IT1183343B - Profili aerodinamici composti cavi e metodo per fabbricare i medesimi - Google Patents
Profili aerodinamici composti cavi e metodo per fabbricare i medesimiInfo
- Publication number
- IT1183343B IT1183343B IT19492/85A IT1949285A IT1183343B IT 1183343 B IT1183343 B IT 1183343B IT 19492/85 A IT19492/85 A IT 19492/85A IT 1949285 A IT1949285 A IT 1949285A IT 1183343 B IT1183343 B IT 1183343B
- Authority
- IT
- Italy
- Prior art keywords
- cables
- manufacturing
- same
- aerodynamic profiles
- profiles composed
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
- B29D99/00—Subject matter not provided for in other groups of this subclass
- B29D99/0025—Producing blades or the like, e.g. blades for turbines, propellers, or wings
- B29D99/0028—Producing blades or the like, e.g. blades for turbines, propellers, or wings hollow blades
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
- B23P15/04—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine or like blades from several pieces
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/16—Blades
- B64C11/20—Constructional features
- B64C11/26—Fabricated blades
-
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
-
- 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
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/49336—Blade making
- Y10T29/49337—Composite blade
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/49336—Blade making
- Y10T29/49339—Hollow blade
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49799—Providing transitory integral holding or handling portion
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
- Y10T29/49863—Assembling or joining with prestressing of part
- Y10T29/49867—Assembling or joining with prestressing of part of skin on frame member
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
- Y10T29/49893—Peripheral joining of opposed mirror image parts to form a hollow body
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Composite Materials (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Laminated Bodies (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/579,631 US4594761A (en) | 1984-02-13 | 1984-02-13 | Method of fabricating hollow composite airfoils |
Publications (2)
Publication Number | Publication Date |
---|---|
IT8519492A0 IT8519492A0 (it) | 1985-02-13 |
IT1183343B true IT1183343B (it) | 1987-10-22 |
Family
ID=24317703
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT19492/85A IT1183343B (it) | 1984-02-13 | 1985-02-13 | Profili aerodinamici composti cavi e metodo per fabbricare i medesimi |
Country Status (6)
Country | Link |
---|---|
US (1) | US4594761A (it) |
JP (1) | JPS60204903A (it) |
DE (1) | DE3504377A1 (it) |
FR (1) | FR2559423B1 (it) |
GB (1) | GB2154287B (it) |
IT (1) | IT1183343B (it) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103890366A (zh) * | 2011-10-24 | 2014-06-25 | 赫拉克勒斯公司 | 用于附接中空部件的设备 |
Families Citing this family (99)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH670406A5 (it) * | 1987-03-19 | 1989-06-15 | Bbc Brown Boveri & Cie | |
US4720244A (en) * | 1987-05-21 | 1988-01-19 | Hudson Products Corporation | Fan blade for an axial flow fan and method of forming same |
US4873751A (en) * | 1988-12-27 | 1989-10-17 | United Technologies Corporation | Fabrication or repair technique for integrally bladed rotor assembly |
US5056738A (en) * | 1989-09-07 | 1991-10-15 | General Electric Company | Damper assembly for a strut in a jet propulsion engine |
FR2654463A1 (fr) * | 1989-11-15 | 1991-05-17 | Snecma | Element de stator de turbomachine. |
US5120197A (en) * | 1990-07-16 | 1992-06-09 | General Electric Company | Tip-shrouded blades and method of manufacture |
