DE69622002D1 - Gepfeilte Turbomaschinenschaufel - Google Patents
Gepfeilte TurbomaschinenschaufelInfo
- Publication number
- DE69622002D1 DE69622002D1 DE69622002T DE69622002T DE69622002D1 DE 69622002 D1 DE69622002 D1 DE 69622002D1 DE 69622002 T DE69622002 T DE 69622002T DE 69622002 T DE69622002 T DE 69622002T DE 69622002 D1 DE69622002 D1 DE 69622002D1
- Authority
- DE
- Germany
- Prior art keywords
- swept
- turbo machine
- machine blade
- blade
- turbo
- 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
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
- F01D5/16—Form or construction for counteracting blade vibration
-
- 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
- F01D5/141—Shape, i.e. outer, aerodynamic form
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D21/00—Pump involving supersonic speed of pumped fluids
-
- 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
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
- F04D29/324—Blades
-
- 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
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/38—Blades
- F04D29/384—Blades characterised by form
-
- 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
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/38—Blades
- F04D29/384—Blades characterised by form
- F04D29/386—Skewed blades
-
- 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
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
- F05D2220/327—Application in turbines in gas turbines to drive shrouded, high solidity propeller
-
- 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
- F05D2240/302—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor characteristics related to shock waves, transonic or supersonic flow
-
- 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
- F05D2250/70—Shape
-
- 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
- F05D2250/70—Shape
- F05D2250/71—Shape curved
- F05D2250/711—Shape curved convex
-
- 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
- F05D2250/70—Shape
- F05D2250/71—Shape curved
- F05D2250/712—Shape curved concave
-
- 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
- F05D2250/70—Shape
- F05D2250/71—Shape curved
- F05D2250/713—Shape curved inflexed
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US08/559,965 US5642985A (en) | 1995-11-17 | 1995-11-17 | Swept turbomachinery blade |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69622002D1 true DE69622002D1 (de) | 2002-08-01 |
DE69622002T2 DE69622002T2 (de) | 2002-12-12 |
Family
ID=24235807
Family Applications (3)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE1138877T Pending DE1138877T1 (de) | 1995-11-17 | 1996-11-15 | Gepfeilte Turbomaschinenschaufel |
DE69622002T Expired - Lifetime DE69622002T2 (de) | 1995-11-17 | 1996-11-15 | Gepfeilte Turbomaschinenschaufel |
DE69634933T Expired - Lifetime DE69634933T2 (de) | 1995-11-17 | 1996-11-15 | Gepfeilte Turbomaschinenschaufel |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE1138877T Pending DE1138877T1 (de) | 1995-11-17 | 1996-11-15 | Gepfeilte Turbomaschinenschaufel |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69634933T Expired - Lifetime DE69634933T2 (de) | 1995-11-17 | 1996-11-15 | Gepfeilte Turbomaschinenschaufel |
Country Status (4)
Country | Link |
---|---|
US (4) | US5642985A (de) |
EP (4) | EP1571342B1 (de) |
JP (2) | JP3902278B2 (de) |
DE (3) | DE1138877T1 (de) |
Families Citing this family (87)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5642985A (en) | 1995-11-17 | 1997-07-01 | United Technologies Corporation | Swept turbomachinery blade |
