DE69709203D1 - Hybridwerkstoffgegenstand mit grosser "Festigkeit-Massen"-Verhältnis und Verfahren zu seiner Herstellung - Google Patents
Hybridwerkstoffgegenstand mit grosser "Festigkeit-Massen"-Verhältnis und Verfahren zu seiner HerstellungInfo
- Publication number
- DE69709203D1 DE69709203D1 DE69709203T DE69709203T DE69709203D1 DE 69709203 D1 DE69709203 D1 DE 69709203D1 DE 69709203 T DE69709203 T DE 69709203T DE 69709203 T DE69709203 T DE 69709203T DE 69709203 D1 DE69709203 D1 DE 69709203D1
- Authority
- DE
- Germany
- Prior art keywords
- mass
- strength
- production
- ratio
- hybrid material
- 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
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
- F01D5/286—Particular treatment of blades, e.g. to increase durability or resistance against corrosion or erosion
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C37/00—Component parts, details, accessories or auxiliary operations, not covered by group B29C33/00 or B29C35/00
- B29C37/0078—Measures or configurations for obtaining anchoring effects in the contact areas between layers
- B29C37/0082—Mechanical anchoring
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/06—Fibrous reinforcements only
- B29C70/08—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/46—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
- B29C70/48—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM], e.g. by vacuum
-
- 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
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/08—Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/08—Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
- B29L2031/082—Blades, e.g. for helicopters
-
- 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
- F05D2230/00—Manufacture
- F05D2230/30—Manufacture with deposition of material
- F05D2230/31—Layer deposition
- F05D2230/311—Layer deposition by torch or flame spraying
-
- 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
- F05D2230/00—Manufacture
- F05D2230/30—Manufacture with deposition of material
- F05D2230/31—Layer deposition
- F05D2230/312—Layer deposition by plasma spraying
-
- 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
- F05D2240/303—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the leading edge of a rotor 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
- 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
- Y10T29/4998—Combined manufacture including applying or shaping of fluent material
- Y10T29/49982—Coating
-
- 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
- Y10T29/4998—Combined manufacture including applying or shaping of fluent material
- Y10T29/49982—Coating
- Y10T29/49984—Coating and casting
-
- 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
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249924—Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
- Y10T428/24994—Fiber embedded in or on the surface of a polymeric matrix
- Y10T428/24995—Two or more layers
-
- 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
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249924—Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
- Y10T428/24994—Fiber embedded in or on the surface of a polymeric matrix
- Y10T428/24995—Two or more layers
- Y10T428/249951—Including a free metal or alloy constituent
-
- 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
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249924—Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
- Y10T428/24994—Fiber embedded in or on the surface of a polymeric matrix
- Y10T428/24995—Two or more layers
- Y10T428/249952—At least one thermosetting synthetic polymeric material layer