CA2042218A1 (en) * | 1990-07-20 | 1992-01-21 | Jan C. Schilling | Composite airfoil with increased shear capability |
US5141400A (en) * | 1991-01-25 | 1992-08-25 | General Electric Company | Wide chord fan blade |
GB9112043D0 (en) * | 1991-06-05 | 1991-07-24 | Sec Dep For The Defence | A titanium compressor blade having a wear resistant portion |
FR2680384B1 (fr) * | 1991-08-13 | 1995-03-10 | Plastiremo | Couronne d'aubage a montage simplifie et aube pour sa realisation. |
US5180282A (en) * | 1991-09-27 | 1993-01-19 | General Electric Company | Gas turbine engine structural frame with multi-yoke attachment of struts to outer casing |
FR2685383B1 (fr) * | 1991-12-18 | 1994-02-11 | Snecma | Bras structural du carter d'une turbomachine. |
US5375978A (en) * | 1992-05-01 | 1994-12-27 | General Electric Company | Foreign object damage resistant composite blade and manufacture |
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 |
FR2719552B1 (fr) * | 1994-05-04 | 1996-07-26 | Eurocopter France | Aube de redresseur pour dispositif anti-couple à rotor et stator redresseur carénés d'hélicoptère. |
FR2719553B1 (fr) * | 1994-05-04 | 1996-07-26 | Eurocopter France | Dispositif anti-couple à rotor arrière et stator redresseur carénés pour hélicoptère. |
FR2721000B1 (fr) * | 1994-06-10 | 1996-08-23 | Eurocopter France | Aube de redresseur en composite, redresseur la comportant, pour dispositif anti-couple à rotor et stator redresseur carénés, et leur procédé de fabrication. |
US5486096A (en) * | 1994-06-30 | 1996-01-23 | United Technologies Corporation | Erosion resistant surface protection |
US5634771A (en) * | 1995-09-25 | 1997-06-03 | General Electric Company | Partially-metallic blade for a gas turbine |
US5655883A (en) * | 1995-09-25 | 1997-08-12 | General Electric Company | Hybrid blade for a gas turbine |
US5720597A (en) * | 1996-01-29 | 1998-02-24 | General Electric Company | Multi-component blade for a gas turbine |
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 |
US5876651A (en) * | 1996-05-29 | 1999-03-02 | United Technologies Corporation | Method for forming a composite structure |
US5765993A (en) * | 1996-09-27 | 1998-06-16 | Chromalloy Gas Turbine Corporation | Replacement vane assembly for fan exit guide |
US5931641A (en) * | 1997-04-25 | 1999-08-03 | General Electric Company | Steam turbine blade having areas of different densities |
US5839882A (en) * | 1997-04-25 | 1998-11-24 | General Electric Company | Gas turbine blade having areas of different densities |
US6048174A (en) * | 1997-09-10 | 2000-04-11 | United Technologies Corporation | Impact resistant hollow airfoils |
US6173925B1 (en) * | 1998-04-16 | 2001-01-16 | Daimlerchrysler Ag | Skin-rib structure |
US6139303A (en) * | 1998-11-20 | 2000-10-31 | United Technologies Corporation | Fixture for disposing a laser blocking material in an airfoil |
US6177038B1 (en) * | 1998-11-20 | 2001-01-23 | United Technologies Corporation | Method for orienting an airfoil for processing and for forming a mask for the airfoil |
US6224361B1 (en) * | 1998-11-20 | 2001-05-01 | United Technologies Corportion | Tool for disposing laser blocking material in an airfoil |
US6544460B2 (en) * | 1998-11-20 | 2003-04-08 | United Technologies Corporation | Method and fixture for disposing filler material in an article |
DE10051223A1 (de) | 2000-10-16 | 2002-04-25 | Alstom Switzerland Ltd | Verbindbare Statorelemente |
US6619917B2 (en) | 2000-12-19 | 2003-09-16 | United Technologies Corporation | Machined fan exit guide vane attachment pockets for use in a gas turbine |
US7141303B2 (en) * | 2001-03-06 | 2006-11-28 | 3M Innovative Properties Company | Protective articles |