US6071077A (en) * | 1996-04-09 | 2000-06-06 | Rolls-Royce Plc | Swept fan blade |
GB9607316D0 (en) * | 1996-04-09 | 1996-06-12 | Rolls Royce Plc | Swept fan blade |
DE19812624A1 (de) | 1998-03-23 | 1999-09-30 | Bmw Rolls Royce Gmbh | Rotor-Schaufelblatt einer Axialströmungsmaschine |
EP0957236A1 (de) * | 1998-05-15 | 1999-11-17 | Asea Brown Boveri AG | Turbinenlaufschaufel |
US6195983B1 (en) | 1999-02-12 | 2001-03-06 | General Electric Company | Leaned and swept fan outlet guide vanes |
GB9922619D0 (en) * | 1999-09-25 | 1999-11-24 | Rolls Royce Plc | A gas turbine engine blade containment assembly |
US6312219B1 (en) | 1999-11-05 | 2001-11-06 | General Electric Company | Narrow waist vane |
US6299412B1 (en) | 1999-12-06 | 2001-10-09 | General Electric Company | Bowed compressor airfoil |
US6328533B1 (en) | 1999-12-21 | 2001-12-11 | General Electric Company | Swept barrel airfoil |
US6338609B1 (en) | 2000-02-18 | 2002-01-15 | General Electric Company | Convex compressor casing |
US6561761B1 (en) | 2000-02-18 | 2003-05-13 | General Electric Company | Fluted compressor flowpath |
US7334990B2 (en) * | 2002-01-29 | 2008-02-26 | Ramgen Power Systems, Inc. | Supersonic compressor |
US20030210980A1 (en) * | 2002-01-29 | 2003-11-13 | Ramgen Power Systems, Inc. | Supersonic compressor |
US7434400B2 (en) * | 2002-09-26 | 2008-10-14 | Lawlor Shawn P | Gas turbine power plant with supersonic shock compression ramps |
US7293955B2 (en) * | 2002-09-26 | 2007-11-13 | Ramgen Power Systrms, Inc. | Supersonic gas compressor |
FR2851798B1 (fr) | 2003-02-27 | 2005-04-29 | Snecma Moteurs | Aube en fleche de turboreacteur |
US6899526B2 (en) * | 2003-08-05 | 2005-05-31 | General Electric Company | Counterstagger compressor airfoil |
DE102004011607B4 (de) * | 2004-03-10 | 2016-11-24 | MTU Aero Engines AG | Verdichter einer Gasturbine sowie Gasturbine |
US7147426B2 (en) * | 2004-05-07 | 2006-12-12 | Pratt & Whitney Canada Corp. | Shockwave-induced boundary layer bleed |
US7204676B2 (en) * | 2004-05-14 | 2007-04-17 | Pratt & Whitney Canada Corp. | Fan blade curvature distribution for high core pressure ratio fan |
US7320575B2 (en) * | 2004-09-28 | 2008-01-22 | General Electric Company | Methods and apparatus for aerodynamically self-enhancing rotor blades |
DE102004054752A1 (de) * | 2004-11-12 | 2006-05-18 | Rolls-Royce Deutschland Ltd & Co Kg | Schaufel einer Strömungsarbeitsmaschine mit erweiterter Randprofiltiefe |
US7374403B2 (en) * | 2005-04-07 | 2008-05-20 | General Electric Company | Low solidity turbofan |
US7476086B2 (en) * | 2005-04-07 | 2009-01-13 | General Electric Company | Tip cambered swept blade |
DE102005059438B3 (de) * | 2005-12-13 | 2007-07-19 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Turbostrahlantrieb |
JP4863162B2 (ja) * | 2006-05-26 | 2012-01-25 | 株式会社Ihi | ターボファンエンジンのファン動翼 |
US7726937B2 (en) | 2006-09-12 | 2010-06-01 | United Technologies Corporation | Turbine engine compressor vanes |
GB0620769D0 (en) * | 2006-10-19 | 2006-11-29 | Rolls Royce Plc | A fan blade |
JP4664890B2 (ja) * | 2006-11-02 | 2011-04-06 | 三菱重工業株式会社 | 遷音速翼及び軸流回転機 |
FR2908152B1 (fr) * | 2006-11-08 | 2009-02-06 | Snecma Sa | Aube en fleche de turbomachine |
US8087884B2 (en) | 2006-11-30 | 2012-01-03 | General Electric Company | Advanced booster stator vane |
US8292574B2 (en) | 2006-11-30 | 2012-10-23 | General Electric Company | Advanced booster system |
US7967571B2 (en) * | 2006-11-30 | 2011-06-28 | General Electric Company | Advanced booster rotor blade |
