IL81034A - Convergent-divergent film coolant passage - Google Patents

Convergent-divergent film coolant passage

Info

Publication number
IL81034A
IL81034A IL81034A IL8103486A IL81034A IL 81034 A IL81034 A IL 81034A IL 81034 A IL81034 A IL 81034A IL 8103486 A IL8103486 A IL 8103486A IL 81034 A IL81034 A IL 81034A
Authority
IL
Israel
Prior art keywords
convergent
coolant passage
film coolant
divergent film
divergent
Prior art date
Application number
IL81034A
Other languages
English (en)
Other versions
IL81034A0 (en
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 IL81034A0 publication Critical patent/IL81034A0/xx
Publication of IL81034A publication Critical patent/IL81034A/xx

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/18Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/186Film cooling
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/10Two-dimensional
    • F05D2250/12Two-dimensional rectangular
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/10Two-dimensional
    • F05D2250/12Two-dimensional rectangular
    • F05D2250/121Two-dimensional rectangular square
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/30Arrangement of components
    • F05D2250/32Arrangement of components according to their shape
    • F05D2250/323Arrangement of components according to their shape convergent
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/30Arrangement of components
    • F05D2250/32Arrangement of components according to their shape
    • F05D2250/324Arrangement of components according to their shape divergent
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
IL81034A 1985-12-23 1986-12-18 Convergent-divergent film coolant passage IL81034A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/812,092 US4705455A (en) 1985-12-23 1985-12-23 Convergent-divergent film coolant passage

Publications (2)

Publication Number Publication Date
IL81034A0 IL81034A0 (en) 1987-03-31
IL81034A true IL81034A (en) 1992-07-15

Family

ID=25208471

Family Applications (1)

Application Number Title Priority Date Filing Date
IL81034A IL81034A (en) 1985-12-23 1986-12-18 Convergent-divergent film coolant passage

Country Status (6)

Country Link
US (1) US4705455A (ja)
EP (1) EP0230204B1 (ja)
JP (1) JPH07103801B2 (ja)
CA (1) CA1275052A (ja)
DE (2) DE3683753D1 (ja)
IL (1) IL81034A (ja)

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US6602052B2 (en) * 2001-06-20 2003-08-05 Alstom (Switzerland) Ltd Airfoil tip squealer cooling construction
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US7185736B2 (en) * 2003-08-25 2007-03-06 Fisher Controls International Llc. Aerodynamic noise abatement device and method for air-cooled condensing systems
US7223072B2 (en) * 2004-01-27 2007-05-29 Honeywell International, Inc. Gas turbine engine including airfoils having an improved airfoil film cooling configuration and method therefor
JP5039837B2 (ja) * 2005-03-30 2012-10-03 三菱重工業株式会社 ガスタービン用高温部材
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US7563073B1 (en) 2006-10-10 2009-07-21 Florida Turbine Technologies, Inc. Turbine blade with film cooling slot
US7887294B1 (en) 2006-10-13 2011-02-15 Florida Turbine Technologies, Inc. Turbine airfoil with continuous curved diffusion film holes
US7798765B2 (en) * 2007-04-12 2010-09-21 United Technologies Corporation Out-flow margin protection for a gas turbine engine
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US8066484B1 (en) 2007-11-19 2011-11-29 Florida Turbine Technologies, Inc. Film cooling hole for a turbine airfoil
US8128366B2 (en) * 2008-06-06 2012-03-06 United Technologies Corporation Counter-vortex film cooling hole design
US20090304494A1 (en) * 2008-06-06 2009-12-10 United Technologies Corporation Counter-vortex paired film cooling hole design
US8066482B2 (en) * 2008-11-25 2011-11-29 Alstom Technology Ltd. Shaped cooling holes for reduced stress
US9810081B2 (en) 2010-06-11 2017-11-07 Siemens Energy, Inc. Cooled conduit for conveying combustion gases
US8672613B2 (en) 2010-08-31 2014-03-18 General Electric Company Components with conformal curved film holes and methods of manufacture
FR2964731B1 (fr) * 2010-09-09 2015-01-30 Snecma Dispositif d’echange thermique par jet impactant et utilisation d’un tel dispositif
US8591191B1 (en) * 2010-11-22 2013-11-26 Florida Turbine Technologies, Inc. Film cooling hole for turbine airfoil
US9249670B2 (en) * 2011-12-15 2016-02-02 General Electric Company Components with microchannel cooling
US8522558B1 (en) * 2012-02-15 2013-09-03 United Technologies Corporation Multi-lobed cooling hole array
US9279330B2 (en) 2012-02-15 2016-03-08 United Technologies Corporation Gas turbine engine component with converging/diverging cooling passage
BR112014031176A2 (pt) 2012-06-13 2017-06-27 Gen Electric paredes de motor de turbina a gás
US9309771B2 (en) 2012-10-25 2016-04-12 United Technologies Corporation Film cooling channel array with multiple metering portions
US9316104B2 (en) 2012-10-25 2016-04-19 United Technologies Corporation Film cooling channel array having anti-vortex properties
CN107076416B (zh) 2014-08-26 2020-05-19 西门子能源公司 用于燃气涡轮发动机中的声共振器的薄膜冷却孔装置
US20160090843A1 (en) * 2014-09-30 2016-03-31 General Electric Company Turbine components with stepped apertures
CN104747242A (zh) * 2015-03-12 2015-07-01 中国科学院工程热物理研究所 一种离散气膜冷却孔
US20160298462A1 (en) * 2015-04-09 2016-10-13 United Technologies Corporation Cooling passages for a gas turbine engine component
US10010937B2 (en) 2015-11-09 2018-07-03 General Electric Company Additive manufacturing method for making overhanging tabs in cooling holes
US20180171872A1 (en) * 2016-12-15 2018-06-21 General Electric Company Cooling assembly for a turbine assembly
US10760431B2 (en) * 2017-09-07 2020-09-01 General Electric Company Component for a turbine engine with a cooling hole
US20190071977A1 (en) * 2017-09-07 2019-03-07 General Electric Company Component for a turbine engine with a cooling hole
US10539026B2 (en) 2017-09-21 2020-01-21 United Technologies Corporation Gas turbine engine component with cooling holes having variable roughness
US11401818B2 (en) * 2018-08-06 2022-08-02 General Electric Company Turbomachine cooling trench
CN109141542B (zh) * 2018-09-14 2020-04-10 长春工程学院 基于临界水深槽工作原理的矩形渠道无槽量水方法
US10822958B2 (en) * 2019-01-16 2020-11-03 General Electric Company Component for a turbine engine with a cooling hole
US11674686B2 (en) 2021-05-11 2023-06-13 Honeywell International Inc. Coating occlusion resistant effusion cooling holes for gas turbine engine
CN115898554B (zh) * 2023-03-09 2023-06-30 中国航发四川燃气涡轮研究院 涡轮叶片的气膜孔结构

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Also Published As

Publication number Publication date
JPH07103801B2 (ja) 1995-11-08
DE3683753D1 (de) 1992-03-12
EP0230204A2 (en) 1987-07-29
EP0230204A3 (en) 1989-04-12
EP0230204B1 (en) 1992-01-29
IL81034A0 (en) 1987-03-31
CA1275052A (en) 1990-10-09
JPS62162701A (ja) 1987-07-18
DE230204T1 (de) 1987-12-17
US4705455A (en) 1987-11-10

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Legal Events

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