US6705011B1 (en) | 2003-02-10 | 2004-03-16 | United Technologies Corporation | Turbine element manufacture |
FR2879496B1 (fr) * | 2004-12-16 | 2008-12-12 | Eurocopter France | Procede et dispositif de fabrication d'une carene de rotor d'helicoptere, et carene obtenue |
US7481573B2 (en) * | 2005-06-30 | 2009-01-27 | Spx Corporation | Mixing impeller with pre-shaped tip elements |
AU2006202877B2 (en) * | 2005-06-30 | 2010-12-02 | Spx Flow, Inc. | Mixing impeller and method with weld locations |
GB2427900B (en) * | 2005-07-02 | 2007-10-10 | Rolls Royce Plc | Vane support in a gas turbine engine |
AU2006297891B2 (en) * | 2005-10-03 | 2012-01-19 | Nolato Meditech Ab | Method and machine for producing a hollow product |
EP1801357B1 (fr) | 2005-12-22 | 2010-10-27 | Techspace Aero | Aubage statorique de turbomachine, turbomachine comportant l'aubage et aube de turbomachine |
US7648336B2 (en) * | 2006-01-03 | 2010-01-19 | General Electric Company | Apparatus and method for assembling a gas turbine stator |
WO2007099129A2 (en) | 2006-03-01 | 2007-09-07 | Coloplast A/S | Urisheath with moulded unrolling strip |
US20080072569A1 (en) * | 2006-09-27 | 2008-03-27 | Thomas Ory Moniz | Guide vane and method of fabricating the same |
DE102006061915A1 (de) * | 2006-12-21 | 2008-07-03 | Rolls-Royce Deutschland Ltd & Co Kg | Hybrid-Fanschaufel und Verfahren zu deren Herstellung |
US7753653B2 (en) * | 2007-01-12 | 2010-07-13 | General Electric Company | Composite inlet guide vane |
US7980817B2 (en) * | 2007-04-16 | 2011-07-19 | United Technologies Corporation | Gas turbine engine vane |
US7607287B2 (en) * | 2007-05-29 | 2009-10-27 | United Technologies Corporation | Airfoil acoustic impedance control |
GB2450934B (en) | 2007-07-13 | 2009-10-07 | Rolls Royce Plc | A Component with a damping filler |
SG154344A1 (en) * | 2008-01-09 | 2009-08-28 | United Technologies Corp | Airfoil mask, airfoil and mask system, and masking method for edge profile finishing |
GB0808840D0 (en) | 2008-05-15 | 2008-06-18 | Rolls Royce Plc | A compound structure |
US8333552B2 (en) * | 2008-06-20 | 2012-12-18 | General Electric Company | Combined acoustic absorber and heat exchanging outlet guide vanes |
GB2462102B (en) | 2008-07-24 | 2010-06-16 | Rolls Royce Plc | An aerofoil sub-assembly, an aerofoil and a method of making an aerofoil |
DE102008047043A1 (de) * | 2008-09-13 | 2010-03-18 | Mtu Aero Engines Gmbh | Ersatzteil für eine Gasturbinen-Schaufel einer Gasturbine, Gasturbinen-Schaufel sowie ein Verfahren zur Reparatur einer Gasturbinen-Schaufel |
GB0822909D0 (en) * | 2008-12-17 | 2009-01-21 | Rolls Royce Plc | Airfoil |
GB0901235D0 (en) | 2009-01-27 | 2009-03-11 | Rolls Royce Plc | An article with a filler |
GB0901318D0 (en) | 2009-01-28 | 2009-03-11 | Rolls Royce Plc | A method of joining plates of material to form a structure |
US8177513B2 (en) * | 2009-02-18 | 2012-05-15 | General Electric Company | Method and apparatus for a structural outlet guide vane |
FR2944839B1 (fr) * | 2009-04-22 | 2014-05-09 | Snecma | Carter intermediaire de turbomachine d'aeronef comprenant des bras structuraux de raccord a fonctions mecanique et aerodynamique dissociees |
US8967078B2 (en) * | 2009-08-27 | 2015-03-03 | United Technologies Corporation | Abrasive finish mask and method of polishing a component |
GB201001000D0 (en) | 2010-01-22 | 2010-03-10 | Rolls Royce Plc | Method of forming a hollow component with an internal structure |
US8814523B2 (en) * | 2010-03-01 | 2014-08-26 | Vari-Form, Inc. | Hydroformed turbine blade |
FR2958980B1 (fr) * | 2010-04-14 | 2013-03-15 | Snecma | Dispositif redresseur pour turbomachine |
GB201009216D0 (en) | 2010-06-02 | 2010-07-21 | Rolls Royce Plc | Rotationally balancing a rotating part |