DE102007020476A1 (de) * | 2007-04-27 | 2008-11-06 | Rolls-Royce Deutschland Ltd & Co Kg | Vorderkantenverlauf für Turbomaschinenkomponenten |
DE102007028787B4 (de) * | 2007-06-22 | 2013-05-23 | Ingersoll-Rand Klimasysteme Deutschland Gmbh | Kühlcontainer für land-, straßen- und schienengebundene Fahrzeuge |
DE102007028788B4 (de) * | 2007-06-22 | 2013-04-18 | Thermo King Container-Denmark A/S | Kühlcontainer für Schiffe |
WO2009000461A2 (de) * | 2007-06-22 | 2008-12-31 | Thermo King Deutschland Gmbh | Kühlcontainer für land-, strassen- und schienengebundene fahrzeuge |
JP2009008014A (ja) * | 2007-06-28 | 2009-01-15 | Mitsubishi Electric Corp | 軸流ファン |
FR2926856B1 (fr) * | 2008-01-30 | 2013-03-29 | Snecma | Compresseur de turboreacteur |
US8147207B2 (en) * | 2008-09-04 | 2012-04-03 | Siemens Energy, Inc. | Compressor blade having a ratio of leading edge sweep to leading edge dihedral in a range of 1:1 to 3:1 along the radially outer portion |
JP4923073B2 (ja) * | 2009-02-25 | 2012-04-25 | 株式会社日立製作所 | 遷音速翼 |
FR2974060B1 (fr) * | 2011-04-15 | 2013-11-22 | Snecma | Dispositif de propulsion a helices contrarotatives et coaxiales non-carenees |
US9790797B2 (en) * | 2011-07-05 | 2017-10-17 | United Technologies Corporation | Subsonic swept fan blade |
EP2568114A1 (de) | 2011-09-09 | 2013-03-13 | Siemens Aktiengesellschaft | Verfahren zum Profilieren einer Ersatzschaufel als ein Eratzteil für eine Altschaufel für eine Axialströmungsmaschine |
FR2983234B1 (fr) * | 2011-11-29 | 2014-01-17 | Snecma | Aube pour disque aubage monobloc de turbomachine |
FR2986285B1 (fr) * | 2012-01-30 | 2014-02-14 | Snecma | Aube pour soufflante de turboreacteur |
US9017036B2 (en) | 2012-02-29 | 2015-04-28 | United Technologies Corporation | High order shaped curve region for an airfoil |
FR2989107B1 (fr) * | 2012-04-04 | 2017-03-31 | Snecma | Aube de rotor de turbomachine |
US9121285B2 (en) * | 2012-05-24 | 2015-09-01 | General Electric Company | Turbine and method for reducing shock losses in a turbine |
FR2991373B1 (fr) * | 2012-05-31 | 2014-06-20 | Snecma | Aube de soufflante pour turboreacteur d'avion a profil cambre en sections de pied |
US9920653B2 (en) | 2012-12-20 | 2018-03-20 | United Technologies Corporation | Low pressure ratio fan engine having a dimensional relationship between inlet and fan size |
US9932933B2 (en) | 2012-12-20 | 2018-04-03 | United Technologies Corporation | Low pressure ratio fan engine having a dimensional relationship between inlet and fan size |
US9568009B2 (en) | 2013-03-11 | 2017-02-14 | Rolls-Royce Corporation | Gas turbine engine flow path geometry |
WO2015023325A1 (en) * | 2013-08-12 | 2015-02-19 | United Technologies Corporation | Non-axisymmetric fan flow path |
US9574567B2 (en) | 2013-10-01 | 2017-02-21 | General Electric Company | Supersonic compressor and associated method |
US10495106B2 (en) | 2014-02-19 | 2019-12-03 | United Technologies Corporation | Gas turbine engine airfoil |
WO2015175051A2 (en) | 2014-02-19 | 2015-11-19 | United Technologies Corporation | Gas turbine engine airfoil |
US9599064B2 (en) | 2014-02-19 | 2017-03-21 | United Technologies Corporation | Gas turbine engine airfoil |
WO2015175056A2 (en) * | 2014-02-19 | 2015-11-19 | United Technologies Corporation | Gas turbine engine airfoil |
US9163517B2 (en) * | 2014-02-19 | 2015-10-20 | United Technologies Corporation | Gas turbine engine airfoil |
US10584715B2 (en) | 2014-02-19 | 2020-03-10 | United Technologies Corporation | Gas turbine engine airfoil |