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Materials Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Laminated Bodies (AREA)
- Injection Moulding Of Plastics Or The Like (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9602535A FR2745589B1 (fr) | 1996-02-29 | 1996-02-29 | Piece hybride a haut rapport resistance-masse et procede de realisation |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69709203D1 true DE69709203D1 (de) | 2002-01-31 |
DE69709203T2 DE69709203T2 (de) | 2002-08-22 |
Family
ID=9489708
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69709203T Expired - Fee Related DE69709203T2 (de) | 1996-02-29 | 1997-02-27 | Hybridwerkstoffgegenstand mit grosser "Festigkeit-Massen"-Verhältnis und Verfahren zu seiner Herstellung |
Country Status (4)
Country | Link |
---|---|
US (2) | US5887332A (de) |
EP (1) | EP0792738B1 (de) |
DE (1) | DE69709203T2 (de) |
FR (1) | FR2745589B1 (de) |
Families Citing this family (59)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19751129C1 (de) * | 1997-11-19 | 1999-06-17 | Mtu Muenchen Gmbh | FAN-Rotorschaufel für ein Triebwerk |
US6416647B1 (en) * | 1998-04-21 | 2002-07-09 | Applied Materials, Inc. | Electro-chemical deposition cell for face-up processing of single semiconductor substrates |
US6261433B1 (en) | 1998-04-21 | 2001-07-17 | Applied Materials, Inc. | Electro-chemical deposition system and method of electroplating on substrates |
US6258220B1 (en) * | 1998-11-30 | 2001-07-10 | Applied Materials, Inc. | Electro-chemical deposition system |
DE19900233A1 (de) * | 1999-01-07 | 2000-07-13 | Moeller Plast Gmbh | Verfahren zur Herstellung eines hochbelastbaren Bauteils aus Kunststoff und hochbelastbares Bauteil |
US6282786B1 (en) * | 1999-08-16 | 2001-09-04 | General Electric Company | Method of making injection formed hybrid airfoil |
DE19959598A1 (de) * | 1999-12-10 | 2001-06-13 | Rolls Royce Deutschland | Verfahren zum Herstellen einer Schaufel einer Strömungsmaschine |
US20050145499A1 (en) * | 2000-06-05 | 2005-07-07 | Applied Materials, Inc. | Plating of a thin metal seed layer |
US7273535B2 (en) * | 2003-09-17 | 2007-09-25 | Applied Materials, Inc. | Insoluble anode with an auxiliary electrode |
GB2365078B (en) * | 2000-07-27 | 2004-04-21 | Rolls Royce Plc | A gas turbine engine blade |
US6875331B2 (en) * | 2002-07-11 | 2005-04-05 | Applied Materials, Inc. | Anode isolation by diffusion differentials |
US7223323B2 (en) * | 2002-07-24 | 2007-05-29 | Applied Materials, Inc. | Multi-chemistry plating system |
US20040134775A1 (en) * | 2002-07-24 | 2004-07-15 | Applied Materials, Inc. | Electrochemical processing cell |
US20040217005A1 (en) * | 2002-07-24 | 2004-11-04 | Aron Rosenfeld | Method for electroplating bath chemistry control |
US7247222B2 (en) * | 2002-07-24 | 2007-07-24 | Applied Materials, Inc. | Electrochemical processing cell |
US7128823B2 (en) | 2002-07-24 | 2006-10-31 | Applied Materials, Inc. | Anolyte for copper plating |
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 |
DE10337866B4 (de) * | 2003-08-18 | 2014-07-24 | MTU Aero Engines AG | Verfahren zur Herstellung von Bauteilen für Gasturbinen |
US20050092602A1 (en) * | 2003-10-29 | 2005-05-05 | Harald Herchen | Electrochemical plating cell having a membrane stack |
US20050092601A1 (en) * | 2003-10-29 | 2005-05-05 | Harald Herchen | Electrochemical plating cell having a diffusion member |
US20060102467A1 (en) * | 2004-11-15 | 2006-05-18 | Harald Herchen | Current collimation for thin seed and direct plating |
US7329101B2 (en) * | 2004-12-29 | 2008-02-12 | General Electric Company | Ceramic composite with integrated compliance/wear layer |
FR2892339B1 (fr) * | 2005-10-21 | 2009-08-21 | Snecma Sa | Procede de fabrication d'une aube de turbomachine composite, et aube obtenue par ce procede |
