DE50311059D1 - Gussform - Google Patents
GussformInfo
- Publication number
- DE50311059D1 DE50311059D1 DE50311059T DE50311059T DE50311059D1 DE 50311059 D1 DE50311059 D1 DE 50311059D1 DE 50311059 T DE50311059 T DE 50311059T DE 50311059 T DE50311059 T DE 50311059T DE 50311059 D1 DE50311059 D1 DE 50311059D1
- Authority
- DE
- Germany
- Prior art keywords
- mold
- 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 - Lifetime
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/22—Moulds for peculiarly-shaped castings
- B22C9/24—Moulds for peculiarly-shaped castings for hollow articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
-
- 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
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/10—Cores; Manufacture or installation of cores
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP03024967A EP1529580B1 (de) | 2003-10-29 | 2003-10-29 | Gussform |
Publications (1)
Publication Number | Publication Date |
---|---|
DE50311059D1 true DE50311059D1 (de) | 2009-02-26 |
Family
ID=34429245
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE50311059T Expired - Lifetime DE50311059D1 (de) | 2003-10-29 | 2003-10-29 | Gussform |
Country Status (3)
Country | Link |
---|---|
US (1) | US7237595B2 (de) |
EP (1) | EP1529580B1 (de) |
DE (1) | DE50311059D1 (de) |
Families Citing this family (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7325587B2 (en) * | 2005-08-30 | 2008-02-05 | United Technologies Corporation | Method for casting cooling holes |
US20080005903A1 (en) * | 2006-07-05 | 2008-01-10 | United Technologies Corporation | External datum system and film hole positioning using core locating holes |
US20090000754A1 (en) | 2007-06-27 | 2009-01-01 | United Technologies Corporation | Investment casting cores and methods |
CH700320A1 (de) * | 2009-01-30 | 2010-07-30 | Alstom Technology Ltd | Verfahren zum herstellen eines bauteils einer gasturbine. |
US20110088379A1 (en) * | 2009-10-15 | 2011-04-21 | General Electric Company | Exhaust gas diffuser |
DE102010025678A1 (de) * | 2010-06-30 | 2012-01-05 | Voith Patent Gmbh | Stator und Verfahren zum Herstellen eines Stators |
US9249687B2 (en) | 2010-10-27 | 2016-02-02 | General Electric Company | Turbine exhaust diffusion system and method |
US20130280093A1 (en) | 2012-04-24 | 2013-10-24 | Mark F. Zelesky | Gas turbine engine core providing exterior airfoil portion |
US9957813B2 (en) * | 2013-02-19 | 2018-05-01 | United Technologies Corporation | Gas turbine engine airfoil platform cooling passage and core |
JP6452736B2 (ja) * | 2014-06-18 | 2019-01-16 | シーメンス エナジー インコーポレイテッド | 一体的な壁厚制御のためのフィルム孔突出部を用いるタービンブレードインベストメント鋳造 |
US10118217B2 (en) | 2015-12-17 | 2018-11-06 | General Electric Company | Method and assembly for forming components having internal passages using a jacketed core |
US9968991B2 (en) | 2015-12-17 | 2018-05-15 | General Electric Company | Method and assembly for forming components having internal passages using a lattice structure |
US10099284B2 (en) | 2015-12-17 | 2018-10-16 | General Electric Company | Method and assembly for forming components having a catalyzed internal passage defined therein |
US10137499B2 (en) | 2015-12-17 | 2018-11-27 | General Electric Company | Method and assembly for forming components having an internal passage defined therein |
US9579714B1 (en) | 2015-12-17 | 2017-02-28 | General Electric Company | Method and assembly for forming components having internal passages using a lattice structure |
US9987677B2 (en) | 2015-12-17 | 2018-06-05 | General Electric Company | Method and assembly for forming components having internal passages using a jacketed core |
US10099283B2 (en) | 2015-12-17 | 2018-10-16 | General Electric Company | Method and assembly for forming components having an internal passage defined therein |