US8794925B2 (en) | 2010-08-24 | 2014-08-05 | United Technologies Corporation | Root region of a blade for a gas turbine engine |
GB2485831B (en) | 2010-11-26 | 2012-11-21 | Rolls Royce Plc | A method of manufacturing a component |
US8727721B2 (en) * | 2010-12-30 | 2014-05-20 | General Electric Company | Vane with spar mounted composite airfoil |
US8690531B2 (en) * | 2010-12-30 | 2014-04-08 | General Electroc Co. | Vane with spar mounted composite airfoil |
DE102011008695A1 (de) * | 2011-01-15 | 2012-07-19 | Mtu Aero Engines Gmbh | Verfahren zum generativen Herstellen eines Bauelements mit einer integrierten Dämpfung für eine Strömungsmaschine und generativ hergestelltes Bauelement mit einer integrierten Dämpfung für eine Strömungsmaschine |
US8906181B2 (en) * | 2011-06-30 | 2014-12-09 | United Technologies Corporation | Fan blade finishing |
GB201115485D0 (en) | 2011-09-08 | 2011-10-26 | Rolls Royce Plc | An aerofoil assembly |
US8734925B2 (en) * | 2011-10-19 | 2014-05-27 | Hexcel Corporation | High pressure molding of composite parts |
US11035238B2 (en) | 2012-06-19 | 2021-06-15 | Raytheon Technologies Corporation | Airfoil including adhesively bonded shroud |
US9441496B2 (en) * | 2012-09-26 | 2016-09-13 | United Technologies Corporation | Structural guide vane internal topology |
US9527262B2 (en) * | 2012-09-28 | 2016-12-27 | General Electric Company | Layered arrangement, hot-gas path component, and process of producing a layered arrangement |
US9534498B2 (en) * | 2012-12-14 | 2017-01-03 | United Technologies Corporation | Overmolded vane platform |
US9003657B2 (en) * | 2012-12-18 | 2015-04-14 | General Electric Company | Components with porous metal cooling and methods of manufacture |
WO2014137468A1 (en) * | 2013-03-07 | 2014-09-12 | Rolls-Royce Canada, Ltd. | Gas turbine engine comprising an outboard insertion system of vanes and corresponding assembling method |
GB201306123D0 (en) * | 2013-04-05 | 2013-05-22 | Rolls Royce Plc | Vane assembly and method of making the same |
US9845162B2 (en) * | 2013-05-03 | 2017-12-19 | The Boeing Company | Protective finish for wing tip devices |
US9840929B2 (en) * | 2013-05-28 | 2017-12-12 | Pratt & Whitney Canada Corp. | Gas turbine engine vane assembly and method of mounting same |
JP6167677B2 (ja) * | 2013-06-06 | 2017-07-26 | 株式会社Ihi | ファンにおける翼及びファン |
FR3008639B1 (fr) * | 2013-07-18 | 2015-08-07 | Snecma | Procede d'assemblage de pieces de turbomachine et ensemble mis en œuvre lors d'un tel procede |
FR3010047B1 (fr) * | 2013-09-04 | 2017-03-31 | Snecma | Structure de liaison moteur-nacelle a platine a vis |
GB201316731D0 (en) * | 2013-09-20 | 2013-11-06 | Rolls Royce Plc | Manufacture of hollow aerofoil |
DE102013219774A1 (de) * | 2013-09-30 | 2015-04-02 | MTU Aero Engines AG | Schaufel für eine Gasturbine |
US10408224B2 (en) * | 2014-01-23 | 2019-09-10 | United Technologies Corporation | Fan blades with abrasive tips |
US10822970B2 (en) * | 2014-11-06 | 2020-11-03 | Raytheon Technologies Corporation | Gas turbine engine structural guide vanes |
WO2016090405A1 (en) * | 2014-12-08 | 2016-06-16 | Peter John Murdoch | A method of forming a fibre metal composite component |
FR3057295B1 (fr) * | 2016-10-12 | 2020-12-11 | Safran Aircraft Engines | Aube comprenant une plate-forme et une pale assemblees |
EP3428061B1 (en) * | 2017-07-13 | 2020-09-09 | Ratier-Figeac SAS | Protection of propeller components |
FR3074219B1 (fr) * | 2017-11-30 | 2019-10-25 | Safran Aircraft Engines | Ensemble de turbomachine avec une aube de stator a plateforme integree et moyens de maintien. |
US11073027B2 (en) * | 2018-05-17 | 2021-07-27 | Raytheon Technologies Corporation | Mold tool and methods for airfoil bonding |