WO2015126824A1 (en) | 2014-02-19 | 2015-08-27 | United Technologies Corporation | Gas turbine engine airfoil |
EP3108105B1 (de) | 2014-02-19 | 2021-05-12 | Raytheon Technologies Corporation | Gasturbinenmotor-tragfläche |
US9567858B2 (en) | 2014-02-19 | 2017-02-14 | United Technologies Corporation | Gas turbine engine airfoil |
US10605259B2 (en) | 2014-02-19 | 2020-03-31 | United Technologies Corporation | Gas turbine engine airfoil |
US9140127B2 (en) | 2014-02-19 | 2015-09-22 | United Technologies Corporation | Gas turbine engine airfoil |
EP3108104B1 (de) | 2014-02-19 | 2019-06-12 | United Technologies Corporation | Gasturbinenmotor-tragfläche |
EP3108106B1 (de) | 2014-02-19 | 2022-05-04 | Raytheon Technologies Corporation | Schaufelblatt eines gasturbinenmotors |
EP4279706A3 (de) | 2014-02-19 | 2024-02-28 | RTX Corporation | Gasturbinenmotorschaufel |
US10570915B2 (en) | 2014-02-19 | 2020-02-25 | United Technologies Corporation | Gas turbine engine airfoil |
EP3108100B1 (de) | 2014-02-19 | 2021-04-14 | Raytheon Technologies Corporation | Gasturbinengebläseschaufel |
EP3108101B1 (de) | 2014-02-19 | 2022-04-20 | Raytheon Technologies Corporation | Gasturbinenmotor-tragfläche |
WO2015178974A2 (en) | 2014-02-19 | 2015-11-26 | United Technologies Corporation | Gas turbine engine airfoil |
EP3108116B1 (de) | 2014-02-19 | 2024-01-17 | RTX Corporation | Gasturbinenmotor |
EP3108117B2 (de) | 2014-02-19 | 2023-10-11 | Raytheon Technologies Corporation | Gasturbinenmotorschaufel |
EP3108103B1 (de) | 2014-02-19 | 2023-09-27 | Raytheon Technologies Corporation | Fanschaufel für ein gastrubinentriebwerk |
EP3575551B1 (de) * | 2014-02-19 | 2021-10-27 | Raytheon Technologies Corporation | Gasturbinenmotorschaufel |
RU2606294C1 (ru) * | 2015-07-06 | 2017-01-10 | Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения имени П.И. Баранова" | Рабочее колесо высокооборотного осевого вентилятора |
GB201512688D0 (en) * | 2015-07-20 | 2015-08-26 | Rolls Royce Plc | Aerofoil |
GB2544735B (en) * | 2015-11-23 | 2018-02-07 | Rolls Royce Plc | Vanes of a gas turbine engine |
US10479519B2 (en) * | 2015-12-31 | 2019-11-19 | United Technologies Corporation | Nacelle short inlet for fan blade removal |
US10458426B2 (en) | 2016-09-15 | 2019-10-29 | General Electric Company | Aircraft fan with low part-span solidity |
GB201702383D0 (en) * | 2017-02-14 | 2017-03-29 | Rolls Royce Plc | Gas turbine engine fan blade with axial lean |
GB201719538D0 (en) * | 2017-11-24 | 2018-01-10 | Rolls Royce Plc | Gas turbine engine |
FR3129686B1 (fr) * | 2021-11-29 | 2024-07-12 | Safran Aircraft Engines | Aube pour une soufflante carénée d’une turbomachine |
US12066027B2 (en) | 2022-08-11 | 2024-08-20 | Next Gen Compression Llc | Variable geometry supersonic compressor |
Family Cites Families (45)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2735612A (en) * | 1956-02-21 | hausmann | ||
US1964525A (en) * | 1932-07-30 | 1934-06-26 | Gen Electric | Fan blade |
US2154313A (en) * | 1938-04-01 | 1939-04-11 | Gen Electric | Directing vane |
US2628768A (en) | 1946-03-27 | 1953-02-17 | Kantrowitz Arthur | Axial-flow compressor |
US2935246A (en) * | 1949-06-02 | 1960-05-03 | Onera (Off Nat Aerospatiale) | Shock wave compressors, especially for use in connection with continuous flow engines for aircraft |
FR996967A (fr) * | 1949-09-06 | 1951-12-31 | Rateau Soc | Perfectionnement aux aubages de turbomachines |
US2689681A (en) | 1949-09-17 | 1954-09-21 | United Aircraft Corp | Reversely rotating screw type multiple impeller compressor |
