PT2113583E - Estruturas compósitas construídas com um coeficiente de expansão térmica graduado para aplicações em ambientes extremos - Google Patents
Estruturas compósitas construídas com um coeficiente de expansão térmica graduado para aplicações em ambientes extremos Download PDFInfo
- Publication number
- PT2113583E PT2113583E PT91588798T PT09158879T PT2113583E PT 2113583 E PT2113583 E PT 2113583E PT 91588798 T PT91588798 T PT 91588798T PT 09158879 T PT09158879 T PT 09158879T PT 2113583 E PT2113583 E PT 2113583E
- Authority
- PT
- Portugal
- Prior art keywords
- built
- thermal expansion
- composite structures
- extreme environment
- environment applications
- Prior art date
Links
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/115—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces by spraying molten metal, i.e. spray sintering, spray casting
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
- B22F5/009—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of turbine components other than turbine blades
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
- B22F7/06—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
- B22F7/08—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools with one or more parts not made from powder
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/02—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings only including layers of metallic material
- C23C28/021—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings only including layers of metallic material including at least one metal alloy layer
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/02—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings only including layers of metallic material
- C23C28/023—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings only including layers of metallic material only coatings of metal elements only
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/02—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings only including layers of metallic material
- C23C28/028—Including graded layers in composition or in physical properties, e.g. density, porosity, grain size
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/04—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/78—Other construction of jet pipes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
- F02K9/32—Constructional parts; Details not otherwise provided for
- F02K9/34—Casings; Combustion chambers; Liners thereof
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
- B22F10/20—Direct sintering or melting
- B22F10/25—Direct deposition of metal particles, e.g. direct metal deposition [DMD] or laser engineered net shaping [LENS]
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
- B22F10/20—Direct sintering or melting
- B22F10/28—Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM]
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2999/00—Aspects linked to processes or compositions used in powder metallurgy
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B33—ADDITIVE MANUFACTURING TECHNOLOGY
- B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
- B33Y50/00—Data acquisition or data processing for additive manufacturing
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- 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
- F05D2300/21—Oxide ceramics
-
- 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
- F05D2300/50—Intrinsic material properties or characteristics
- F05D2300/502—Thermal properties
- F05D2300/5021—Expansivity
- F05D2300/50212—Expansivity dissimilar
-
- 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
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P10/00—Technologies related to metal processing
- Y02P10/25—Process efficiency
-
- 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
- Y10T29/49616—Structural member making
-
- 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
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12535—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.] with additional, spatially distinct nonmetal component
- Y10T428/12611—Oxide-containing component
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Organic Chemistry (AREA)
- Metallurgy (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Composite Materials (AREA)
- Powder Metallurgy (AREA)
- Laminated Bodies (AREA)
- Standing Axle, Rod, Or Tube Structures Coupled By Welding, Adhesion, Or Deposition (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US12/110,595 US8512808B2 (en) | 2008-04-28 | 2008-04-28 | Built-up composite structures with a graded coefficient of thermal expansion for extreme environment applications |
Publications (1)
Publication Number | Publication Date |
---|---|
PT2113583E true PT2113583E (pt) | 2015-08-25 |
Family
ID=40858597
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PT91588798T PT2113583E (pt) | 2008-04-28 | 2009-04-27 | Estruturas compósitas construídas com um coeficiente de expansão térmica graduado para aplicações em ambientes extremos |
Country Status (5)
Country | Link |
---|---|
US (2) | US8512808B2 (pt) |
EP (1) | EP2113583B1 (pt) |
JP (1) | JP5623025B2 (pt) |
ES (1) | ES2545590T3 (pt) |
PT (1) | PT2113583E (pt) |
Families Citing this family (35)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
US8626478B1 (en) | 2010-07-16 | 2014-01-07 | The Boeing Company | Cross flow parameter calculation for aerodynamic analysis |
GB201015267D0 (en) * | 2010-09-14 | 2010-10-27 | Rolls Royce Plc | An object forming assembly |
US8974865B2 (en) * | 2011-02-23 | 2015-03-10 | General Electric Company | Component and a method of processing a component |
US8997496B2 (en) | 2011-06-29 | 2015-04-07 | United Technologies Corporation | Hybrid exhaust component |
EP2551040A1 (en) * | 2011-07-25 | 2013-01-30 | EADS Deutschland GmbH | Method of manufacturing a component by hot isostatic pressing |
FR2981700B1 (fr) * | 2011-10-24 | 2016-08-26 | Snecma Propulsion Solide | Dispositif de fixation d'une piece creuse |
GB201119238D0 (en) * | 2011-11-08 | 2011-12-21 | Rolls Royce Plc | A hot isostatic pressing tool and a method of manufacturing an article from powder material by hot isostatic pressing |
WO2013187936A1 (en) * | 2012-06-15 | 2013-12-19 | Pratt & Whitney Rocketdyne, Inc. | Additive manufacturing flow control |
US10167738B2 (en) | 2013-03-14 | 2019-01-01 | United Technologies Corporation | Compressor case snap assembly |
EP2789597B1 (en) | 2013-04-12 | 2017-11-15 | Ansaldo Energia IP UK Limited | Method for obtaining a configuration for joining a ceramic thermal insulating material to a metallic structure |
CA2915299A1 (en) | 2013-07-10 | 2015-01-15 | Dustin M. Bush | Methods for producing forged products and other worked products |
EP2839905A1 (en) * | 2013-08-22 | 2015-02-25 | Astrium GmbH | Manufacturing of components from parts made from different materials, particularly of space transportation components such as combustion chambers for thrusters |
WO2015047450A2 (en) * | 2013-09-30 | 2015-04-02 | United Technologies Corporation | A nonmetallic airfoil with a compliant attachment |
EP2886448B1 (en) * | 2013-12-20 | 2017-03-08 | Airbus Operations GmbH | A load bearing element and a method for manufacturing a load bearing element |
US9649690B2 (en) * | 2014-02-25 | 2017-05-16 | General Electric Company | System having layered structure and method of making the same |
JP6258739B2 (ja) * | 2014-03-26 | 2018-01-10 | 日本電子株式会社 | 3次元積層造形装置及び3次元積層造形方法 |
FR3020291B1 (fr) * | 2014-04-29 | 2017-04-21 | Saint Jean Ind | Procede de fabrication de pieces metalliques ou en composite a matrice metallique issues de fabrication additive suivie d'une operation de forgeage desdites pieces |
US10012104B2 (en) * | 2014-10-14 | 2018-07-03 | United Technologies Corporation | Gas turbine engine convergent/divergent nozzle with unitary synchronization ring for roller track nozzle |
GB201421894D0 (en) * | 2014-12-09 | 2015-01-21 | Ge Oil & Gas Uk Ltd | End fitting and method of manufacture |
CN104874797B (zh) * | 2015-06-05 | 2017-08-25 | 西迪技术股份有限公司 | 一种硬质合金功能梯度材料的成型方法 |
FR3038535B1 (fr) * | 2015-07-10 | 2017-08-11 | Commissariat Energie Atomique | Assemblage comprenant deux elements de coefficient de dilatation thermique differents et un joint fritte heterogene en densite et procede de fabrication de l'assemblage |
US20170051625A1 (en) * | 2015-08-17 | 2017-02-23 | United Technologies Corporation | Blade outer air seal component with varying thermal expansion coefficient |
DE102015219360A1 (de) * | 2015-10-07 | 2017-04-13 | Siemens Aktiengesellschaft | Auftragen einer Lotschicht mittels eines additiven Fertigungsverfahrens |
CA3011463C (en) | 2016-01-14 | 2020-07-07 | Arconic Inc. | Methods for producing forged products and other worked products |
US10343218B2 (en) | 2016-02-29 | 2019-07-09 | General Electric Company | Casting with a second metal component formed around a first metal component using hot isostactic pressing |
CN106335644B (zh) * | 2016-09-23 | 2019-03-29 | 江西洪都航空工业集团有限责任公司 | 一种整体成型尾喷口结构 |
RU175398U1 (ru) * | 2017-04-24 | 2017-12-04 | Алексей Витальевич Солодовников | Камера жидкостного ракетного двигателя |
US11465243B2 (en) * | 2017-11-06 | 2022-10-11 | The Boeing Company | Interlayered structures for joining dissimilar materials and methods for joining dissimilar metals |
US11333105B1 (en) * | 2018-04-27 | 2022-05-17 | United States Of America As Represented By The Administrator Of Nasa | Thrust chamber liner and fabrication method therefor |
US20190329355A1 (en) * | 2018-04-27 | 2019-10-31 | United States Of America As Represented By The Administrator Of Nasa | Method for Fabricating Seal-Free Multi-Metallic Thrust Chamber Liner |
US11426818B2 (en) | 2018-08-10 | 2022-08-30 | The Research Foundation for the State University | Additive manufacturing processes and additively manufactured products |
DE102019211709A1 (de) * | 2019-08-05 | 2021-02-11 | Hermle Maschinenbau Gmbh | Verfahren und Anordnung zum Herstellen eines Bauteils mittels heißisostatischem Pressen |
US12070881B2 (en) | 2019-09-19 | 2024-08-27 | Flow International Corporation | Systems and methods of interim and end of process treatment of manufactured articles using high pressure and waterjets |
US11459980B2 (en) | 2019-12-02 | 2022-10-04 | Rohr, Inc. | Compression ring for exhaust nozzle and center body attachment |
Family Cites Families (51)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2759249A (en) | 1950-06-20 | 1956-08-21 | Babcock & Wilcox Co | Welding dissimilar metal members with welded joint, including stabilized ferritic metal zone |
US3284174A (en) * | 1962-04-16 | 1966-11-08 | Ind Fernand Courtoy Bureau Et | Composite structures made by bonding ceramics, cermets, alloys, heavy alloys and metals of different thermal expansion coefficient |
US3633520A (en) * | 1970-04-02 | 1972-01-11 | Us Army | Gradient armor system |
JPS5412903B2 (pt) | 1974-04-15 | 1979-05-26 | ||
DD124649A1 (pt) | 1975-05-12 | 1977-03-09 | ||
FR2411062A1 (fr) * | 1977-12-07 | 1979-07-06 | Pechiney Aluminium | Procede d'assemblage de pieces a base d'aluminium et de pieces en acier |
DE2845716C2 (de) * | 1978-10-20 | 1985-08-01 | Volkswagenwerk Ag, 3180 Wolfsburg | Thermisch hoch beanspruchbare Verbindung |
US4333670A (en) * | 1980-05-05 | 1982-06-08 | General Atomic Company | Stepped transition joint |
US4333671A (en) | 1980-05-05 | 1982-06-08 | General Atomic Company | Friction welded transition joint |
EP0109814B1 (en) | 1982-11-17 | 1988-02-03 | Ae Plc | Joining silicon nitride to metals |
US4512699A (en) * | 1983-05-17 | 1985-04-23 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Daze fasteners |
DE3418473A1 (de) * | 1984-05-18 | 1985-11-21 | Daimler-Benz Ag, 7000 Stuttgart | Verbindung zwischen mindestens zwei thermisch hochbelasteten koerpern, wie rohre, ringe, scheiben, platten u.dgl. |
JPS61117171A (ja) * | 1984-11-08 | 1986-06-04 | 新明和工業株式会社 | 熱応力緩和体 |
JPS62256777A (ja) * | 1986-04-30 | 1987-11-09 | 日本鋼管株式会社 | セラミツク−金属接合体の冷却方法 |
JPS6313664A (ja) | 1986-07-04 | 1988-01-20 | Kubota Ltd | 異種材料の接合方法 |
US4702406A (en) | 1986-10-16 | 1987-10-27 | Carolina Power & Light Company | Forming stable welded joints between dissimilar metals |
US4834569A (en) * | 1987-05-13 | 1989-05-30 | The Boeing Company | Thermal expansion compensating joint assembly |
JPH01312015A (ja) * | 1988-06-10 | 1989-12-15 | Toshiba Corp | 熱膨張調整部材の製造方法 |
CA2041418A1 (en) | 1990-05-31 | 1991-12-01 | Albert G. Tobin | Method of protecting ceramic surfaces |
CA2038273A1 (en) * | 1990-06-29 | 1991-12-30 | Paul A. Siemers | Tube fabrication with reusable mandrel |
JP2734484B2 (ja) * | 1990-09-03 | 1998-03-30 | 三菱重工業株式会社 | 熱間静水加圧処理法 |
US5277496A (en) | 1990-10-17 | 1994-01-11 | Ametek, Inc. | High temperature optical probe |
US5633093A (en) * | 1991-06-25 | 1997-05-27 | Dana Corporation | Counterweight attachment technique |
FR2685035B1 (fr) * | 1991-12-16 | 1994-03-25 | Aerospatiale | Dispositif de montage de deux pieces en materiaux a coefficients de dilatation differents, soumises a des variations de temperature elevees. |
US5811055A (en) * | 1996-02-06 | 1998-09-22 | Geiger; Michael B. | Torch mounted gas scavaging system for manual and robotic welding and cutting torches |
FR2745589B1 (fr) | 1996-02-29 | 1998-04-30 | Snecma | Piece hybride a haut rapport resistance-masse et procede de realisation |
CA2232517C (en) * | 1997-03-21 | 2004-02-17 | Honda Giken Kogyo Kabushiki Kaisha .) | Functionally gradient material and method for producing the same |
US5861714A (en) * | 1997-06-27 | 1999-01-19 | Osram Sylvania Inc. | Ceramic envelope device, lamp with such a device, and method of manufacture of such devices |
DE69812014T2 (de) * | 1997-08-29 | 2003-12-24 | Hughes Electronics Corp., El Segundo | Raketenmotor mit einem Verbindungsstück zwischen Verbrennungskammer und Injektor |
US6089444A (en) * | 1997-09-02 | 2000-07-18 | Mcdonnell Douglas Corporation | Process of bonding copper and tungsten |
US6733907B2 (en) * | 1998-03-27 | 2004-05-11 | Siemens Westinghouse Power Corporation | Hybrid ceramic material composed of insulating and structural ceramic layers |
US6227432B1 (en) | 1999-02-18 | 2001-05-08 | Showa Aluminum Corporation | Friction agitation jointing method of metal workpieces |
DE19927734C2 (de) * | 1999-06-17 | 2002-04-11 | Astrium Gmbh | Schubkammer eines Antriebstriebwerks für Satelliten und Transportgeräte für Raumfahrtanwendungen |
US6352385B1 (en) | 2000-07-31 | 2002-03-05 | General Electric Company | Mechanical coupling for cooperating rotatable members |
JP2002309323A (ja) * | 2001-04-12 | 2002-10-23 | Toyama Prefecture | 低融点金属及び酸化物系セラミックスの傾斜機能材料及びその製造方法 |
US7097091B2 (en) | 2001-07-25 | 2006-08-29 | Hitachi, Ltd. | Friction stir welding method and component part welded by the method |
US20040024482A1 (en) * | 2002-07-29 | 2004-02-05 | Dawn White | Engineered thermal management devices and methods of the same |
US7470341B2 (en) * | 2002-09-18 | 2008-12-30 | Smith International, Inc. | Method of manufacturing a cutting element from a partially densified substrate |
US6912984B2 (en) | 2003-03-28 | 2005-07-05 | Eaton Corporation | Composite lightweight engine poppet valve |
AU2003238525A1 (en) | 2003-05-14 | 2004-12-03 | Alstom Technology Ltd | Method for welding together structural components and rotor produced according to said method |
US20050042023A1 (en) * | 2003-08-20 | 2005-02-24 | Jones Steve R. | Structural assemblies using integrally molded, and welded mechanically locking z-pins |
US7543662B2 (en) * | 2005-02-15 | 2009-06-09 | Smith International, Inc. | Stress-relieved diamond inserts |
JP2006347778A (ja) * | 2005-06-13 | 2006-12-28 | Gifu Prefecture | 傾斜機能材料の製造方法及び傾斜機能材料 |
US7807231B2 (en) * | 2005-11-30 | 2010-10-05 | General Electric Company | Process for forming thermal barrier coating resistant to infiltration |
US7754342B2 (en) * | 2005-12-19 | 2010-07-13 | General Electric Company | Strain tolerant corrosion protecting coating and spray method of application |
US7763356B2 (en) | 2006-03-13 | 2010-07-27 | United Technologies Corporation | Bond coating and thermal barrier compositions, processes for applying both, and their coated articles |
US20080160274A1 (en) | 2006-12-31 | 2008-07-03 | Chi Hung Dang | Coefficient of thermal expansion adaptor |
US20090208773A1 (en) | 2007-08-24 | 2009-08-20 | Lehigh University | Graded transitions for joining dissimilar metals and methods of fabrication therefor |
US7762447B2 (en) | 2008-03-20 | 2010-07-27 | Ut-Battelle, Llc | Multiple pass and multiple layer friction stir welding and material enhancement processes |
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 |
-
2008
- 2008-04-28 US US12/110,595 patent/US8512808B2/en not_active Expired - Fee Related
-
2009
- 2009-04-27 EP EP09158879.8A patent/EP2113583B1/en active Active
- 2009-04-27 PT PT91588798T patent/PT2113583E/pt unknown
- 2009-04-27 ES ES09158879.8T patent/ES2545590T3/es active Active
- 2009-04-28 JP JP2009109553A patent/JP5623025B2/ja not_active Expired - Fee Related
-
2013
- 2013-07-23 US US13/948,260 patent/US10316792B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
JP5623025B2 (ja) | 2014-11-12 |
EP2113583B1 (en) | 2015-06-03 |
US20130305727A1 (en) | 2013-11-21 |
JP2009299185A (ja) | 2009-12-24 |
US10316792B2 (en) | 2019-06-11 |
US8512808B2 (en) | 2013-08-20 |
EP2113583A1 (en) | 2009-11-04 |
ES2545590T3 (es) | 2015-09-14 |
US20090269497A1 (en) | 2009-10-29 |
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