FR3097452B1 (fr) * | 2019-06-20 | 2021-05-21 | Safran Aircraft Engines | Procédé de revêtement d’une aube de redresseur de turbomachine, aube de redresseur associée |
CN110439630B (zh) * | 2019-08-12 | 2022-07-29 | 航天材料及工艺研究所 | 一种变厚度复合材料静子叶片及其成型方法 |
FR3100741B1 (fr) * | 2019-09-13 | 2021-09-10 | Safran | Dispositif de fabrication d’une piece creuse |
US11905847B1 (en) * | 2022-10-21 | 2024-02-20 | Rtx Corporation | Airfoil with venturi tube |
US12078083B2 (en) * | 2022-12-20 | 2024-09-03 | Rtx Corporation | Contour weaves for interwoven vanes |
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US2641439A (en) * | 1947-10-01 | 1953-06-09 | Chrysler Corp | Cooled turbine or compressor blade |
GB778685A (en) * | 1953-11-20 | 1957-07-10 | Bristol Aircraft Ltd | Improvements in or relating to the construction and manufacture of aerofoils and thelike |
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DE1776015A1 (de) * | 1968-09-04 | 1971-09-16 | Daimler Benz Ag | Turbinenschaufel |
US3623204A (en) * | 1970-02-02 | 1971-11-30 | Gen Motors Corp | Method of fabricating hollow gas turbine blades |
US3695778A (en) * | 1970-09-18 | 1972-10-03 | Trw Inc | Turbine blade |
US3886647A (en) * | 1971-07-07 | 1975-06-03 | Trw Inc | Method of making erosion resistant articles |
US3903578A (en) * | 1972-02-28 | 1975-09-09 | United Aircraft Corp | Composite fan blade and method of construction |
US3799701A (en) * | 1972-02-28 | 1974-03-26 | United Aircraft Corp | Composite fan blade and method of construction |
US3981616A (en) * | 1974-10-22 | 1976-09-21 | The United States Of America As Represented By The Secretary Of The Air Force | Hollow composite compressor blade |
US4221539A (en) * | 1977-04-20 | 1980-09-09 | The Garrett Corporation | Laminated airfoil and method for turbomachinery |
US4273601A (en) * | 1977-10-31 | 1981-06-16 | Structural Composites Industries, Inc. | Method for the production of elongated resin impregnated filament composite structures |
FR2453294A1 (fr) * | 1979-04-04 | 1980-10-31 | Snecma | Dispositif de fixation d'aubes sur un rotor de compresseur pour turbo-reacteur |
US4301584A (en) * | 1980-01-31 | 1981-11-24 | United Technologies Corporation | Method of forming fiber and metal matrix composite |
DE3113079C2 (de) * | 1981-04-01 | 1985-11-21 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Aerodynamischer Groß-Flügel und Verfahren zu dessen Herstellung |
DE3151413A1 (de) * | 1981-12-24 | 1983-07-14 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | "schaufel einer stroemungsmaschine, insbesondere gasturbine" |
JPS58214602A (ja) * | 1982-06-07 | 1983-12-13 | Hitachi Ltd | タ−ビンノズル翼 |
-
1984
- 1984-02-13 US US06/579,631 patent/US4594761A/en not_active Expired - Lifetime
-
1985
- 1985-02-04 GB GB08502795A patent/GB2154287B/en not_active Expired
- 1985-02-06 FR FR8501667A patent/FR2559423B1/fr not_active Expired
- 1985-02-08 DE DE19853504377 patent/DE3504377A1/de not_active Ceased
- 1985-02-12 JP JP60023690A patent/JPS60204903A/ja active Granted
- 1985-02-13 IT IT19492/85A patent/IT1183343B/it active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103890366A (zh) * | 2011-10-24 | 2014-06-25 | 赫拉克勒斯公司 | 用于附接中空部件的设备 |
Also Published As
Publication number | Publication date |
---|---|
GB2154287B (en) | 1988-04-20 |
US4594761A (en) | 1986-06-17 |
FR2559423A1 (fr) | 1985-08-16 |
DE3504377A1 (de) | 1985-08-14 |
FR2559423B1 (fr) | 1987-01-16 |
GB8502795D0 (en) | 1985-03-06 |
GB2154287A (en) | 1985-09-04 |
JPH0427365B2 (it) | 1992-05-11 |
JPS60204903A (ja) | 1985-10-16 |
IT8519492A0 (it) | 1985-02-13 |
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