US10150158B2 (en) | 2015-12-17 | 2018-12-11 | General Electric Company | Method and assembly for forming components having internal passages using a jacketed core |
US10099276B2 (en) | 2015-12-17 | 2018-10-16 | General Electric Company | Method and assembly for forming components having an internal passage defined therein |
US10046389B2 (en) | 2015-12-17 | 2018-08-14 | General Electric Company | Method and assembly for forming components having internal passages using a jacketed core |
US11090712B2 (en) * | 2016-03-24 | 2021-08-17 | Siemens Energy Global GmbH & Co. KG | Method of manufacturing a hybridized core with protruding cast in cooling features for investment casting |
US10335853B2 (en) | 2016-04-27 | 2019-07-02 | General Electric Company | Method and assembly for forming components using a jacketed core |
US10286450B2 (en) | 2016-04-27 | 2019-05-14 | General Electric Company | Method and assembly for forming components using a jacketed core |
US10830052B2 (en) | 2016-09-15 | 2020-11-10 | Honeywell International Inc. | Gas turbine component with cooling aperture having shaped inlet and method of forming the same |
US10315248B2 (en) | 2016-11-17 | 2019-06-11 | General Electric Company | Methods and apparatuses using cast in core reference features |
US10927705B2 (en) * | 2018-08-17 | 2021-02-23 | Raytheon Technologies Corporation | Method for forming cooling holes having separate complex and simple geometry sections |
US11998974B2 (en) * | 2022-08-30 | 2024-06-04 | General Electric Company | Casting core for a cast engine component |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3646185A (en) * | 1967-03-13 | 1972-02-29 | Irving C Jennings | Method of casting a diffuser element |
FR2731639A1 (de) * | 1976-12-07 | 1996-09-20 | Rolls Royce Plc | |
US4565490A (en) * | 1981-06-17 | 1986-01-21 | Rice Ivan G | Integrated gas/steam nozzle |
US4669957A (en) * | 1985-12-23 | 1987-06-02 | United Technologies Corporation | Film coolant passage with swirl diffuser |
US5295530A (en) * | 1992-02-18 | 1994-03-22 | General Motors Corporation | Single-cast, high-temperature, thin wall structures and methods of making the same |
US5296308A (en) * | 1992-08-10 | 1994-03-22 | Howmet Corporation | Investment casting using core with integral wall thickness control means |
US5465780A (en) * | 1993-11-23 | 1995-11-14 | Alliedsignal Inc. | Laser machining of ceramic cores |
US5623985A (en) * | 1996-03-13 | 1997-04-29 | Pcc Airfoils, Inc. | Apparatus and method for molding an article |
US5609779A (en) * | 1996-05-15 | 1997-03-11 | General Electric Company | Laser drilling of non-circular apertures |
US5950705A (en) * | 1996-12-03 | 1999-09-14 | General Electric Company | Method for casting and controlling wall thickness |
DE19821770C1 (de) * | 1998-05-14 | 1999-04-15 | Siemens Ag | Verfahren und Vorrichtung zur Herstellung eines metallischen Hohlkörpers |
US6340047B1 (en) * | 1999-03-22 | 2002-01-22 | General Electric Company | Core tied cast airfoil |
DE19939179B4 (de) * | 1999-08-20 | 2007-08-02 | Alstom | Kühlbare Schaufel für eine Gasturbine |
DE10053356A1 (de) * | 2000-10-27 | 2002-05-08 | Alstom Switzerland Ltd | Gekühltes Bauteil, Gusskern für die Herstellung eines solchen Bauteils, sowie Verfahren zum Herstellen eines solchen Bauteils |
GB2373319B (en) * | 2001-03-12 | 2005-03-30 | Rolls Royce Plc | Combustion apparatus |
US6932571B2 (en) * | 2003-02-05 | 2005-08-23 | United Technologies Corporation | Microcircuit cooling for a turbine blade tip |
-
2003
- 2003-10-29 EP EP03024967A patent/EP1529580B1/de not_active Expired - Lifetime
- 2003-10-29 DE DE50311059T patent/DE50311059D1/de not_active Expired - Lifetime
-
2004
- 2004-10-28 US US10/977,736 patent/US7237595B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
EP1529580A1 (de) | 2005-05-11 |
US7237595B2 (en) | 2007-07-03 |
US20060032604A1 (en) | 2006-02-16 |
EP1529580B1 (de) | 2009-01-07 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |