ATE524255T1 - Feinguss - Google Patents
FeingussInfo
- Publication number
- ATE524255T1 ATE524255T1 AT05254403T AT05254403T ATE524255T1 AT E524255 T1 ATE524255 T1 AT E524255T1 AT 05254403 T AT05254403 T AT 05254403T AT 05254403 T AT05254403 T AT 05254403T AT E524255 T1 ATE524255 T1 AT E524255T1
- Authority
- AT
- Austria
- Prior art keywords
- core
- investment casting
- feed
- installing
- molding die
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C7/00—Patterns; Manufacture thereof so far as not provided for in other classes
- B22C7/02—Lost patterns
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/10—Cores; Manufacture or installation of cores
- B22C9/103—Multipart cores
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/02—Sand moulds or like moulds for shaped castings
- B22C9/04—Use of lost patterns
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D29/00—Removing castings from moulds, not restricted to casting processes covered by a single main group; Removing cores; Handling ingots
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Molds, Cores, And Manufacturing Methods Thereof (AREA)
- Braking Arrangements (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/891,660 US7172012B1 (en) | 2004-07-14 | 2004-07-14 | Investment casting |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE524255T1 true ATE524255T1 (de) | 2011-09-15 |
Family
ID=34941835
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT05254403T ATE524255T1 (de) | 2004-07-14 | 2005-07-14 | Feinguss |
Country Status (5)
Country | Link |
---|---|
US (2) | US7172012B1 (de) |
EP (1) | EP1616642B1 (de) |
JP (1) | JP2006026742A (de) |
KR (1) | KR100686658B1 (de) |
AT (1) | ATE524255T1 (de) |
Families Citing this family (66)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7172012B1 (en) * | 2004-07-14 | 2007-02-06 | United Technologies Corporation | Investment casting |
US7569172B2 (en) * | 2005-06-23 | 2009-08-04 | United Technologies Corporation | Method for forming turbine blade with angled internal ribs |
US7306026B2 (en) * | 2005-09-01 | 2007-12-11 | United Technologies Corporation | Cooled turbine airfoils and methods of manufacture |
US7185695B1 (en) * | 2005-09-01 | 2007-03-06 | United Technologies Corporation | Investment casting pattern manufacture |
US7744347B2 (en) * | 2005-11-08 | 2010-06-29 | United Technologies Corporation | Peripheral microcircuit serpentine cooling for turbine airfoils |
FR2896710B1 (fr) * | 2006-01-27 | 2009-10-30 | Snecma Sa | Procede de fabrication de piece de turbomachine comportant des orifices d'evacuation d'air de refroidissement |
US7686065B2 (en) * | 2006-05-15 | 2010-03-30 | United Technologies Corporation | Investment casting core assembly |
US20080005903A1 (en) † | 2006-07-05 | 2008-01-10 | United Technologies Corporation | External datum system and film hole positioning using core locating holes |
US20080110024A1 (en) * | 2006-11-14 | 2008-05-15 | Reilly P Brennan | Airfoil casting methods |
US7980819B2 (en) | 2007-03-14 | 2011-07-19 | United Technologies Corporation | Cast features for a turbine engine airfoil |
US7779892B2 (en) * | 2007-05-09 | 2010-08-24 | United Technologies Corporation | Investment casting cores and methods |
US8066052B2 (en) * | 2007-06-07 | 2011-11-29 | United Technologies Corporation | Cooled wall thickness control |
US8434997B2 (en) * | 2007-08-22 | 2013-05-07 | United Technologies Corporation | Gas turbine engine case for clearance control |
US20090112354A1 (en) * | 2007-10-30 | 2009-04-30 | Tahany Ibrahim El-Wardany | Method of determining optimal parameters for machining a workpiece |
US8236190B2 (en) * | 2008-06-13 | 2012-08-07 | United Technologies Corporation | Recast removal method |
US9174271B2 (en) * | 2008-07-02 | 2015-11-03 | United Technologies Corporation | Casting system for investment casting process |
US8157527B2 (en) * | 2008-07-03 | 2012-04-17 | United Technologies Corporation | Airfoil with tapered radial cooling passage |
FR2933884B1 (fr) * | 2008-07-16 | 2012-07-27 | Snecma | Procede de fabrication d'une piece d'aubage. |
US8572844B2 (en) * | 2008-08-29 | 2013-11-05 | United Technologies Corporation | Airfoil with leading edge cooling passage |
US8303252B2 (en) * | 2008-10-16 | 2012-11-06 | United Technologies Corporation | Airfoil with cooling passage providing variable heat transfer rate |
US8109725B2 (en) | 2008-12-15 | 2012-02-07 | United Technologies Corporation | Airfoil with wrapped leading edge cooling passage |
US8240999B2 (en) * | 2009-03-31 | 2012-08-14 | United Technologies Corporation | Internally supported airfoil and method for internally supporting a hollow airfoil during manufacturing |
CA2748304C (en) | 2009-05-20 | 2017-07-04 | Howmet Corporation | Pt-al-hf/zr coating and method |
EP2445668A2 (de) * | 2009-06-26 | 2012-05-02 | Havasu | Verfahren zur formung von armaturen und befestigungen |
EP2462079A4 (de) * | 2009-08-09 | 2015-07-29 | Rolls Royce Corp | Träger für einen gebrannten artikel |
US20110094698A1 (en) * | 2009-10-28 | 2011-04-28 | Howmet Corporation | Fugitive core tooling and method |
US8434546B1 (en) | 2010-03-30 | 2013-05-07 | Honda Motor Co., Ltd. | Casting mold core retention device and method |
US20130333855A1 (en) * | 2010-12-07 | 2013-12-19 | Gary B. Merrill | Investment casting utilizing flexible wax pattern tool for supporting a ceramic core along its length during wax injection |
CN102802834B (zh) * | 2010-12-07 | 2016-06-22 | 西门子能源有限公司 | 使用柔性蜡模工具的熔模铸造 |
US9879546B2 (en) * | 2012-06-21 | 2018-01-30 | United Technologies Corporation | Airfoil cooling circuits |
US9486853B2 (en) | 2012-09-14 | 2016-11-08 | United Technologies Corporation | Casting of thin wall hollow airfoil sections |
US20140102656A1 (en) | 2012-10-12 | 2014-04-17 | United Technologies Corporation | Casting Cores and Manufacture Methods |
JP6037756B2 (ja) * | 2012-10-12 | 2016-12-07 | 三菱重工業株式会社 | 鋳型製造方法及び鋳型 |
WO2014113184A1 (en) * | 2013-01-18 | 2014-07-24 | General Electric Company | Method of forming cast-in cooling holes in an aircraft component |
US9695696B2 (en) | 2013-07-31 | 2017-07-04 | General Electric Company | Turbine blade with sectioned pins |
US10427213B2 (en) | 2013-07-31 | 2019-10-01 | General Electric Company | Turbine blade with sectioned pins and method of making same |
US9132476B2 (en) * | 2013-10-31 | 2015-09-15 | Siemens Aktiengesellschaft | Multi-wall gas turbine airfoil cast using a ceramic core formed with a fugitive insert and method of manufacturing same |
WO2015126488A2 (en) * | 2013-12-23 | 2015-08-27 | United Technologies Corporation | Lost core structural frame |
US10022790B2 (en) | 2014-06-18 | 2018-07-17 | Siemens Aktiengesellschaft | Turbine airfoil cooling system with leading edge impingement cooling system turbine blade investment casting using film hole protrusions for integral wall thickness control |
US10337353B2 (en) * | 2014-12-31 | 2019-07-02 | General Electric Company | Casing ring assembly with flowpath conduction cut |
US20160298462A1 (en) * | 2015-04-09 | 2016-10-13 | United Technologies Corporation | Cooling passages for a gas turbine engine component |
GB201508795D0 (en) * | 2015-05-22 | 2015-07-01 | Rolls Royce Plc | Cooling of turbine blades |
US9845728B2 (en) | 2015-10-15 | 2017-12-19 | Rohr, Inc. | Forming a nacelle inlet for a turbine engine propulsion system |
US10307816B2 (en) | 2015-10-26 | 2019-06-04 | United Technologies Corporation | Additively manufactured core for use in casting an internal cooling circuit of a gas turbine engine component |
US10226812B2 (en) | 2015-12-21 | 2019-03-12 | United Technologies Corporation | Additively manufactured core for use in casting an internal cooling circuit of a gas turbine engine component |
CN107913980B (zh) * | 2016-10-11 | 2024-05-17 | 北京航空材料研究院股份有限公司 | 弯管模具 |
US10465527B2 (en) * | 2016-11-17 | 2019-11-05 | General Electric Company | Support for a multi-wall core |
US20180161859A1 (en) * | 2016-12-13 | 2018-06-14 | General Electric Company | Integrated casting core-shell structure for making cast component with non-linear holes |
US20180161857A1 (en) * | 2016-12-13 | 2018-06-14 | General Electric Company | Integrated casting core-shell structure for making cast components having thin root components |
US11813669B2 (en) | 2016-12-13 | 2023-11-14 | General Electric Company | Method for making an integrated core-shell structure |
US20180161854A1 (en) * | 2016-12-13 | 2018-06-14 | General Electric Company | Integrated casting core-shell structure |
US20180161866A1 (en) * | 2016-12-13 | 2018-06-14 | General Electric Company | Multi-piece integrated core-shell structure for making cast component |
US20180161852A1 (en) * | 2016-12-13 | 2018-06-14 | General Electric Company | Integrated casting core-shell structure with printed tubes for making cast component |
GB201701365D0 (en) * | 2017-01-27 | 2017-03-15 | Rolls Royce Plc | A ceramic core for an investment casting process |
DE102017106775A1 (de) * | 2017-03-29 | 2018-10-04 | Nemak, S.A.B. De C.V. | Gießkern und Verfahren zu seiner Herstellung |
US10391670B2 (en) | 2017-06-28 | 2019-08-27 | General Electric Company | Additively manufactured integrated casting core structure with ceramic shell |
US10391549B2 (en) | 2017-06-28 | 2019-08-27 | General Electric Company | Additively manufactured casting core-shell hybrid mold and ceramic shell |
US10974312B2 (en) | 2017-06-28 | 2021-04-13 | General Electric Company | Additively manufactured casting core-shell mold with integrated filter and ceramic shell |
US11173542B2 (en) | 2017-06-28 | 2021-11-16 | General Electric Company | Additively manufactured casting core-shell mold and ceramic shell with variable thermal properties |
US11192172B2 (en) | 2017-06-28 | 2021-12-07 | General Electric Company | Additively manufactured interlocking casting core structure with ceramic shell |
US20190111472A1 (en) * | 2017-10-18 | 2019-04-18 | General Electric Company | High temperature engineering stiffness core-shell mold for casting |
US20190375000A1 (en) * | 2018-06-11 | 2019-12-12 | United Technologies Corporation | Method for casting cooling holes for an internal cooling circuit of a gas turbine engine component |
US11433990B2 (en) | 2018-07-09 | 2022-09-06 | Rohr, Inc. | Active laminar flow control system with composite panel |
US11642720B2 (en) * | 2019-10-16 | 2023-05-09 | Raytheon Technologies Corporation | Integral core bumpers |
US11203058B2 (en) | 2019-11-22 | 2021-12-21 | Raytheon Technologies Corporation | Turbine blade casting with strongback core |
US11685123B2 (en) | 2020-12-01 | 2023-06-27 | Raytheon Technologies Corporation | Erodible support structure for additively manufactured article and process therefor |
Family Cites Families (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3596703A (en) * | 1968-10-01 | 1971-08-03 | Trw Inc | Method of preventing core shift in casting articles |
US3604884A (en) | 1969-04-24 | 1971-09-14 | Essar Corp | Electrode feed control for edm machine |
US3957104A (en) | 1974-02-27 | 1976-05-18 | The United States Of America As Represented By The Administrator Of The United States National Aeronautics And Space Administration | Method of making an apertured casting |
US4197443A (en) | 1977-09-19 | 1980-04-08 | General Electric Company | Method and apparatus for forming diffused cooling holes in an airfoil |
EP0084234A1 (de) * | 1981-12-16 | 1983-07-27 | Vickers Plc | Feingiessverfahren und Form |
GB2150875B (en) | 1983-12-07 | 1986-07-02 | Rolls Royce | Investment casting |
US4922076A (en) | 1987-06-01 | 1990-05-01 | Technical Manufacturing Systems, Inc. | Electro-discharge machining electrode |
US4819325A (en) | 1987-06-01 | 1989-04-11 | Technical Manufacturing Systems, Inc. | Method of forming electro-discharge machining electrode |
US5296308A (en) * | 1992-08-10 | 1994-03-22 | Howmet Corporation | Investment casting using core with integral wall thickness control means |
US5382133A (en) | 1993-10-15 | 1995-01-17 | United Technologies Corporation | High coverage shaped diffuser film hole for thin walls |
US5605639A (en) | 1993-12-21 | 1997-02-25 | United Technologies Corporation | Method of producing diffusion holes in turbine components by a multiple piece electrode |
US5637239A (en) | 1995-03-31 | 1997-06-10 | United Technologies Corporation | Curved electrode and method for electrical discharge machining curved cooling holes |
US5735335A (en) * | 1995-07-11 | 1998-04-07 | Extrude Hone Corporation | Investment casting molds and cores |
AU3631297A (en) * | 1997-07-11 | 1999-02-08 | Gyorgy Kecskes | Trash container, waste collecting vehicle, and indoor trash bin for collecting waste materials selectively |
US6003754A (en) * | 1997-10-21 | 1999-12-21 | Allison Advanced Development Co. | Airfoil for a gas turbine engine and method of manufacture |
DE19821770C1 (de) * | 1998-05-14 | 1999-04-15 | Siemens Ag | Verfahren und Vorrichtung zur Herstellung eines metallischen Hohlkörpers |
GB0114503D0 (en) * | 2001-06-14 | 2001-08-08 | Rolls Royce Plc | Air cooled aerofoil |
US6595748B2 (en) * | 2001-08-02 | 2003-07-22 | General Electric Company | Trichannel airfoil leading edge cooling |
US6637500B2 (en) | 2001-10-24 | 2003-10-28 | United Technologies Corporation | Cores for use in precision investment casting |
US6556411B1 (en) * | 2002-04-02 | 2003-04-29 | Marconi Communications, Inc. | Purge protection cartridge with three-way attachment clip |
US6668906B2 (en) | 2002-04-29 | 2003-12-30 | United Technologies Corporation | Shaped core for cast cooling passages and enhanced part definition |
US6705831B2 (en) | 2002-06-19 | 2004-03-16 | United Technologies Corporation | Linked, manufacturable, non-plugging microcircuits |
US20050087319A1 (en) * | 2003-10-16 | 2005-04-28 | Beals James T. | Refractory metal core wall thickness control |
US7124546B2 (en) * | 2003-11-18 | 2006-10-24 | Pella Corporation | Muntin bar connector with positioning tabs |
US7172012B1 (en) * | 2004-07-14 | 2007-02-06 | United Technologies Corporation | Investment casting |
-
2004
- 2004-07-14 US US10/891,660 patent/US7172012B1/en active Active
-
2005
- 2005-06-30 KR KR1020050057416A patent/KR100686658B1/ko not_active IP Right Cessation
- 2005-07-11 JP JP2005201148A patent/JP2006026742A/ja active Pending
- 2005-07-14 EP EP05254403A patent/EP1616642B1/de not_active Not-in-force
- 2005-07-14 AT AT05254403T patent/ATE524255T1/de not_active IP Right Cessation
-
2006
- 2006-01-17 US US11/333,967 patent/US7520312B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
US7520312B2 (en) | 2009-04-21 |
KR100686658B1 (ko) | 2007-02-26 |
EP1616642A1 (de) | 2006-01-18 |
JP2006026742A (ja) | 2006-02-02 |
EP1616642B1 (de) | 2011-09-14 |
KR20060048724A (ko) | 2006-05-18 |
US20080006384A1 (en) | 2008-01-10 |
US7172012B1 (en) | 2007-02-06 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |