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公开(公告)号:JP2003181599A
公开(公告)日:2003-07-02
申请号:JP2002309155
申请日:2002-10-24
Applicant: UNITED TECHNOLOGIES CORP
Inventor: SHAH DILIP M , THOMPSON BEALS JAMES , MARCIN JOHN JOSEPH JR , MURRAY STEPHEN DOUGLAS
Abstract: PROBLEM TO BE SOLVED: To provide a core for investment casting capable of manufacturing the core thinner than a present ceramic core and having improved mechanical characteristics. SOLUTION: The core is a composite article including a heat resistant metal element and a ceramic element. The heat resistant metal element is provided so as to improve the mechanical characteristics of the core or to allow the core having a shape and a shape dimension which cannot be obtained by the other method. In one embodiment, the overall core can be formed of the heat resistant metal constituting element. The core can be used for investment-casting a gas turbine superhard alloy constituting element. COPYRIGHT: (C)2003,JPO
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公开(公告)号:JP2000192208A
公开(公告)日:2000-07-11
申请号:JP36705799
申请日:1999-12-24
Applicant: UNITED TECHNOLOGIES CORP
Inventor: MARCIN JOHN JOSEPH JR , SCHIRRA JOHN JOSEPH , GIUGNO RALPH , NUNES JOY JOHN
IPC: C22C19/05 , B22D17/00 , B22D21/00 , C22C1/02 , C22C19/03 , C22C19/07 , C22F1/00 , C22F1/10 , C23C20060101 , F02C7/00
Abstract: PROBLEM TO BE SOLVED: To obtain the strength, durability and fatigue resistance matched for a corresponding superalloy forged member by executing the heat treatment at a specific temp. for specific time to the superalloy die casting member having blow hole and element segregation in cast condition. SOLUTION: The Ni base superalloy is heated and melted at the temp. higher than the melting temp. by 10-38 deg.C under reducing pressure of
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公开(公告)号:JP2000197957A
公开(公告)日:2000-07-18
申请号:JP36051899
申请日:1999-12-20
Applicant: UNITED TECHNOLOGIES CORP
Inventor: SCHIRRA JOHN J , ANDERSON DAVID WILLIAM , MARCIN JOHN JOSEPH JR , PRIVITZER EBERHART , SAMUELSON JEFFERY WILLIAM , TU JOHN SIUMING
IPC: B22D17/20
Abstract: PROBLEM TO BE SOLVED: To execute die casting a member having high m.p. in a good condition by selecting the ratio of the inside diameter and the outside diameter of a sleeve so as to minimize the thermal deformation of the sleeve in the case of pouring molten material into the shot sleeve. SOLUTION: The cylindrical sleeve has the inside diameter Ri and the outside diameter Ro in the cold state, and as the molten material is poured into a low portion, the low portion is expanded more than the portion at the upper side and deformed as shown with the broken line to form an elliptic shape shown with a major axis Ma and a minor axis Mm. In such a case, the ratio (Ro/Ri) of the outside diameter and the inside diameter is desirable to be at least 1.5. In this way, the molten material having suitable volume, (particularly, in the case of filling only a small portion of the molten material), is formed as bow shape in the longitudinal direction or formed as the elliptic shape, and it can be sufficiently minimized that the sleeve is thermally deformed and the machine can be prevented from jamming. further, the inside diameter is desirable to be at least 1.5 inch.
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公开(公告)号:JP2000192179A
公开(公告)日:2000-07-11
申请号:JP36705699
申请日:1999-12-24
Applicant: UNITED TECHNOLOGIES CORP
Inventor: SCHIRRA JOHN J , GIUGNO RALPH , GUSTAFSON WALTER FREDERICK , MARCIN JOHN JOSEPH JR , SAMUELSON JEFFREY WILLIAM , NORTON DELWYN EARLE
IPC: C22C19/05 , B22D17/00 , B22D21/00 , C22C1/02 , C22C19/03 , C22C19/07 , C22F1/00 , C22F1/10 , C23C20060101 , F02C7/00
Abstract: PROBLEM TO BE SOLVED: To form a die-cast member with a material having a high melting temp. such as a nickel base superalloy. SOLUTION: This die-cast member is composed of IN718 which is a nickel base superalloy. The microstructure of the member does not contain flowlines and has the fine average grain size of, for instance, ASTM3 or that finer than this. As the illustrative members, gas turbine engine members such as blades, vanes, cases and seals are included.
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公开(公告)号:ES2235445T3
公开(公告)日:2005-07-01
申请号:ES99310240
申请日:1999-12-20
Applicant: UNITED TECHNOLOGIES CORP
Inventor: SCHIRRA JOHN J , MARCIN JOHN JOSEPH JR , ANDERSON DAVID WILLIAM , PRIVITZER EBERHART , SAMUELSON JEFFERY WILLIAM , TU JOHN SIUMING
IPC: B22D17/20
Abstract: Un aparato de fundición a presión para fabricar objetos compuestos de un material que tiene una temperatura de fusión por encima de 1093ºC o más particularmente por encima de 1649ºC, comprendiendo el aparato: - una unidad (24) de fusión para fusión de al menos una carga única del material; - un troquel (36) de piezas múltiples, que define la cavidad del troquel ; - un manguito de disparo (30) generalmente cilíndrico, en comunicación de fluido con el troquel (36) y para recibir material fundido de la unidad (24) de fusión, teniendo el manguito radios interno (Ri) y externo (Ro); y - una unidad (40) de pistón en acoplamiento móvil y de cierre hermético con el manguito de disparo (30) a lo largo de una carrera del pistón para forzar el material desde el manguito de disparo (30) dentro de la cavidad (36) del troquel; caracterizado porque el aparato comprende además: - el medio (22) para proporcionar un entorno de presión reducida para la unidad (24) de fusión, el troquel (36) y el manguito de disparo (30); y porque - el radio (Ri) interno del manguito tiene al menos 25mm; y - la relación (Ro/Ri) es al menos 1,25.
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公开(公告)号:CA2408815C
公开(公告)日:2008-02-12
申请号:CA2408815
申请日:2002-10-18
Applicant: UNITED TECHNOLOGIES CORP
Inventor: MARCIN JOHN JOSEPH JR , MURRAY STEPHEN DOUGLAS , BEALS JAMES THOMPSON , SHAH DILIP M
Abstract: Concepts for fabricating improved cores for investment casting are described. The cores are composite which include refractory metal elements (200) and ceramic elements (120). The refractory metal elements are provided to enhance the mechanical properties of the core and/or to permit the fabrication of cores having shapes and geometries that could not otherwise be achieved. In one embodiment, the entire core may be made of refractory metal components. The cores may be used to investment cast gas turbine superalloy components.
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公开(公告)号:DE69923930T2
公开(公告)日:2006-04-06
申请号:DE69923930
申请日:1999-12-20
Applicant: UNITED TECHNOLOGIES CORP
Inventor: SCHIRRA JOHN J , MARCIN JOHN JOSEPH JR , ANDERSON DAVID WILLIAM , PRIVITZER EBERHART , SAMUELSON JEFFERY WILLIAM , TU JOHN SIUMING
IPC: B22D17/20
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公开(公告)号:DE60224631D1
公开(公告)日:2008-03-06
申请号:DE60224631
申请日:2002-10-23
Applicant: UNITED TECHNOLOGIES CORP
Inventor: SHAH DILIP M , MARCIN JOHN JOSEPH JR , THOMPSON BEALS JAMES , MURRAY STEPHEN DOUGLAS
Abstract: Concepts for fabricating improved cores for investment casting are described. The cores are composite and include refractory metal elements (200,202,204,206,208,210,212,214,216) and ceramic elements (120). The refractory metal elements are provided to enhance the mechanical properties of the core and/or to permit the fabrication of cores having shapes and geometries that could not otherwise be achieved. In one embodiment, the entire core may be made of refractory metal components. The cores may be used to investment cast gas turbine superalloy components.
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公开(公告)号:AT383918T
公开(公告)日:2008-02-15
申请号:AT02257358
申请日:2002-10-23
Applicant: UNITED TECHNOLOGIES CORP
Inventor: SHAH DILIP M , MARCIN JOHN JOSEPH JR , THOMPSON BEALS JAMES , MURRAY STEPHEN DOUGLAS
Abstract: Concepts for fabricating improved cores for investment casting are described. The cores are composite and include refractory metal elements (200,202,204,206,208,210,212,214,216) and ceramic elements (120). The refractory metal elements are provided to enhance the mechanical properties of the core and/or to permit the fabrication of cores having shapes and geometries that could not otherwise be achieved. In one embodiment, the entire core may be made of refractory metal components. The cores may be used to investment cast gas turbine superalloy components.
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公开(公告)号:DE60239112D1
公开(公告)日:2011-03-17
申请号:DE60239112
申请日:2002-10-23
Applicant: UNITED TECHNOLOGIES CORP
Inventor: SHAH DILIP M , THOMPSON BEALS JAMES , MARCIN JOHN JOSEPH JR , MURRAY STEPHEN DOUGLAS
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