6893214B2 (en) * | 2002-12-20 | 2005-05-17 | General Electric Company | Shroud segment and assembly with surface recessed seal bridging adjacent members |
| US6884030B2 (en) | 2002-12-20 | 2005-04-26 | General Electric Company | Methods and apparatus for securing multi-piece nozzle assemblies |
| US7311790B2 (en) * | 2003-04-25 | 2007-12-25 | Siemens Power Generation, Inc. | Hybrid structure using ceramic tiles and method of manufacture |
| US20050158171A1 (en) * | 2004-01-15 | 2005-07-21 | General Electric Company | Hybrid ceramic matrix composite turbine blades for improved processibility and performance |
| US7351364B2 (en) * | 2004-01-29 | 2008-04-01 | Siemens Power Generation, Inc. | Method of manufacturing a hybrid structure |
| US7086829B2 (en) * | 2004-02-03 | 2006-08-08 | General Electric Company | Film cooling for the trailing edge of a steam cooled nozzle |
| US7066717B2 (en) * | 2004-04-22 | 2006-06-27 | Siemens Power Generation, Inc. | Ceramic matrix composite airfoil trailing edge arrangement |
| GB2417295B (en) * | 2004-08-21 | 2006-10-25 | Rolls Royce Plc | A component having a cooling arrangement |
| US7217096B2 (en) * | 2004-12-13 | 2007-05-15 | General Electric Company | Fillet energized turbine stage |
| US7435058B2 (en) * | 2005-01-18 | 2008-10-14 | Siemens Power Generation, Inc. | Ceramic matrix composite vane with chordwise stiffener |
| US8137611B2 (en) * | 2005-03-17 | 2012-03-20 | Siemens Energy, Inc. | Processing method for solid core ceramic matrix composite airfoil |
| US7452182B2 (en) * | 2005-04-07 | 2008-11-18 | Siemens Energy, Inc. | Multi-piece turbine vane assembly |
| US7316539B2 (en) * | 2005-04-07 | 2008-01-08 | Siemens Power Generation, Inc. | Vane assembly with metal trailing edge segment |
| US7393183B2 (en) * | 2005-06-17 | 2008-07-01 | Siemens Power Generation, Inc. | Trailing edge attachment for composite airfoil |
| US7563071B2 (en) * | 2005-08-04 | 2009-07-21 | Siemens Energy, Inc. | Pin-loaded mounting apparatus for a refractory component in a combustion turbine engine |
| US7730727B2 (en) | 2005-09-06 | 2010-06-08 | American Air Liquide, Inc. | Flexible flow control device for cogeneration ducting applications |
| JP4147239B2 (ja) * | 2005-11-17 | 2008-09-10 | 川崎重工業株式会社 | ダブルジェット式フィルム冷却構造 |
| US7976274B2 (en) * | 2005-12-08 | 2011-07-12 | General Electric Company | Methods and apparatus for assembling turbine engines |
| US7371043B2 (en) * | 2006-01-12 | 2008-05-13 | Siemens Power Generation, Inc. | CMC turbine shroud ring segment and fabrication method |
| US7600978B2 (en) * | 2006-07-27 | 2009-10-13 | Siemens Energy, Inc. | Hollow CMC airfoil with internal stitch |
| US20100034662A1 (en) * | 2006-12-26 | 2010-02-11 | General Electric Company | Cooled airfoil and method for making an airfoil having reduced trail edge slot flow |
| US7722317B2 (en) * | 2007-01-25 | 2010-05-25 | Siemens Energy, Inc. | CMC to metal attachment mechanism |
| JP5474279B2 (ja) * | 2007-03-06 | 2014-04-16 | 株式会社Ihi | 冷却タービン翼 |
| US20090014926A1 (en) * | 2007-07-09 | 2009-01-15 | Siemens Power Generation, Inc. | Method of constructing a hollow fiber reinforced structure |
| US7967570B2 (en) * | 2007-07-27 | 2011-06-28 | United Technologies Corporation | Low transient thermal stress turbine engine components |
| WO2009048357A1 (en) * | 2007-10-11 | 2009-04-16 | Volvo Aero Corporation | A method for producing a vane, such a vane and a stator component comprising the vane |
| JP4577662B2 (ja) * | 2007-10-11 | 2010-11-10 | 株式会社Ihi | タービン翼 |
| US7934906B2 (en) * | 2007-11-14 | 2011-05-03 | Siemens Energy, Inc. | Turbine blade tip cooling system |
| US8096770B2 (en) * | 2008-09-25 | 2012-01-17 | Siemens Energy, Inc. | Trailing edge cooling for turbine blade airfoil |
| US8382436B2 (en) | 2009-01-06 | 2013-02-26 | General Electric Company | Non-integral turbine blade platforms and systems |
| US8262345B2 (en) * | 2009-02-06 | 2012-09-11 | General Electric Company | Ceramic matrix composite turbine engine |
| FR2946552B1 (fr) * | 2009-06-10 | 2012-06-01 | Snecma | Procede pour l'usinage par outil pcd d'aubes de turbine en cmc. |
| US9422816B2 (en) * | 2009-06-26 | 2016-08-23 | United Technologies Corporation | Airfoil with hybrid drilled and cutback trailing edge |
| US8206096B2 (en) * | 2009-07-08 | 2012-06-26 | General Electric Company | Composite turbine nozzle |
| US8256088B2 (en) * | 2009-08-24 | 2012-09-04 | Siemens Energy, Inc. | Joining mechanism with stem tension and interlocked compression ring |
| JP5709879B2 (ja) * | 2009-10-20 | 2015-04-30 | シーメンス エナジー インコーポレイテッド | ガスタービンエンジン |
| US8894363B2 (en) | 2011-02-09 | 2014-11-25 | Siemens Energy, Inc. | Cooling module design and method for cooling components of a gas turbine system |
| US8632297B2 (en) | 2010-09-29 | 2014-01-21 | General Electric Company | Turbine airfoil and method for cooling a turbine airfoil |
| US8790067B2 (en) | 2011-04-27 | 2014-07-29 | United Technologies Corporation | Blade clearance control using high-CTE and low-CTE ring members |
| US9011085B2 (en) * | 2011-05-26 | 2015-04-21 | United Technologies Corporation | Ceramic matrix composite continuous “I”-shaped fiber geometry airfoil for a gas turbine engine |
| US8739547B2 (en) | 2011-06-23 | 2014-06-03 | United Technologies Corporation | Gas turbine engine joint having a metallic member, a CMC member, and a ceramic key |
| US8864492B2 (en) | 2011-06-23 | 2014-10-21 | United Technologies Corporation | Reverse flow combustor duct attachment |
| US9335051B2 (en) | 2011-07-13 | 2016-05-10 | United Technologies Corporation | Ceramic matrix composite combustor vane ring assembly |
| US8920127B2 (en) | 2011-07-18 | 2014-12-30 | United Technologies Corporation | Turbine rotor non-metallic blade attachment |
| US8834109B2 (en) * | 2011-08-03 | 2014-09-16 | United Technologies Corporation | Vane assembly for a gas turbine engine |
| US8882448B2 (en) | 2011-09-09 | 2014-11-11 | Siemens Aktiengesellshaft | Cooling system in a turbine airfoil assembly including zigzag cooling passages interconnected with radial passageways |
| US8840363B2 (en) | 2011-09-09 | 2014-09-23 | Siemens Energy, Inc. | Trailing edge cooling system in a turbine airfoil assembly |
| JP5536001B2 (ja) * | 2011-09-20 | 2014-07-02 | 株式会社日立製作所 | ガスタービン翼フィルム冷却孔の設定方法及びガスタービン翼 |
| US9127560B2 (en) | 2011-12-01 | 2015-09-08 | General Electric Company | Cooled turbine blade and method for cooling a turbine blade |
| US8967974B2 (en) | 2012-01-03 | 2015-03-03 | General Electric Company | Composite airfoil assembly |
| US9051842B2 (en) * | 2012-01-05 | 2015-06-09 | General Electric Company | System and method for cooling turbine blades |
| US9587492B2 (en) | 2012-05-04 | 2017-03-07 | General Electric Company | Turbomachine component having an internal cavity reactivity neutralizer and method of forming the same |
| US9109453B2 (en) * | 2012-07-02 | 2015-08-18 | United Technologies Corporation | Airfoil cooling arrangement |
| US9670790B2 (en) | 2012-09-28 | 2017-06-06 | United Technologies Corporation | Turbine vane with mistake reduction feature |
| JP6038620B2 (ja) * | 2012-12-05 | 2016-12-07 | 三菱日立パワーシステムズ株式会社 | ガスタービン冷却翼およびガスタービン冷却翼の補修方法 |
| US9790801B2 (en) * | 2012-12-27 | 2017-10-17 | United Technologies Corporation | Gas turbine engine component having suction side cutback opening |
| US20140208771A1 (en) * | 2012-12-28 | 2014-07-31 | United Technologies Corporation | Gas turbine engine component cooling arrangement |
| US8985949B2 (en) | 2013-04-29 | 2015-03-24 | Siemens Aktiengesellschaft | Cooling system including wavy cooling chamber in a trailing edge portion of an airfoil assembly |
| WO2015012918A2 (en) | 2013-06-04 | 2015-01-29 | United Technologies Corporation | Gas turbine engine airfoil trailing edge suction side cooling |
| EP3030752A1 (en) * | 2013-08-06 | 2016-06-15 | General Electric Company | Mounting apparatus for low-ductility turbine nozzle |
| US20150184518A1 (en) * | 2013-12-26 | 2015-07-02 | Ching-Pang Lee | Turbine airfoil cooling system with nonlinear trailing edge exit slots |
| EP2921649B1 (en) * | 2014-03-19 | 2021-04-28 | Ansaldo Energia IP UK Limited | Airfoil portion of a rotor blade or guide vane of a turbo-machine |
| EP3023696B1 (en) * | 2014-11-20 | 2019-08-28 | Ansaldo Energia Switzerland AG | Lobe lance for a gas turbine combustor |
| US9810084B1 (en) * | 2015-02-06 | 2017-11-07 | United Technologies Corporation | Gas turbine engine turbine vane baffle and serpentine cooling passage |
| CN104895618B (zh) * | 2015-04-10 | 2017-02-01 | 中国科学院工程热物理研究所 | 超高负荷低压涡轮叶片、高负荷低压涡轮、航空燃气涡轮发动机 |
| US9797263B2 (en) | 2015-05-26 | 2017-10-24 | Rolls-Royce Corporation | Monolithic ceramic rods to enable cooling holes in CMC |
| US10024175B2 (en) | 2015-05-26 | 2018-07-17 | Rolls-Royce Corporation | Cooling holes manufactured with EBC in place |
| US9702551B2 (en) * | 2015-06-11 | 2017-07-11 | Haier Us Appliance Solutions, Inc. | Gas burner |
| DE102015213090A1 (de) * | 2015-07-13 | 2017-01-19 | Siemens Aktiengesellschaft | Schaufel für eine Strömungskraftmaschine und Verfahren zu deren Herstellung |
| US11230935B2 (en) | 2015-09-18 | 2022-01-25 | General Electric Company | Stator component cooling |
| US20170089579A1 (en) * | 2015-09-30 | 2017-03-30 | General Electric Company | Cmc articles having small complex features for advanced film cooling |
| US10563867B2 (en) * | 2015-09-30 | 2020-02-18 | General Electric Company | CMC articles having small complex features for advanced film cooling |
| US10344598B2 (en) | 2015-12-03 | 2019-07-09 | General Electric Company | Trailing edge cooling for a turbine blade |
| US20170176012A1 (en) * | 2015-12-22 | 2017-06-22 | General Electric Company | Fuel injectors and staged fuel injection systems in gas turbines |
| US10408073B2 (en) | 2016-01-20 | 2019-09-10 | General Electric Company | Cooled CMC wall contouring |
| US10309254B2 (en) * | 2016-02-26 | 2019-06-04 | General Electric Company | Nozzle segment for a gas turbine engine with ribs defining radially spaced internal cooling channels |
| JP6681749B2 (ja) * | 2016-03-03 | 2020-04-15 | 三菱航空機株式会社 | 高温空気の機体張り付き対策構造および航空機 |
| US10519779B2 (en) * | 2016-03-16 | 2019-12-31 | General Electric Company | Radial CMC wall thickness variation for stress response |
| US10415397B2 (en) * | 2016-05-11 | 2019-09-17 | General Electric Company | Ceramic matrix composite airfoil cooling |
| US10494930B2 (en) | 2016-06-16 | 2019-12-03 | General Electric Company | Ceramic matrix composite component cooling |
| US10443401B2 (en) * | 2016-09-02 | 2019-10-15 | United Technologies Corporation | Cooled turbine vane with alternately orientated film cooling hole rows |
| US10539026B2 (en) * | 2017-09-21 | 2020-01-21 | United Technologies Corporation | Gas turbine engine component with cooling holes having variable roughness |
| US10570751B2 (en) | 2017-11-22 | 2020-02-25 | General Electric Company | Turbine engine airfoil assembly |
| US11008888B2 (en) | 2018-07-17 | 2021-05-18 | Rolls-Royce Corporation | Turbine vane assembly with ceramic matrix composite components |
| US10830063B2 (en) | 2018-07-20 | 2020-11-10 | Rolls-Royce North American Technologies Inc. | Turbine vane assembly with ceramic matrix composite components |
| US10605103B2 (en) | 2018-08-24 | 2020-03-31 | Rolls-Royce Corporation | CMC airfoil assembly |
| US10927689B2 (en) * | 2018-08-31 | 2021-02-23 | Rolls-Royce Corporation | Turbine vane assembly with ceramic matrix composite components mounted to case |
| US10767497B2 (en) | 2018-09-07 | 2020-09-08 | Rolls-Royce Corporation | Turbine vane assembly with ceramic matrix composite components |
| US11149567B2 (en) | 2018-09-17 | 2021-10-19 | Rolls-Royce Corporation | Ceramic matrix composite load transfer roller joint |
| US10890077B2 (en) | 2018-09-26 | 2021-01-12 | Rolls-Royce Corporation | Anti-fret liner |
| US10859268B2 (en) | 2018-10-03 | 2020-12-08 | Rolls-Royce Plc | Ceramic matrix composite turbine vanes and vane ring assemblies |
| US11149568B2 (en) | 2018-12-20 | 2021-10-19 | Rolls-Royce Plc | Sliding ceramic matrix composite vane assembly for gas turbine engines |
| US10961857B2 (en) | 2018-12-21 | 2021-03-30 | Rolls-Royce Plc | Turbine section of a gas turbine engine with ceramic matrix composite vanes |
| US11047247B2 (en) | 2018-12-21 | 2021-06-29 | Rolls-Royce Plc | Turbine section of a gas turbine engine with ceramic matrix composite vanes |
| US10883376B2 (en) | 2019-02-01 | 2021-01-05 | Rolls-Royce Plc | Turbine vane assembly with ceramic matrix composite vanes |
| US10767493B2 (en) | 2019-02-01 | 2020-09-08 | Rolls-Royce Plc | Turbine vane assembly with ceramic matrix composite vanes |
| US11008880B2 (en) | 2019-04-23 | 2021-05-18 | Rolls-Royce Plc | Turbine section assembly with ceramic matrix composite vane |
| US11193393B2 (en) | 2019-04-23 | 2021-12-07 | Rolls-Royce Plc | Turbine section assembly with ceramic matrix composite vane |
| US10975708B2 (en) | 2019-04-23 | 2021-04-13 | Rolls-Royce Plc | Turbine section assembly with ceramic matrix composite vane |
| US10954802B2 (en) | 2019-04-23 | 2021-03-23 | Rolls-Royce Plc | Turbine section assembly with ceramic matrix composite vane |
| US11149559B2 (en) | 2019-05-13 | 2021-10-19 | Rolls-Royce Plc | Turbine section assembly with ceramic matrix composite vane |
| US11193381B2 (en) | 2019-05-17 | 2021-12-07 | Rolls-Royce Plc | Turbine vane assembly having ceramic matrix composite components with sliding support |
| US10890076B1 (en) | 2019-06-28 | 2021-01-12 | Rolls-Royce Plc | Turbine vane assembly having ceramic matrix composite components with expandable spar support |
| US11162432B2 (en) * | 2019-09-19 | 2021-11-02 | General Electric Company | Integrated nozzle and diaphragm with optimized internal vane thickness |
| US20210108517A1 (en) * | 2019-10-15 | 2021-04-15 | United Technologies Corporation | Cmc airfoil with cooling holes |
| JP6745012B1 (ja) * | 2019-10-31 | 2020-08-26 | 三菱日立パワーシステムズ株式会社 | タービン翼及びこれを備えたガスタービン |
| US11473444B2 (en) * | 2019-11-08 | 2022-10-18 | Raytheon Technologies Corporation | Ceramic airfoil with cooling air turn |
| US11242760B2 (en) * | 2020-01-22 | 2022-02-08 | General Electric Company | Turbine rotor blade with integral impingement sleeve by additive manufacture |
| US11319822B2 (en) | 2020-05-06 | 2022-05-03 | Rolls-Royce North American Technologies Inc. | Hybrid vane segment with ceramic matrix composite airfoils |
| US11879360B2 (en) * | 2020-10-30 | 2024-01-23 | General Electric Company | Fabricated CMC nozzle assemblies for gas turbine engines |
| US11603765B1 (en) * | 2021-07-16 | 2023-03-14 | Raytheon Technologies Corporation | Airfoil assembly with fiber-reinforced composite rings and toothed exit slot |
| US11560799B1 (en) | 2021-10-22 | 2023-01-24 | Rolls-Royce High Temperature Composites Inc. | Ceramic matrix composite vane assembly with shaped load transfer features |
| US11732596B2 (en) | 2021-12-22 | 2023-08-22 | Rolls-Royce Plc | Ceramic matrix composite turbine vane assembly having minimalistic support spars |
| CN118339363A (zh) | 2021-12-28 | 2024-07-12 | 三菱重工业株式会社 | 转动叶片及具备该转动叶片的燃气涡轮 |
| US11713679B1 (en) * | 2022-01-27 | 2023-08-01 | Raytheon Technologies Corporation | Tangentially bowed airfoil |
| DE102024206063A1 (de) | 2024-06-28 | 2025-12-31 | Rolls-Royce Deutschland Ltd & Co Kg | Turbinenschaufel, insbesondere für ein Gasturbinentriebwerk |
Family Cites Families (26)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3515499A (en) * | 1968-04-22 | 1970-06-02 | Aerojet General Co | Blades and blade assemblies for turbine engines,compressors and the like |
| US3819295A (en) | 1972-09-21 | 1974-06-25 | Gen Electric | Cooling slot for airfoil blade |
| GB1560683A (en) * | 1972-11-28 | 1980-02-06 | Rolls Royce | Turbine blade |
| US4006999A (en) | 1975-07-17 | 1977-02-08 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Leading edge protection for composite blades |
| US4203706A (en) * | 1977-12-28 | 1980-05-20 | United Technologies Corporation | Radial wafer airfoil construction |
| US4324843A (en) * | 1980-02-13 | 1982-04-13 | United Technologies Corporation | Continuous length silicon carbide fiber reinforced ceramic composites |
| GB2097479B (en) | 1981-04-24 | 1984-09-05 | Rolls Royce | Cooled vane for a gas turbine engine |
| JPS60187701A (ja) * | 1984-03-06 | 1985-09-25 | Toshiba Corp | ガスタ−ビン冷却翼 |
| US4705455A (en) | 1985-12-23 | 1987-11-10 | United Technologies Corporation | Convergent-divergent film coolant passage |
| GB2189553B (en) | 1986-04-25 | 1990-05-23 | Rolls Royce | Cooled vane |
| US5102299A (en) | 1986-11-10 | 1992-04-07 | The United States Of America As Represented By The Secretary Of The Air Force | Airfoil trailing edge cooling configuration |
| US5720431A (en) | 1988-08-24 | 1998-02-24 | United Technologies Corporation | Cooled blades for a gas turbine engine |
| US5667359A (en) * | 1988-08-24 | 1997-09-16 | United Technologies Corp. | Clearance control for the turbine of a gas turbine engine |
| US5326224A (en) * | 1991-03-01 | 1994-07-05 | General Electric Company | Cooling hole arrangements in jet engine components exposed to hot gas flow |
| US6129515A (en) * | 1992-11-20 | 2000-10-10 | United Technologies Corporation | Turbine airfoil suction aided film cooling means |
| US5288207A (en) | 1992-11-24 | 1994-02-22 | United Technologies Corporation | Internally cooled turbine airfoil |
| US5271715A (en) * | 1992-12-21 | 1993-12-21 | United Technologies Corporation | Cooled turbine blade |
| US5355668A (en) | 1993-01-29 | 1994-10-18 | General Electric Company | Catalyst-bearing component of gas turbine engine |
| JPH07223876A (ja) * | 1993-06-25 | 1995-08-22 | Hitachi Ltd | 繊維強化複合材とその製法およびそれを用いた部材 |
| US5516260A (en) | 1994-10-07 | 1996-05-14 | General Electric Company | Bonded turbine airfuel with floating wall cooling insert |
| US5630700A (en) | 1996-04-26 | 1997-05-20 | General Electric Company | Floating vane turbine nozzle |
| US5931638A (en) * | 1997-08-07 | 1999-08-03 | United Technologies Corporation | Turbomachinery airfoil with optimized heat transfer |
| US6077036A (en) * | 1998-08-20 | 2000-06-20 | General Electric Company | Bowed nozzle vane with selective TBC |
| US6126397A (en) * | 1998-12-22 | 2000-10-03 | United Technologies Corporation | Trailing edge cooling apparatus for a gas turbine airfoil |
| US6102658A (en) * | 1998-12-22 | 2000-08-15 | United Technologies Corporation | Trailing edge cooling apparatus for a gas turbine airfoil |
| US6422819B1 (en) * | 1999-12-09 | 2002-07-23 | General Electric Company | Cooled airfoil for gas turbine engine and method of making the same |
-
2000
- 2000-02-18 US US09/507,407 patent/US6325593B1/en not_active Expired - Lifetime
- 2000-12-15 JP JP2000381168A patent/JP4883834B2/ja not_active Expired - Lifetime
- 2000-12-15 DE DE60028529T patent/DE60028529T2/de not_active Expired - Lifetime
- 2000-12-15 EP EP00311265A patent/EP1126135B1/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| EP1126135A3 (en) | 2003-01-08 |
| US6325593B1 (en) | 2001-12-04 |
| DE60028529T2 (de) | 2006-12-28 |
| EP1126135A2 (en) | 2001-08-22 |
| DE60028529D1 (de) | 2006-07-20 |
| EP1126135B1 (en) | 2006-06-07 |
| JP2001227302A (ja) | 2001-08-24 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP4883834B2 (ja) | 後縁ブロックが冷却されるセラミックタービン翼形部 | |
| US6609884B2 (en) | Cooling of gas turbine engine aerofoils | |
| US7632062B2 (en) | Turbine rotor blades | |
| US6322322B1 (en) | High temperature airfoil | |
| EP1118747B1 (en) | An aerofoil for an axial flow turbomachine | |
| US10822973B2 (en) | Shroud for a gas turbine engine | |
| JP4052380B2 (ja) | 接線方向流バッフルおよび該バッフルを配置したタービンノズル | |
| US8197211B1 (en) | Composite air cooled turbine rotor blade | |
| CN110821572B (zh) | 包含端壁挡板的涡轮 | |
| JPH10274002A (ja) | ガスタービンエンジンの動翼の冷却通路の乱流器構造 | |
| JP2017072128A (ja) | ステータ部品 | |
| US20190085705A1 (en) | Component for a turbine engine with a film-hole | |
| US20250146418A1 (en) | Turbine incorporating splitters | |
| JP2003120204A (ja) | ガスタービンエンジン用のタービン翼形部 | |
| US8297925B2 (en) | Aerofoil configuration | |
| JP2017020493A (ja) | タービンバンドのアンチコーディングフランジ | |
| JP2001200704A (ja) | ガスタービン・エンジンの冷却された翼形部及びその製造方法 | |
| CN102678187A (zh) | 用于燃气涡轮发动机的涡轮机轮叶及其制造方法 | |
| CN114135342A (zh) | 具有带有复合物和金属部分的根部区段的燃气涡轮发动机转子叶片 | |
| US10724380B2 (en) | CMC blade with internal support | |
| US6544001B2 (en) | Gas turbine engine system | |
| CN114060099B (zh) | 用于燃气涡轮发动机的涡轮区段的转子组件 | |
| US11220921B2 (en) | Vane assembly | |
| JP2006046343A (ja) | タービン動翼のフレア・バットレス |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20071213 |
|
| A621 | Written request for application examination |
Free format text: JAPANESE INTERMEDIATE CODE: A621 Effective date: 20071213 |
|
| RD02 | Notification of acceptance of power of attorney |
Free format text: JAPANESE INTERMEDIATE CODE: A7422 Effective date: 20100201 |
|
| RD04 | Notification of resignation of power of attorney |
Free format text: JAPANESE INTERMEDIATE CODE: A7424 Effective date: 20100201 |
|
| A131 | Notification of reasons for refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A131 Effective date: 20100323 |
|
| A601 | Written request for extension of time |
Free format text: JAPANESE INTERMEDIATE CODE: A601 Effective date: 20100622 |
|
| A602 | Written permission of extension of time |
Free format text: JAPANESE INTERMEDIATE CODE: A602 Effective date: 20100625 |
|
| A601 | Written request for extension of time |
Free format text: JAPANESE INTERMEDIATE CODE: A601 Effective date: 20100722 |
|
| A602 | Written permission of extension of time |
Free format text: JAPANESE INTERMEDIATE CODE: A602 Effective date: 20100727 |
|
| A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20100922 |
|
| A131 | Notification of reasons for refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A131 Effective date: 20101207 |
|
| A601 | Written request for extension of time |
Free format text: JAPANESE INTERMEDIATE CODE: A601 Effective date: 20110304 |
|
| A602 | Written permission of extension of time |
Free format text: JAPANESE INTERMEDIATE CODE: A602 Effective date: 20110309 |
|
| A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20110607 |
|
| A131 | Notification of reasons for refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A131 Effective date: 20110726 |
|
| A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20110921 |
|
| TRDD | Decision of grant or rejection written | ||
| A01 | Written decision to grant a patent or to grant a registration (utility model) |
Free format text: JAPANESE INTERMEDIATE CODE: A01 Effective date: 20111108 |
|
| A01 | Written decision to grant a patent or to grant a registration (utility model) |
Free format text: JAPANESE INTERMEDIATE CODE: A01 |
|
| A61 | First payment of annual fees (during grant procedure) |
Free format text: JAPANESE INTERMEDIATE CODE: A61 Effective date: 20111206 |
|
| FPAY | Renewal fee payment (event date is renewal date of database) |
Free format text: PAYMENT UNTIL: 20141216 Year of fee payment: 3 |
|
| R150 | Certificate of patent or registration of utility model |
Free format text: JAPANESE INTERMEDIATE CODE: R150 Ref document number: 4883834 Country of ref document: JP Free format text: JAPANESE INTERMEDIATE CODE: R150 |
|
| R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
| R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
| R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
| R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
| R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
| R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
| EXPY | Cancellation because of completion of term |