US2660401A (en) * | 1951-08-07 | 1953-11-24 | Gen Electric | Turbine bucket |
US2830753A (en) * | 1951-11-10 | 1958-04-15 | Edward A Stalker | Axial flow compressors with circular arc blades |
US2915238A (en) * | 1953-10-23 | 1959-12-01 | Szydlowski Joseph | Axial flow compressors |
US2934259A (en) * | 1956-06-18 | 1960-04-26 | United Aircraft Corp | Compressor blading |
US3444817A (en) * | 1967-08-23 | 1969-05-20 | William J Caldwell | Fluid pump |
US3416725A (en) * | 1967-10-12 | 1968-12-17 | Acme Engineering And Mfg Corp | Dihedral bladed ventilating fan |
US3546882A (en) * | 1968-04-24 | 1970-12-15 | Gen Electric | Gas turbine engines |
US3692425A (en) * | 1969-01-02 | 1972-09-19 | Gen Electric | Compressor for handling gases at velocities exceeding a sonic value |
US4408957A (en) * | 1972-02-22 | 1983-10-11 | General Motors Corporation | Supersonic blading |
US3843277A (en) * | 1973-02-14 | 1974-10-22 | Gen Electric | Sound attenuating inlet duct |
US3989406A (en) * | 1974-11-26 | 1976-11-02 | Bolt Beranek And Newman, Inc. | Method of and apparatus for preventing leading edge shocks and shock-related noise in transonic and supersonic rotor blades and the like |
US4012172A (en) * | 1975-09-10 | 1977-03-15 | Avco Corporation | Low noise blades for axial flow compressors |
US4012165A (en) | 1975-12-08 | 1977-03-15 | United Technologies Corporation | Fan structure |
US4123196A (en) * | 1976-11-01 | 1978-10-31 | General Electric Company | Supersonic compressor with off-design performance improvement |
GB1598616A (en) | 1977-06-29 | 1981-09-23 | Kawasaki Heavy Ind Ltd | Diagonal-flow fan wheel with blades of developable surface shape |
IT1165216B (it) * | 1979-06-15 | 1987-04-22 | Mancinelli Euro Emme | Gruppo ventilatore per il convogliamento di aria attraverso una apertura circolare |
US4370097A (en) | 1979-07-16 | 1983-01-25 | United Technologies Corporation | Noise reduction means for prop-fan |
US4358246A (en) * | 1979-07-16 | 1982-11-09 | United Technologies Corporation | Noise reduction means for prop-fan and the construction thereof |
GB2164098B (en) * | 1984-09-07 | 1988-12-07 | Rolls Royce | Improvements in or relating to aerofoil section members for turbine engines |
JPS62114105U (de) * | 1986-01-09 | 1987-07-20 | ||
FR2603953B1 (fr) * | 1986-09-12 | 1991-02-22 | Peugeot Aciers Et Outillage | Pale profilee d'helice et son application aux motoventilateurs |
US4726737A (en) | 1986-10-28 | 1988-02-23 | United Technologies Corporation | Reduced loss swept supersonic fan blade |
US4784575A (en) * | 1986-11-19 | 1988-11-15 | General Electric Company | Counterrotating aircraft propulsor blades |
JPS63126501U (de) * | 1987-02-13 | 1988-08-18 | ||
SU1528965A1 (ru) * | 1988-02-17 | 1989-12-15 | Ташкентский Политехнический Институт Им.А.Р.Бируни | Рабочее колесо центробежного вентил тора |
JPH0745801B2 (ja) * | 1988-08-11 | 1995-05-17 | 三菱重工業株式会社 | 三次元タービン動翼 |
US5064345A (en) * | 1989-11-16 | 1991-11-12 | Airflow Research And Manufacturing Corporation | Multi-sweep blade with abrupt sweep transition |
US5088892A (en) * | 1990-02-07 | 1992-02-18 | United Technologies Corporation | Bowed airfoil for the compression section of a rotary machine |
US5112192A (en) * | 1990-07-26 | 1992-05-12 | General Signal Corporation | Mixing impellers and impeller systems for mixing and blending liquids and liquid suspensions having a wide range of viscosities |
US5167489A (en) * | 1991-04-15 | 1992-12-01 | General Electric Company | Forward swept rotor blade |
JPH0527201U (ja) * | 1991-09-19 | 1993-04-09 | 株式会社日立製作所 | 軸流タービン |
GB9307288D0 (en) | 1993-04-07 | 1993-06-02 | Rolls Royce Plc | Gas turbine engine casing construction |
JPH07224794A (ja) * | 1993-12-14 | 1995-08-22 | Mitsubishi Heavy Ind Ltd | 軸流機械の動翼 |
JP3118136B2 (ja) * | 1994-03-28 | 2000-12-18 | 株式会社先進材料利用ガスジェネレータ研究所 | 軸流圧縮機のケーシング |
US5584661A (en) | 1994-05-02 | 1996-12-17 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Forward sweep, low noise rotor blade |
US5642985A (en) * | 1995-11-17 | 1997-07-01 | United Technologies Corporation | Swept turbomachinery blade |
GB9607316D0 (en) | 1996-04-09 | 1996-06-12 | Rolls Royce Plc | Swept fan blade |
US6071077A (en) | 1996-04-09 | 2000-06-06 | Rolls-Royce Plc | Swept fan blade |
-
1995
- 1995-11-17 US US08/559,965 patent/US5642985A/en not_active Ceased
-
1996
- 1996-11-13 JP JP30141696A patent/JP3902278B2/ja not_active Expired - Lifetime
- 1996-11-15 EP EP05008514A patent/EP1571342B1/de not_active Expired - Lifetime
- 1996-11-15 EP EP10012698A patent/EP2278124A1/de not_active Withdrawn
- 1996-11-15 DE DE1138877T patent/DE1138877T1/de active Pending
- 1996-11-15 EP EP96308303A patent/EP0774567B1/de not_active Expired - Lifetime
- 1996-11-15 DE DE69622002T patent/DE69622002T2/de not_active Expired - Lifetime
- 1996-11-15 EP EP01112128A patent/EP1138877B1/de not_active Expired - Lifetime
- 1996-11-15 DE DE69634933T patent/DE69634933T2/de not_active Expired - Lifetime
-
1999
- 1999-06-30 US US09/343,736 patent/USRE38040E1/en not_active Expired - Lifetime
-
2001
- 2001-06-05 US US09/874,931 patent/USRE43710E1/en not_active Expired - Lifetime
-
2006
- 2006-11-08 JP JP2006302189A patent/JP4417947B2/ja not_active Expired - Lifetime
-
2010
- 2010-05-21 US US12/785,222 patent/USRE45689E1/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
EP2278124A1 (de) | 2011-01-26 |
EP1571342B1 (de) | 2012-06-27 |
EP0774567A1 (de) | 1997-05-21 |
DE69634933D1 (de) | 2005-08-18 |
USRE45689E1 (en) | 2015-09-29 |
USRE38040E1 (en) | 2003-03-18 |
EP1571342A2 (de) | 2005-09-07 |
DE1138877T1 (de) | 2003-05-28 |
USRE43710E1 (en) | 2012-10-02 |
DE69634933T2 (de) | 2006-05-24 |
JP4417947B2 (ja) | 2010-02-17 |
JP2007032579A (ja) | 2007-02-08 |
EP1571342A3 (de) | 2006-01-11 |
JPH09184451A (ja) | 1997-07-15 |
EP0774567B1 (de) | 2002-06-26 |
EP1138877A1 (de) | 2001-10-04 |
DE69622002T2 (de) | 2002-12-12 |
EP1138877B1 (de) | 2005-07-13 |
US5642985A (en) | 1997-07-01 |
JP3902278B2 (ja) | 2007-04-04 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE69622002D1 (de) | Gepfeilte Turbomaschinenschaufel | |
DE69520061D1 (de) | Turbinenschaufel | |
ID16132A (id) | Mesin turbo | |
DE69504071D1 (de) | Turbomaschine | |
DE19681310T1 (de) | Sägeblatt | |
DE69407518D1 (de) | Rotorschaufel | |
DE69838081D1 (de) | Turbinenschaufel | |
DE69822100D1 (de) | Turbinenschaufel | |
DE59705069D1 (de) | Scheibenwischblatt | |
DE69721114D1 (de) | Gekrümmte Gebläseschaufel | |
DE69619643D1 (de) | Flügelprofil | |
DE59507093D1 (de) | Wischblatt | |
NO955221L (no) | Sagblad | |
DE59701478D1 (de) | Konturschneidmaschine | |
DE59711982D1 (de) | Rotorblattanschluss | |
DE69728500D1 (de) | Turbomaschinenrotor | |
DE59706947D1 (de) | Wischerblatt | |
DK0948718T3 (da) | Rotorvinge | |
DE69704986D1 (de) | Doppelströmige Turbomaschine | |
DE59709583D1 (de) | Scheibenwischerblatt | |
KR950029045U (ko) | 로터베이터용 경운날 | |
ITBO960273A0 (it) | Macchina sezionatrice | |
NO974283D0 (no) | Anordning for roterende sagblad | |
BR7400057U (pt) | Lâminas pré-estrutural | |
SE9503336D0 (sv) | Torkarblad |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |