DE602004019613D1 - Refraktärmetallkern - Google Patents
RefraktärmetallkernInfo
- Publication number
- DE602004019613D1 DE602004019613D1 DE602004019613T DE602004019613T DE602004019613D1 DE 602004019613 D1 DE602004019613 D1 DE 602004019613D1 DE 602004019613 T DE602004019613 T DE 602004019613T DE 602004019613 T DE602004019613 T DE 602004019613T DE 602004019613 D1 DE602004019613 D1 DE 602004019613D1
- Authority
- DE
- Germany
- Prior art keywords
- forming
- casting system
- refractory metal
- shape
- features
- 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
- 238000005266 casting Methods 0.000 abstract 3
- 239000002184 metal Substances 0.000 abstract 3
- 239000003870 refractory metal Substances 0.000 abstract 3
- 238000001816 cooling Methods 0.000 abstract 1
- 239000000463 material Substances 0.000 abstract 1
Classifications
-
- A—HUMAN NECESSITIES
- A01—AGRICULTURE; FORESTRY; ANIMAL HUSBANDRY; HUNTING; TRAPPING; FISHING
- A01K—ANIMAL HUSBANDRY; AVICULTURE; APICULTURE; PISCICULTURE; FISHING; REARING OR BREEDING ANIMALS, NOT OTHERWISE PROVIDED FOR; NEW BREEDS OF ANIMALS
- A01K87/00—Fishing rods
- A01K87/02—Connecting devices for parts of the rods
-
- 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
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- Environmental Sciences (AREA)
- Marine Sciences & Fisheries (AREA)
- Animal Husbandry (AREA)
- Biodiversity & Conservation Biology (AREA)
- Molds, Cores, And Manufacturing Methods Thereof (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Transition And Organic Metals Composition Catalysts For Addition Polymerization (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/685,632 US6913064B2 (en) | 2003-10-15 | 2003-10-15 | Refractory metal core |
Publications (1)
Publication Number | Publication Date |
---|---|
DE602004019613D1 true DE602004019613D1 (de) | 2009-04-09 |
Family
ID=34377625
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE602004019613T Expired - Lifetime DE602004019613D1 (de) | 2003-10-15 | 2004-10-15 | Refraktärmetallkern |
Country Status (11)
Country | Link |
---|---|
US (1) | US6913064B2 (de) |
EP (3) | EP2204248B1 (de) |
JP (1) | JP2005118882A (de) |
KR (4) | KR100615489B1 (de) |
CN (1) | CN1315593C (de) |
AT (1) | ATE423643T1 (de) |
CA (1) | CA2484570A1 (de) |
DE (1) | DE602004019613D1 (de) |
RU (1) | RU2282520C2 (de) |
SG (1) | SG111239A1 (de) |
UA (1) | UA77274C2 (de) |
Families Citing this family (58)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7306026B2 (en) * | 2005-09-01 | 2007-12-11 | United Technologies Corporation | Cooled turbine airfoils and methods of manufacture |
US7686065B2 (en) * | 2006-05-15 | 2010-03-30 | United Technologies Corporation | Investment casting core assembly |
US8434997B2 (en) * | 2007-08-22 | 2013-05-07 | United Technologies Corporation | Gas turbine engine case for clearance control |
US7942188B2 (en) * | 2008-03-12 | 2011-05-17 | Vent-Tek Designs, Llc | Refractory metal core |
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 |
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 |
US8347947B2 (en) * | 2009-02-17 | 2013-01-08 | United Technologies Corporation | Process and refractory metal core for creating varying thickness microcircuits for turbine engine components |
US20110135446A1 (en) * | 2009-12-04 | 2011-06-09 | United Technologies Corporation | Castings, Casting Cores, and Methods |
US8914976B2 (en) * | 2010-04-01 | 2014-12-23 | Siemens Energy, Inc. | Turbine airfoil to shroud attachment method |
US8807198B2 (en) | 2010-11-05 | 2014-08-19 | United Technologies Corporation | Die casting system and method utilizing sacrificial core |
US9057523B2 (en) | 2011-07-29 | 2015-06-16 | United Technologies Corporation | Microcircuit cooling for gas turbine engine combustor |
US9260191B2 (en) * | 2011-08-26 | 2016-02-16 | Hs Marston Aerospace Ltd. | Heat exhanger apparatus including heat transfer surfaces |
US9925584B2 (en) | 2011-09-29 | 2018-03-27 | United Technologies Corporation | Method and system for die casting a hybrid component |
US9404654B2 (en) * | 2012-09-26 | 2016-08-02 | United Technologies Corporation | Gas turbine engine combustor with integrated combustor vane |
US9120144B2 (en) * | 2013-02-06 | 2015-09-01 | Siemens Aktiengesellschaft | Casting core for twisted gas turbine engine airfoil having a twisted rib |
CN103240391B (zh) * | 2013-04-25 | 2015-05-27 | 西安西工大超晶科技发展有限责任公司 | 熔模铸造用金属芯的制备方法和基于该金属芯的铝合金铸件的熔模精密铸造方法 |
US10005123B2 (en) * | 2013-10-24 | 2018-06-26 | United Technologies Corporation | Lost core molding cores for forming cooling passages |
EP3105422B1 (de) | 2014-02-14 | 2020-06-10 | United Technologies Corporation | Äussere schaufelluftdichtungsrippenkühlanordnung und verfahren |
US10329916B2 (en) | 2014-05-01 | 2019-06-25 | United Technologies Corporation | Splayed tip features for gas turbine engine airfoil |
FR3023317B1 (fr) * | 2014-07-04 | 2016-08-05 | Snecma | Procede de fabrication d'une aube bi-composant pour moteur a turbine a gaz et aube obtenue par un tel procede |
US10307817B2 (en) | 2014-10-31 | 2019-06-04 | United Technologies Corporation | Additively manufactured casting articles for manufacturing gas turbine engine parts |
US10040115B2 (en) | 2014-10-31 | 2018-08-07 | United Technologies Corporation | Additively manufactured casting articles for manufacturing gas turbine engine parts |
US10507515B2 (en) | 2014-12-15 | 2019-12-17 | United Technologies Corporation | Ceramic core for component casting |
US9988910B2 (en) | 2015-01-30 | 2018-06-05 | United Technologies Corporation | Staggered core printout |
US10502066B2 (en) | 2015-05-08 | 2019-12-10 | United Technologies Corporation | Turbine engine component including an axially aligned skin core passage interrupted by a pedestal |
US10323524B2 (en) | 2015-05-08 | 2019-06-18 | United Technologies Corporation | Axial skin core cooling passage for a turbine engine component |
US10041890B2 (en) * | 2015-08-04 | 2018-08-07 | United Technologies Corporation | Radiopaque protective fill for manufacture, repair, or remanufacture of cooled components |
US10099283B2 (en) | 2015-12-17 | 2018-10-16 | General Electric Company | Method and assembly for forming components having an internal passage defined therein |
US10099276B2 (en) | 2015-12-17 | 2018-10-16 | General Electric Company | Method and assembly for forming components having an internal passage defined therein |
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 |
US10046389B2 (en) | 2015-12-17 | 2018-08-14 | General Electric Company | Method and assembly for forming components having internal passages using a jacketed core |
CN106890945A (zh) * | 2015-12-17 | 2017-06-27 | 通用电气公司 | 模芯组件及熔模铸造方法 |
US9987677B2 (en) | 2015-12-17 | 2018-06-05 | 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 |
US10150158B2 (en) * | 2015-12-17 | 2018-12-11 | General Electric Company | Method and assembly for forming components having internal passages using a jacketed core |
US10118217B2 (en) | 2015-12-17 | 2018-11-06 | General Electric Company | Method and assembly for forming components having internal passages using a jacketed core |
US9579714B1 (en) | 2015-12-17 | 2017-02-28 | General Electric Company | Method and assembly for forming components having internal passages using a lattice structure |
US10815827B2 (en) | 2016-01-25 | 2020-10-27 | Raytheon Technologies Corporation | Variable thickness core for gas turbine engine component |
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 |
US20170335692A1 (en) * | 2016-05-20 | 2017-11-23 | United Technologies Corporation | Refractory metal core and components formed thereby |
US10323569B2 (en) * | 2016-05-20 | 2019-06-18 | United Technologies Corporation | Core assemblies and gas turbine engine components formed therefrom |
CN105921833A (zh) * | 2016-06-01 | 2016-09-07 | 李庆 | 一种去除合金模芯的电解液及去除合金模芯的方法 |
US20180161866A1 (en) * | 2016-12-13 | 2018-06-14 | General Electric Company | Multi-piece integrated core-shell structure for making cast component |
US11813669B2 (en) | 2016-12-13 | 2023-11-14 | General Electric Company | Method for making an integrated core-shell structure |
US10443403B2 (en) | 2017-01-23 | 2019-10-15 | General Electric Company | Investment casting core |
US10596621B1 (en) * | 2017-03-29 | 2020-03-24 | United Technologies Corporation | Method of making complex internal passages in turbine airfoils |
US10556269B1 (en) * | 2017-03-29 | 2020-02-11 | United Technologies Corporation | Apparatus for and method of making multi-walled passages in components |
KR101959751B1 (ko) | 2017-10-13 | 2019-03-19 | 서울대학교 산학협력단 | 항복강도 온도 항상성을 가진 내화성 합금재료 |
US10953461B2 (en) | 2019-03-21 | 2021-03-23 | Raytheon Technologies Corporation | Investment casting method including forming of investment casting core |
CN110948182B (zh) * | 2019-11-11 | 2024-06-11 | 中国航天空气动力技术研究院 | 一种难熔金属毛细芯的成型方法 |
US11654476B2 (en) * | 2020-09-28 | 2023-05-23 | GM Global Technology Operations LLC | Hybrid core for manufacturing of castings |
CN114226643B (zh) * | 2021-12-27 | 2023-05-12 | 洛阳科品钛业股份有限公司 | 一种防止下横臂零件生产过程中型壳胀壳的脱蜡方法 |
US20240218828A1 (en) | 2022-11-01 | 2024-07-04 | General Electric Company | Gas Turbine Engine |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
GB1545584A (en) * | 1975-03-07 | 1979-05-10 | Onera (Off Nat Aerospatiale) | Processes and systems for the formation of surface diffusion alloys on perforate metal workpieces |
IT1096996B (it) * | 1977-07-22 | 1985-08-26 | Rolls Royce | Metodo per la fabbricazione di una pala o lama per motori a turbina a gas |
DE2945531C2 (de) * | 1979-11-10 | 1982-01-07 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Turboschaufel mit einem Matellkern und einem Keramikblatt |
EP0084234A1 (de) * | 1981-12-16 | 1983-07-27 | Vickers Plc | Feingiessverfahren und Form |
GB2126931B (en) * | 1982-09-04 | 1986-04-23 | Rolls Royce | Dissolving ceramic materials |
GB2199822B (en) * | 1987-01-17 | 1990-10-10 | Rolls Royce Plc | Ceramic core material and method of enhancing its leaching rate. |
US5405242A (en) * | 1990-07-09 | 1995-04-11 | United Technologies Corporation | Cooled vane |
US5640767A (en) * | 1995-01-03 | 1997-06-24 | Gen Electric | Method for making a double-wall airfoil |
JP3647612B2 (ja) * | 1997-07-24 | 2005-05-18 | 富士重工業株式会社 | 航空機の前縁構造及びその製造方法 |
JPH1157943A (ja) * | 1997-08-25 | 1999-03-02 | Ebara Corp | ハニカム構造体の製造方法 |
US6190133B1 (en) * | 1998-08-14 | 2001-02-20 | Allison Engine Company | High stiffness airoil and method of manufacture |
US6637500B2 (en) | 2001-10-24 | 2003-10-28 | United Technologies Corporation | Cores for use in precision investment casting |
US6668906B2 (en) * | 2002-04-29 | 2003-12-30 | United Technologies Corporation | Shaped core for cast cooling passages and enhanced part definition |
-
2003
- 2003-10-15 US US10/685,632 patent/US6913064B2/en not_active Expired - Lifetime
-
2004
- 2004-10-08 UA UA20041008187A patent/UA77274C2/uk unknown
- 2004-10-13 CA CA002484570A patent/CA2484570A1/en not_active Abandoned
- 2004-10-14 CN CNB2004100880597A patent/CN1315593C/zh not_active Expired - Fee Related
- 2004-10-14 SG SG200406155A patent/SG111239A1/en unknown
- 2004-10-15 AT AT04256374T patent/ATE423643T1/de not_active IP Right Cessation
- 2004-10-15 EP EP10003446.1A patent/EP2204248B1/de not_active Expired - Lifetime
- 2004-10-15 JP JP2004301078A patent/JP2005118882A/ja active Pending
- 2004-10-15 KR KR1020040082400A patent/KR100615489B1/ko not_active IP Right Cessation
- 2004-10-15 RU RU2004129949/02A patent/RU2282520C2/ru not_active IP Right Cessation
- 2004-10-15 EP EP09001971A patent/EP2060339B1/de not_active Expired - Lifetime
- 2004-10-15 EP EP04256374A patent/EP1524046B1/de not_active Expired - Lifetime
- 2004-10-15 DE DE602004019613T patent/DE602004019613D1/de not_active Expired - Lifetime
-
2006
- 2006-03-08 KR KR1020060021655A patent/KR20060028457A/ko not_active Application Discontinuation
- 2006-03-08 KR KR1020060021652A patent/KR20060028455A/ko not_active Application Discontinuation
- 2006-03-08 KR KR1020060021654A patent/KR20060028456A/ko not_active Application Discontinuation
Also Published As
Publication number | Publication date |
---|---|
EP2204248B1 (de) | 2016-07-27 |
RU2004129949A (ru) | 2006-04-10 |
EP2204248A1 (de) | 2010-07-07 |
EP1524046A1 (de) | 2005-04-20 |
US6913064B2 (en) | 2005-07-05 |
EP2060339A1 (de) | 2009-05-20 |
KR20050036802A (ko) | 2005-04-20 |
KR20060028456A (ko) | 2006-03-29 |
CN1607052A (zh) | 2005-04-20 |
KR100615489B1 (ko) | 2006-08-25 |
EP2060339B1 (de) | 2012-04-18 |
CA2484570A1 (en) | 2005-04-15 |
UA77274C2 (en) | 2006-11-15 |
SG111239A1 (en) | 2005-05-30 |
US20050098296A1 (en) | 2005-05-12 |
KR20060028457A (ko) | 2006-03-29 |
RU2282520C2 (ru) | 2006-08-27 |
EP1524046B1 (de) | 2009-02-25 |
KR20060028455A (ko) | 2006-03-29 |
JP2005118882A (ja) | 2005-05-12 |
CN1315593C (zh) | 2007-05-16 |
ATE423643T1 (de) | 2009-03-15 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |