IL81063A - Film cooling slot with metered flow - Google Patents

Film cooling slot with metered flow

Info

Publication number
IL81063A
IL81063A IL81063A IL8106386A IL81063A IL 81063 A IL81063 A IL 81063A IL 81063 A IL81063 A IL 81063A IL 8106386 A IL8106386 A IL 8106386A IL 81063 A IL81063 A IL 81063A
Authority
IL
Israel
Prior art keywords
film cooling
metered flow
cooling slot
slot
metered
Prior art date
Application number
IL81063A
Other languages
English (en)
Other versions
IL81063A0 (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 IL81063A0 publication Critical patent/IL81063A0/xx
Publication of IL81063A publication Critical patent/IL81063A/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
    • F05D2240/00Components
    • F05D2240/80Platforms for stationary or moving blades
    • F05D2240/81Cooled platforms
    • 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)
IL81063A 1985-12-23 1986-12-22 Film cooling slot with metered flow IL81063A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/812,100 US4726735A (en) 1985-12-23 1985-12-23 Film cooling slot with metered flow

Publications (2)

Publication Number Publication Date
IL81063A0 IL81063A0 (en) 1987-03-31
IL81063A true IL81063A (en) 1991-06-10

Family

ID=25208502

Family Applications (1)

Application Number Title Priority Date Filing Date
IL81063A IL81063A (en) 1985-12-23 1986-12-22 Film cooling slot with metered flow

Country Status (8)

Country Link
US (1) US4726735A (xx)
EP (1) EP0227578B1 (xx)
JP (1) JPS62165502A (xx)
CN (1) CN1008291B (xx)
AU (1) AU593309B2 (xx)
CA (1) CA1274180A (xx)
DE (2) DE227578T1 (xx)
IL (1) IL81063A (xx)

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US8113784B2 (en) * 2009-03-20 2012-02-14 Hamilton Sundstrand Corporation Coolable airfoil attachment section
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US8573938B1 (en) * 2010-11-22 2013-11-05 Florida Turbine Technologies, Inc. Turbine vane with endwall film cooling
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US9790801B2 (en) 2012-12-27 2017-10-17 United Technologies Corporation Gas turbine engine component having suction side cutback opening
EP2956646B1 (en) * 2013-02-15 2020-10-28 United Technologies Corporation Component for a gas turbine engine and corresponding method of forming a cooling hole
US9593590B2 (en) 2013-03-01 2017-03-14 Siemens Energy, Inc. Active bypass flow control for a seal in a gas turbine engine
EP2971667B1 (en) * 2013-03-15 2024-06-12 RTX Corporation Component for a gas turbine engine and method of manufacturing a component for a gas turbine engine
EP3017148A1 (en) * 2013-07-03 2016-05-11 General Electric Company Trench cooling of airfoil structures
US9528380B2 (en) * 2013-12-18 2016-12-27 General Electric Company Turbine bucket and method for cooling a turbine bucket of a gas turbine engine
US9957814B2 (en) 2014-09-04 2018-05-01 United Technologies Corporation Gas turbine engine component with film cooling hole with accumulator
US20160090843A1 (en) * 2014-09-30 2016-03-31 General Electric Company Turbine components with stepped apertures
US10247011B2 (en) * 2014-12-15 2019-04-02 United Technologies Corporation Gas turbine engine component with increased cooling capacity
EP3124746B1 (en) 2015-07-29 2018-12-26 Ansaldo Energia IP UK Limited Method for cooling a turbo-engine component and turbo-engine component
EP3124745B1 (en) 2015-07-29 2018-03-28 Ansaldo Energia IP UK Limited Turbo-engine component with film cooled wall
DE102016204824A1 (de) 2016-03-23 2017-09-28 Siemens Aktiengesellschaft Filmkühllöcher in Gasturbinen - Bauteilen
US10605091B2 (en) * 2016-06-28 2020-03-31 General Electric Company Airfoil with cast features and method of manufacture
US11401818B2 (en) 2018-08-06 2022-08-02 General Electric Company Turbomachine cooling trench
US10767492B2 (en) 2018-12-18 2020-09-08 General Electric Company Turbine engine airfoil
US11566527B2 (en) 2018-12-18 2023-01-31 General Electric Company Turbine engine airfoil and method of cooling
US11352889B2 (en) 2018-12-18 2022-06-07 General Electric Company Airfoil tip rail and method of cooling
US11499433B2 (en) 2018-12-18 2022-11-15 General Electric Company Turbine engine component and method of cooling
US11174736B2 (en) 2018-12-18 2021-11-16 General Electric Company Method of forming an additively manufactured component
US10844728B2 (en) 2019-04-17 2020-11-24 General Electric Company Turbine engine airfoil with a trailing edge
US11339667B2 (en) 2020-08-11 2022-05-24 Raytheon Technologies Corporation Cooling arrangement including overlapping diffusers
US11560803B1 (en) * 2021-11-05 2023-01-24 General Electric Company Component with cooling passage for a turbine engine

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Also Published As

Publication number Publication date
IL81063A0 (en) 1987-03-31
AU593309B2 (en) 1990-02-08
EP0227578A3 (en) 1989-04-12
DE3683742D1 (de) 1992-03-12
CN86108718A (zh) 1987-07-08
DE227578T1 (de) 1987-12-17
US4726735A (en) 1988-02-23
EP0227578B1 (en) 1992-01-29
JPS62165502A (ja) 1987-07-22
CN1008291B (zh) 1990-06-06
CA1274180A (en) 1990-09-18
AU6668086A (en) 1987-06-25
EP0227578A2 (en) 1987-07-01

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