US7435056B2 (en) | 2006-02-28 | 2008-10-14 | Honeywell International Inc. | Leading edge erosion protection for composite stator vanes |
US7780420B1 (en) | 2006-11-16 | 2010-08-24 | Florida Turbine Technologies, Inc. | Turbine blade with a foam metal leading or trailing edge |
US20090120101A1 (en) * | 2007-10-31 | 2009-05-14 | United Technologies Corp. | Organic Matrix Composite Components, Systems Using Such Components, and Methods for Manufacturing Such Components |
US7805839B2 (en) * | 2007-12-31 | 2010-10-05 | Turbine Engine Components Technologies Corporation | Method of manufacturing a turbine fan blade |
US20090266870A1 (en) * | 2008-04-23 | 2009-10-29 | The Boeing Company | Joined composite structures with a graded coefficient of thermal expansion for extreme environment applications |
US8512808B2 (en) | 2008-04-28 | 2013-08-20 | The Boeing Company | Built-up composite structures with a graded coefficient of thermal expansion for extreme environment applications |
US9476928B2 (en) | 2009-04-28 | 2016-10-25 | Textron Innovations Inc. | System and method for detecting sensor leakage |
US8556589B2 (en) * | 2009-06-24 | 2013-10-15 | Teledyne Scientific & Imaging, Llc | Hybrid composite for erosion resistant helicopter blades |
US8256088B2 (en) * | 2009-08-24 | 2012-09-04 | Siemens Energy, Inc. | Joining mechanism with stem tension and interlocked compression ring |
US8979473B2 (en) | 2011-01-07 | 2015-03-17 | United Technologies Corporation | Attachment of threaded holes to composite fan case |
US8672609B2 (en) | 2009-08-31 | 2014-03-18 | United Technologies Corporation | Composite fan containment case assembly |
GB0915087D0 (en) * | 2009-09-01 | 2009-09-30 | Rolls Royce Plc | Aerofoil with erosion resistant leading edge |
DE102009048709B4 (de) * | 2009-10-08 | 2022-11-17 | Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. | Verbundbauteil aus Metall und Faserverbundwerkstoff und Verfahren zur Herstellung |
US8376712B2 (en) * | 2010-01-26 | 2013-02-19 | United Technologies Corporation | Fan airfoil sheath |
US20110182741A1 (en) * | 2010-01-26 | 2011-07-28 | United Technologies Corporation | Composite fan blade leading edge recamber |
JP5808111B2 (ja) * | 2011-02-04 | 2015-11-10 | 三菱重工業株式会社 | 航空機用複合材構造体、これを備えた航空機主翼および航空機胴体 |
US8858184B2 (en) * | 2011-09-21 | 2014-10-14 | Textron Innovations Inc. | Rotor blade erosion protection system |
FR2981292B1 (fr) * | 2011-10-18 | 2013-11-01 | Snecma | Procede de fabrication d'une aube finalisee en materiau composite |
US9279328B2 (en) * | 2011-10-25 | 2016-03-08 | Whitcraft Llc | Airfoil devices, leading edge components, and methods of making |
FR2989991B1 (fr) * | 2012-04-30 | 2016-01-08 | Snecma | Renfort structurel metallique d'aube de turbomachine |
WO2014137448A1 (en) * | 2013-03-08 | 2014-09-12 | United Technologies Corporation | Fan blades with protective sheaths and galvanic shields |
FR3009983B1 (fr) * | 2013-08-29 | 2016-02-12 | Snecma | Procede de fabrication d'un bord de renforcement d'aube et bord de renforcement obtenu par ce procede |
WO2015034612A1 (en) * | 2013-09-09 | 2015-03-12 | United Technologies Corporation | Fan blades and manufacture methods |
EP3044417B1 (de) * | 2013-09-09 | 2019-10-02 | United Technologies Corporation | Bläserschaufeln und herstellungsverfahren |
US9745851B2 (en) | 2015-01-15 | 2017-08-29 | General Electric Company | Metal leading edge on composite blade airfoil and shank |
FR3032145B1 (fr) * | 2015-01-29 | 2017-02-10 | Snecma | Procede de fabrication d'une pale d'helice |
FR3041684B1 (fr) * | 2015-09-28 | 2021-12-10 | Snecma | Aube comprenant un bouclier de bord d'attaque et procede de fabrication de l'aube |
US11149642B2 (en) | 2015-12-30 | 2021-10-19 | General Electric Company | System and method of reducing post-shutdown engine temperatures |
US11053861B2 (en) | 2016-03-03 | 2021-07-06 | General Electric Company | Overspeed protection system and method |
GB2549113A (en) * | 2016-04-05 | 2017-10-11 | Rolls Royce Plc | Composite bodies and their manufacture |
US10337405B2 (en) | 2016-05-17 | 2019-07-02 | General Electric Company | Method and system for bowed rotor start mitigation using rotor cooling |
US10583933B2 (en) | 2016-10-03 | 2020-03-10 | General Electric Company | Method and apparatus for undercowl flow diversion cooling |
US10947993B2 (en) | 2017-11-27 | 2021-03-16 | General Electric Company | Thermal gradient attenuation structure to mitigate rotor bow in turbine engine |
CN114311759B (zh) * | 2022-03-15 | 2022-07-15 | 成都飞机工业(集团)有限责任公司 | 一种壁板筋条成型方法 |
US11879411B2 (en) | 2022-04-07 | 2024-01-23 | General Electric Company | System and method for mitigating bowed rotor in a gas turbine engine |
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US3615276A (en) * | 1969-02-03 | 1971-10-26 | Robertson Co H H | Protected metal article |
CH538549A (de) * | 1970-09-01 | 1973-06-30 | Bbc Brown Boveri & Cie | Verfahren zum Aufbringen von Oberflächenschutzschichten auf Kunststoff |
US3762835A (en) * | 1971-07-02 | 1973-10-02 | Gen Electric | Foreign object damage protection for compressor blades and other structures and related methods |
DE2219301A1 (de) * | 1972-04-20 | 1973-11-08 | Messerschmitt Boelkow Blohm | Verbundwerkstoffbauteil |
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 |
US4075364A (en) * | 1976-04-15 | 1978-02-21 | Brunswick Corporation | Porous ceramic seals and method of making same |
US4338380A (en) * | 1976-04-05 | 1982-07-06 | Brunswick Corporation | Method of attaching ceramics to metals for high temperature operation and laminated composite |
FR2381662A1 (fr) * | 1977-02-28 | 1978-09-22 | Aerospatiale | Pale, notamment pour un rotor d'helicoptere, et son procede de fabrication |
FR2430354A1 (fr) * | 1978-07-07 | 1980-02-01 | Aerospatiale | Helice multipale a pas variable d'un type simplifie |
DE3136283C1 (de) * | 1981-09-12 | 1983-02-03 | Nukem Gmbh, 6450 Hanau | Verfahren zum Metallisieren kohlefaserverstaerkter Kunststoffteile |
US4460531A (en) * | 1982-05-10 | 1984-07-17 | The Boeing Company | Composite fiber reinforced propeller |
DE3568065D1 (en) * | 1984-07-16 | 1989-03-09 | Bbc Brown Boveri & Cie | Process for the deposition of a corrosion-inhibiting layer, comprising protective oxide-forming elements at the base of a gas turbine blade, and a corrosion-inhibiting layer |
DE4104198A1 (de) * | 1991-02-12 | 1992-08-13 | Basf Ag | Verfahren zur herstellung von formteilen mit guten oberflaecheneigenschaften |
US5217654A (en) * | 1992-01-30 | 1993-06-08 | The C. A. Lawton Company | Two-stage mat forming preforming and molding process |
US5433002A (en) * | 1994-05-05 | 1995-07-18 | The United States Of America As Represented By The Secretary Of The Navy | Fabrication process for complex composite parts |
-
1996
- 1996-02-29 FR FR9602535A patent/FR2745589B1/fr not_active Expired - Fee Related
-
1997
- 1997-02-21 US US08/804,074 patent/US5887332A/en not_active Expired - Fee Related
- 1997-02-27 EP EP97400437A patent/EP0792738B1/de not_active Expired - Lifetime
- 1997-02-27 DE DE69709203T patent/DE69709203T2/de not_active Expired - Fee Related
-
1998
- 1998-12-18 US US09/215,292 patent/US6132857A/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
US6132857A (en) | 2000-10-17 |
FR2745589A1 (fr) | 1997-09-05 |
EP0792738A1 (de) | 1997-09-03 |
FR2745589B1 (fr) | 1998-04-30 |
DE69709203T2 (de) | 2002-08-22 |
US5887332A (en) | 1999-03-30 |
EP0792738B1 (de) | 2001-12-19 |
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