UA77274C2 - Casting system for producing components of gas turbine engine (variants) and core made of refractory metal (variants) - Google Patents

Casting system for producing components of gas turbine engine (variants) and core made of refractory metal (variants) Download PDF

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Publication number
UA77274C2
UA77274C2 UA20041008187A UA20041008187A UA77274C2 UA 77274 C2 UA77274 C2 UA 77274C2 UA 20041008187 A UA20041008187 A UA 20041008187A UA 20041008187 A UA20041008187 A UA 20041008187A UA 77274 C2 UA77274 C2 UA 77274C2
Authority
UA
Ukraine
Prior art keywords
refractory metal
casting
metal
rod
refractory
Prior art date
Application number
UA20041008187A
Other languages
English (en)
Ukrainian (uk)
Inventor
Dilip M Shakh
Original Assignee
United Technologies Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by United Technologies Corp filed Critical United Technologies Corp
Publication of UA77274C2 publication Critical patent/UA77274C2/uk

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C9/00Moulds or cores; Moulding processes
    • B22C9/10Cores; Manufacture or installation of cores
    • AHUMAN NECESSITIES
    • A01AGRICULTURE; FORESTRY; ANIMAL HUSBANDRY; HUNTING; TRAPPING; FISHING
    • A01KANIMAL HUSBANDRY; AVICULTURE; APICULTURE; PISCICULTURE; FISHING; REARING OR BREEDING ANIMALS, NOT OTHERWISE PROVIDED FOR; NEW BREEDS OF ANIMALS
    • A01K87/00Fishing rods
    • A01K87/02Connecting devices for parts of the rods
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C9/00Moulds or cores; Moulding processes
    • B22C9/02Sand moulds or like moulds for shaped castings
    • B22C9/04Use 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)
UA20041008187A 2003-10-15 2004-10-08 Casting system for producing components of gas turbine engine (variants) and core made of refractory metal (variants) UA77274C2 (en)

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
UA77274C2 true UA77274C2 (en) 2006-11-15

Family

ID=34377625

Family Applications (1)

Application Number Title Priority Date Filing Date
UA20041008187A UA77274C2 (en) 2003-10-15 2004-10-08 Casting system for producing components of gas turbine engine (variants) and core made of refractory metal (variants)

Country Status (11)

Country Link
US (1) US6913064B2 (de)
EP (3) EP1524046B1 (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)

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RU2687949C2 (ru) * 2014-07-04 2019-05-16 Сафран Эркрафт Энджинз Способ изготовления двухкомпонентной лопасти для газотурбинного двигателя и лопасть, получаемая таким способом

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US10443425B2 (en) 2014-02-14 2019-10-15 United Technologies Corporation Blade outer air seal fin cooling assembly and method
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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
US10323524B2 (en) 2015-05-08 2019-06-18 United Technologies Corporation Axial skin core cooling passage for a turbine engine component
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
US10041890B2 (en) * 2015-08-04 2018-08-07 United Technologies Corporation Radiopaque protective fill for manufacture, repair, or remanufacture of cooled components
US9579714B1 (en) 2015-12-17 2017-02-28 General Electric Company Method and assembly for forming components having internal passages using a lattice structure
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
US10099283B2 (en) 2015-12-17 2018-10-16 General Electric Company Method and assembly for forming components having an internal passage defined therein
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
US10046389B2 (en) 2015-12-17 2018-08-14 General Electric Company Method and assembly for forming components having internal passages using a jacketed core
US10099284B2 (en) 2015-12-17 2018-10-16 General Electric Company Method and assembly for forming components having a catalyzed 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
US10150158B2 (en) * 2015-12-17 2018-12-11 General Electric Company Method and assembly for forming components having internal passages using a jacketed core
US10137499B2 (en) 2015-12-17 2018-11-27 General Electric Company Method and assembly for forming components having an internal passage defined therein
US10118217B2 (en) 2015-12-17 2018-11-06 General Electric Company Method and assembly for forming components having internal passages using a jacketed core
US10815827B2 (en) 2016-01-25 2020-10-27 Raytheon Technologies Corporation Variable thickness core for gas turbine engine component
US10286450B2 (en) 2016-04-27 2019-05-14 General Electric Company Method and assembly for forming components using a jacketed core
US10335853B2 (en) 2016-04-27 2019-07-02 General Electric Company Method and assembly for forming components using a jacketed core
US10323569B2 (en) * 2016-05-20 2019-06-18 United Technologies Corporation Core assemblies and gas turbine engine components formed therefrom
US20170335692A1 (en) * 2016-05-20 2017-11-23 United Technologies Corporation Refractory metal core and components formed thereby
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
US11813669B2 (en) 2016-12-13 2023-11-14 General Electric Company Method for making an integrated core-shell structure
US20180161866A1 (en) * 2016-12-13 2018-06-14 General Electric Company Multi-piece integrated core-shell structure for making cast component
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
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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2687949C2 (ru) * 2014-07-04 2019-05-16 Сафран Эркрафт Энджинз Способ изготовления двухкомпонентной лопасти для газотурбинного двигателя и лопасть, получаемая таким способом

Also Published As

Publication number Publication date
CN1607052A (zh) 2005-04-20
JP2005118882A (ja) 2005-05-12
DE602004019613D1 (de) 2009-04-09
US20050098296A1 (en) 2005-05-12
RU2004129949A (ru) 2006-04-10
EP1524046B1 (de) 2009-02-25
KR20050036802A (ko) 2005-04-20
CN1315593C (zh) 2007-05-16
ATE423643T1 (de) 2009-03-15
EP2204248A1 (de) 2010-07-07
SG111239A1 (en) 2005-05-30
EP1524046A1 (de) 2005-04-20
EP2060339B1 (de) 2012-04-18
KR20060028457A (ko) 2006-03-29
EP2204248B1 (de) 2016-07-27
CA2484570A1 (en) 2005-04-15
KR20060028455A (ko) 2006-03-29
US6913064B2 (en) 2005-07-05
RU2282520C2 (ru) 2006-08-27
KR20060028456A (ko) 2006-03-29
KR100615489B1 (ko) 2006-08-25
EP2060339A1 (de) 2009-05-20

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