JP3989576B2 - ガスタービン用の部分的に金属製の翼 - Google Patents
ガスタービン用の部分的に金属製の翼 Download PDFInfo
- Publication number
- JP3989576B2 JP3989576B2 JP24676896A JP24676896A JP3989576B2 JP 3989576 B2 JP3989576 B2 JP 3989576B2 JP 24676896 A JP24676896 A JP 24676896A JP 24676896 A JP24676896 A JP 24676896A JP 3989576 B2 JP3989576 B2 JP 3989576B2
- Authority
- JP
- Japan
- Prior art keywords
- solid
- blade
- gas turbine
- suction side
- pressure side
- 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
- 229910052751 metal Inorganic materials 0.000 title description 28
- 239000002184 metal Substances 0.000 title description 28
- 239000007787 solid Substances 0.000 claims description 64
- 239000002131 composite material Substances 0.000 claims description 31
- 239000006260 foam Substances 0.000 claims description 19
- 239000000463 material Substances 0.000 claims description 10
- 239000007769 metal material Substances 0.000 claims description 10
- 239000004616 structural foam Substances 0.000 claims description 10
- 239000000203 mixture Substances 0.000 claims description 4
- 239000000835 fiber Substances 0.000 description 5
- 239000011159 matrix material Substances 0.000 description 5
- 229910052755 nonmetal Inorganic materials 0.000 description 4
- 239000004593 Epoxy Substances 0.000 description 3
- 239000011230 binding agent Substances 0.000 description 3
- XQUPVDVFXZDTLT-UHFFFAOYSA-N 1-[4-[[4-(2,5-dioxopyrrol-1-yl)phenyl]methyl]phenyl]pyrrole-2,5-dione Chemical compound O=C1C=CC(=O)N1C(C=C1)=CC=C1CC1=CC=C(N2C(C=CC2=O)=O)C=C1 XQUPVDVFXZDTLT-UHFFFAOYSA-N 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 2
- 239000000956 alloy Substances 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 2
- 239000003822 epoxy resin Substances 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 229920003192 poly(bis maleimide) Polymers 0.000 description 2
- 229920000647 polyepoxide Polymers 0.000 description 2
- 229920001721 polyimide Polymers 0.000 description 2
- 229920000642 polymer Polymers 0.000 description 2
- 239000010936 titanium Substances 0.000 description 2
- 229910052719 titanium Inorganic materials 0.000 description 2
- 239000004642 Polyimide Substances 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 238000009825 accumulation Methods 0.000 description 1
- 238000007792 addition Methods 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 238000004873 anchoring Methods 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 238000000748 compression moulding Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000003628 erosive effect Effects 0.000 description 1
- 239000010419 fine particle Substances 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 239000006261 foam material Substances 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 238000005457 optimization Methods 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 239000009719 polyimide resin Substances 0.000 description 1
- 229920005989 resin Polymers 0.000 description 1
- 239000011347 resin Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 229920005992 thermoplastic resin Polymers 0.000 description 1
- 229920001187 thermosetting polymer Polymers 0.000 description 1
- 238000001721 transfer moulding Methods 0.000 description 1
- 239000002023 wood Substances 0.000 description 1
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
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/282—Selecting composite materials, e.g. blades with reinforcing filaments
-
- 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
- F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow blades
-
- 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)
- Materials Engineering (AREA)
- Architecture (AREA)
- Composite Materials (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US08/533,478 US5634771A (en) | 1995-09-25 | 1995-09-25 | Partially-metallic blade for a gas turbine |
| US08/533478 | 1995-09-25 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JPH09189202A JPH09189202A (ja) | 1997-07-22 |
| JPH09189202A5 JPH09189202A5 (enExample) | 2004-09-30 |
| JP3989576B2 true JP3989576B2 (ja) | 2007-10-10 |
Family
ID=24126125
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP24676896A Expired - Fee Related JP3989576B2 (ja) | 1995-09-25 | 1996-09-19 | ガスタービン用の部分的に金属製の翼 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US5634771A (enExample) |
| EP (1) | EP0764764B1 (enExample) |
| JP (1) | JP3989576B2 (enExample) |
| DE (1) | DE69619045T2 (enExample) |
Families Citing this family (122)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH1054204A (ja) * | 1996-05-20 | 1998-02-24 | General Electric Co <Ge> | ガスタービン用の多構成部翼 |
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| US5839882A (en) * | 1997-04-25 | 1998-11-24 | General Electric Company | Gas turbine blade having areas of different densities |
| US6004097A (en) * | 1997-09-26 | 1999-12-21 | Sure Alloy Steel Corp. | Coal mill exhauster fan |
| US5947688A (en) * | 1997-12-22 | 1999-09-07 | General Electric Company | Frequency tuned hybrid blade |
| US5913661A (en) * | 1997-12-22 | 1999-06-22 | General Electric Company | Striated hybrid blade |
| US6039542A (en) * | 1997-12-24 | 2000-03-21 | General Electric Company | Panel damped hybrid blade |
| US6224339B1 (en) | 1998-07-08 | 2001-05-01 | Allison Advanced Development Company | High temperature airfoil |
| US6033186A (en) * | 1999-04-16 | 2000-03-07 | General Electric Company | Frequency tuned hybrid blade |
| US6282786B1 (en) | 1999-08-16 | 2001-09-04 | General Electric Company | Method of making injection formed hybrid airfoil |
| US6099257A (en) * | 1999-08-31 | 2000-08-08 | General Electric Company | Plastically formed hybrid airfoil |
| US6287080B1 (en) | 1999-11-15 | 2001-09-11 | General Electric Company | Elastomeric formulation used in the construction of lightweight aircraft engine fan blades |
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| EP1186748A1 (de) * | 2000-09-05 | 2002-03-13 | Siemens Aktiengesellschaft | Laufschaufel für eine Strömungsmaschine sowie Strömungsmaschine |
| US6884507B2 (en) * | 2001-10-05 | 2005-04-26 | General Electric Company | Use of high modulus, impact resistant foams for structural components |
| WO2003093101A1 (en) * | 2002-04-29 | 2003-11-13 | Rolls-Royce Naval Marine, Inc. | Propeller |
| FR2852999B1 (fr) * | 2003-03-28 | 2007-03-23 | Snecma Moteurs | Aube allegee de turbomachine et son procede de fabrication |
| US7575417B2 (en) * | 2003-09-05 | 2009-08-18 | General Electric Company | Reinforced fan blade |
| US7211559B2 (en) * | 2003-10-31 | 2007-05-01 | University Of Maryland, Baltimore | Factor VIII compositions and methods |
| JP2005240748A (ja) * | 2004-02-27 | 2005-09-08 | Mitsubishi Electric Corp | 送風機 |
| US7104760B2 (en) * | 2004-05-05 | 2006-09-12 | General Electric Company | Hybrid bucket and related method of pocket design |
| GB2451779A (en) * | 2004-09-22 | 2009-02-11 | Rolls Royce Plc | Manufacturing aerofoil with metal foam core |
| US7789621B2 (en) * | 2005-06-27 | 2010-09-07 | Rolls-Royce North American Technologies, Inc. | Gas turbine engine airfoil |
| GB0516036D0 (en) | 2005-08-04 | 2005-09-14 | Rolls Royce Plc | Aerofoil |
| US7334997B2 (en) * | 2005-09-16 | 2008-02-26 | General Electric Company | Hybrid blisk |
| US7766625B2 (en) * | 2006-03-31 | 2010-08-03 | General Electric Company | Methods and apparatus for reducing stress in turbine buckets |
| US7942639B2 (en) * | 2006-03-31 | 2011-05-17 | General Electric Company | Hybrid bucket dovetail pocket design for mechanical retainment |
| US7588421B2 (en) * | 2006-03-31 | 2009-09-15 | General Electric Company | Methods and apparatus for mechanical retainment of non-metallic fillers in pockets |
| US7547194B2 (en) * | 2006-07-31 | 2009-06-16 | General Electric Company | Rotor blade and method of fabricating the same |
| KR101173327B1 (ko) | 2007-03-07 | 2012-08-10 | 현대중공업 주식회사 | 복합재료를 이용한 선박용 프로펠러 및 그 제조 방법 |
| ES2329324B1 (es) * | 2007-03-30 | 2010-09-06 | Airbus España, S.L. | Borde de ataque de aeronave de material compuesto reforzado. |
| US7828526B2 (en) * | 2007-04-11 | 2010-11-09 | General Electric Company | Metallic blade having a composite inlay |
| US7901189B2 (en) | 2007-05-14 | 2011-03-08 | General Electric Company | Wind-turbine blade and method for reducing noise in wind turbine |
| US20090081032A1 (en) * | 2007-09-20 | 2009-03-26 | General Electric Company | Composite airfoil |
| ITTO20080013A1 (it) * | 2008-01-09 | 2009-07-10 | Rosati Flii S R L | Ventola a geometria variabile e procedimento per la fabbricazione delle relative pale |
| DE102008031329A1 (de) * | 2008-07-02 | 2010-01-07 | Mtu Aero Engines Gmbh | Verfahren zum Herstellen von Gasturbinenschaufeln |
| RU2401727C2 (ru) * | 2008-12-25 | 2010-10-20 | Российская Федерация, от имени которой выступает государственный заказчик - Министерство промышленности и торговли (Минпромторг России) | Способ изготовления облегченной лопатки для газотурбинных двигателей |
| US8251651B2 (en) * | 2009-01-28 | 2012-08-28 | United Technologies Corporation | Segmented ceramic matrix composite turbine airfoil component |
| DE102009036018A1 (de) * | 2009-08-04 | 2011-02-17 | Siemens Aktiengesellschaft | Thermoplastendstufenschaufel |
| US8083489B2 (en) * | 2009-04-16 | 2011-12-27 | United Technologies Corporation | Hybrid structure fan blade |
| US8585368B2 (en) | 2009-04-16 | 2013-11-19 | United Technologies Corporation | Hybrid structure airfoil |
| US8075274B2 (en) * | 2009-05-13 | 2011-12-13 | Hamilton Sundstrand Corporation | Reinforced composite fan blade |
| EP2461923B1 (en) | 2009-08-09 | 2016-10-05 | Rolls-Royce Corporation | Method for forming a cast article |
| GB0916758D0 (en) * | 2009-09-24 | 2009-11-04 | Rolls Royce Plc | A hybrid component |
| DE102010006384A1 (de) * | 2010-01-29 | 2011-08-04 | Lufthansa Technik AG, 22335 | Reparaturverfahren für ein Verbundbauteil für ein Luftfahrzeug, Verbundbauteil für ein Luftfahrzeug und Einrichtung zur Reparatur eines Verbundbauteiles für ein Luftfahrzeug |
| FR2956875B1 (fr) * | 2010-02-26 | 2012-09-21 | Snecma | Aube allegee pour turbomachine, carter comportant une pluralite d'une telle aube et turbomachine comportant au moins un tel carter |
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| DE102012023617A1 (de) * | 2012-12-04 | 2014-06-05 | Voith Patent Gmbh | Schaufelblatt für eine Wasserturbine |
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| US11572796B2 (en) | 2020-04-17 | 2023-02-07 | Raytheon Technologies Corporation | Multi-material vane for a gas turbine engine |
| US11795831B2 (en) | 2020-04-17 | 2023-10-24 | Rtx Corporation | Multi-material vane for a gas turbine engine |
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| CN115701482A (zh) * | 2021-08-02 | 2023-02-10 | 通用电气公司 | 用于燃气涡轮发动机的具有易碎翼梁的转子叶片 |
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| US11560801B1 (en) | 2021-12-23 | 2023-01-24 | Rolls-Royce North American Technologies Inc. | Fan blade with internal magnetorheological fluid damping |
| US11795827B1 (en) * | 2022-04-04 | 2023-10-24 | General Electric Company | Airfoil assembly with a structurally reinforced foam core |
| US11753942B1 (en) | 2022-04-11 | 2023-09-12 | General Electric Company | Frangible airfoils |
| US20230392504A1 (en) * | 2022-06-03 | 2023-12-07 | Raytheon Technologies Corporation | Polymeric foams for hollow cavities |
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| FR3158536A1 (fr) * | 2024-01-24 | 2025-07-25 | Safran Aircraft Engines | Aube comportant un corps metallique et un noyau non metallique et procédé de fabrication d’une telle aube |
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| GB1284538A (en) * | 1968-11-19 | 1972-08-09 | Rolls Royce | Blade for a fluid flow machine |
| US3695778A (en) * | 1970-09-18 | 1972-10-03 | Trw Inc | Turbine blade |
| FR2165264A5 (en) * | 1971-12-23 | 1973-08-03 | Onera (Off Nat Aerospatiale) | Turbine blades - of synthetic resin incorporate reinforcing plate which is exposed at the leading edge |
| US3779338A (en) * | 1972-01-27 | 1973-12-18 | Bolt Beranek & Newman | Method of reducing sound generation in fluid flow systems embodying foil structures and the like |
| US3903578A (en) * | 1972-02-28 | 1975-09-09 | United Aircraft Corp | Composite fan blade and method of construction |
| US4118147A (en) * | 1976-12-22 | 1978-10-03 | General Electric Company | Composite reinforcement of metallic airfoils |
| US4108572A (en) * | 1976-12-23 | 1978-08-22 | United Technologies Corporation | Composite rotor blade |
| US4594761A (en) * | 1984-02-13 | 1986-06-17 | General Electric Company | Method of fabricating hollow composite airfoils |
| GB2168111B (en) * | 1984-12-08 | 1988-05-18 | Rolls Royce | Rotor aerofoil blade containment |
| US5145320A (en) * | 1990-08-28 | 1992-09-08 | The United States Of America As Represented By The Secretary Of The Navy | Mass loaded composite rotor for vibro-acoustic application |
| US5269658A (en) * | 1990-12-24 | 1993-12-14 | United Technologies Corporation | Composite blade with partial length spar |
| JPH04272499A (ja) * | 1991-02-27 | 1992-09-29 | Matsushita Electric Ind Co Ltd | 送風機およびその羽根車の製造方法 |
| GB2254892A (en) * | 1991-04-16 | 1992-10-21 | Gen Electric | Hollow airfoil. |
| FR2688264A1 (fr) * | 1992-03-04 | 1993-09-10 | Snecma | Redresseur de turbomachine a aubes ayant une face alveolee chargee en materiau composite. |
| FR2695163B1 (fr) * | 1992-09-02 | 1994-10-28 | Snecma | Aube creuse pour turbomachine et son procédé de fabrication. |
| FR2698126B1 (fr) * | 1992-11-18 | 1994-12-16 | Snecma | Aube creuse de soufflante ou compresseur de turbomachine. |
| US5429877A (en) * | 1993-10-20 | 1995-07-04 | The United States Of America As Represented By The Secretary Of The Air Force | Internally reinforced hollow titanium alloy components |
-
1995
- 1995-09-25 US US08/533,478 patent/US5634771A/en not_active Expired - Fee Related
-
1996
- 1996-09-19 JP JP24676896A patent/JP3989576B2/ja not_active Expired - Fee Related
- 1996-09-25 EP EP96306989A patent/EP0764764B1/en not_active Expired - Lifetime
- 1996-09-25 DE DE69619045T patent/DE69619045T2/de not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| EP0764764A1 (en) | 1997-03-26 |
| JPH09189202A (ja) | 1997-07-22 |
| DE69619045D1 (de) | 2002-03-21 |
| US5634771A (en) | 1997-06-03 |
| DE69619045T2 (de) | 2002-10-17 |
| EP0764764B1 (en) | 2002-02-06 |
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