RU2013100413A - Аэродинамический профиль (варианты ) - Google Patents

Аэродинамический профиль (варианты ) Download PDF

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Publication number
RU2013100413A
RU2013100413A RU2013100413/06A RU2013100413A RU2013100413A RU 2013100413 A RU2013100413 A RU 2013100413A RU 2013100413/06 A RU2013100413/06 A RU 2013100413/06A RU 2013100413 A RU2013100413 A RU 2013100413A RU 2013100413 A RU2013100413 A RU 2013100413A
Authority
RU
Russia
Prior art keywords
aerodynamic profile
groove
specified
high pressure
line
Prior art date
Application number
RU2013100413/06A
Other languages
English (en)
Russian (ru)
Inventor
Бенджамин Пол ЛЕЙСИ
Original Assignee
Дженерал Электрик Компани
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 Дженерал Электрик Компани filed Critical Дженерал Электрик Компани
Publication of RU2013100413A publication Critical patent/RU2013100413A/ru

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/186—Film cooling
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/20—Rotors
    • F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • F05D2240/303—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the leading edge of a rotor blade
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/80—Platforms for stationary or moving blades
    • F05D2240/81—Cooled platforms
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/30—Arrangement of components
    • F05D2250/32—Arrangement of components according to their shape
    • F05D2250/324—Arrangement of components according to their shape divergent
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/202—Heat transfer, e.g. cooling by film cooling
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
RU2013100413/06A 2012-01-13 2013-01-10 Аэродинамический профиль (варианты ) RU2013100413A (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/349,852 2012-01-13
US13/349,852 US8870535B2 (en) 2012-01-13 2012-01-13 Airfoil

Publications (1)

Publication Number Publication Date
RU2013100413A true RU2013100413A (ru) 2014-07-20

Family

ID=47561371

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2013100413/06A RU2013100413A (ru) 2012-01-13 2013-01-10 Аэродинамический профиль (варианты )

Country Status (4)

Country Link
US (1) US8870535B2 (enExample)
EP (1) EP2615245B1 (enExample)
JP (1) JP6105942B2 (enExample)
RU (1) RU2013100413A (enExample)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
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US9080451B2 (en) * 2012-06-28 2015-07-14 General Electric Company Airfoil
DE102013109116A1 (de) * 2012-08-27 2014-03-27 General Electric Company (N.D.Ges.D. Staates New York) Bauteil mit Kühlkanälen und Verfahren zur Herstellung
EP2971674B1 (en) * 2013-03-14 2022-10-19 Raytheon Technologies Corporation Gas turbine engine stator vane platform cooling
CN105339593B (zh) * 2013-07-03 2017-10-13 通用电气公司 翼形件结构的沟槽冷却
US20160090843A1 (en) * 2014-09-30 2016-03-31 General Electric Company Turbine components with stepped apertures
EP3043025A1 (de) * 2015-01-09 2016-07-13 Siemens Aktiengesellschaft Filmgekühltes Gasturbinenbauteil
US11933323B2 (en) * 2015-07-23 2024-03-19 Onesubsea Ip Uk Limited Short impeller for a turbomachine
KR101839656B1 (ko) 2015-08-13 2018-04-26 두산중공업 주식회사 가스터빈 블레이드
KR101853550B1 (ko) * 2016-08-22 2018-04-30 두산중공업 주식회사 가스 터빈 블레이드
US20180230812A1 (en) * 2017-01-13 2018-08-16 General Electric Company Film hole arrangement for a turbine engine
US10570747B2 (en) * 2017-10-02 2020-02-25 DOOSAN Heavy Industries Construction Co., LTD Enhanced film cooling system
GB201819064D0 (en) 2018-11-23 2019-01-09 Rolls Royce Aerofoil stagnation zone cooling
US12497896B2 (en) * 2023-05-31 2025-12-16 General Electric Company Airfoil assembly with platform film holes

Family Cites Families (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2613910A (en) * 1947-01-24 1952-10-14 Edward A Stalker Slotted turbine blade
US3515499A (en) * 1968-04-22 1970-06-02 Aerojet General Co Blades and blade assemblies for turbine engines,compressors and the like
GB1209692A (en) * 1968-05-14 1970-10-21 Rolls Royce Method and apparatus for the spark-machining of workpieces and a spark-machining electrode for use therein
US4672727A (en) * 1985-12-23 1987-06-16 United Technologies Corporation Method of fabricating film cooling slot in a hollow airfoil
US5486093A (en) * 1993-09-08 1996-01-23 United Technologies Corporation Leading edge cooling of turbine airfoils
US5374162A (en) 1993-11-30 1994-12-20 United Technologies Corporation Airfoil having coolable leading edge region
US5458461A (en) 1994-12-12 1995-10-17 General Electric Company Film cooled slotted wall
US6050777A (en) * 1997-12-17 2000-04-18 United Technologies Corporation Apparatus and method for cooling an airfoil for a gas turbine engine
US6164912A (en) * 1998-12-21 2000-12-26 United Technologies Corporation Hollow airfoil for a gas turbine engine
US6210111B1 (en) 1998-12-21 2001-04-03 United Technologies Corporation Turbine blade with platform cooling
US6994521B2 (en) * 2003-03-12 2006-02-07 Florida Turbine Technologies, Inc. Leading edge diffusion cooling of a turbine airfoil for a gas turbine engine
US20070141385A1 (en) * 2005-12-21 2007-06-21 General Electric Company Method of coating gas turbine components
US7510367B2 (en) * 2006-08-24 2009-03-31 Siemens Energy, Inc. Turbine airfoil with endwall horseshoe cooling slot
US7553534B2 (en) * 2006-08-29 2009-06-30 General Electric Company Film cooled slotted wall and method of making the same
US7540712B1 (en) * 2006-09-15 2009-06-02 Florida Turbine Technologies, Inc. Turbine airfoil with showerhead cooling holes
US7980819B2 (en) * 2007-03-14 2011-07-19 United Technologies Corporation Cast features for a turbine engine airfoil
US8105030B2 (en) * 2008-08-14 2012-01-31 United Technologies Corporation Cooled airfoils and gas turbine engine systems involving such airfoils
US8092176B2 (en) * 2008-09-16 2012-01-10 Siemens Energy, Inc. Turbine airfoil cooling system with curved diffusion film cooling hole
US8057182B2 (en) * 2008-11-21 2011-11-15 General Electric Company Metered cooling slots for turbine blades
US8109725B2 (en) * 2008-12-15 2012-02-07 United Technologies Corporation Airfoil with wrapped leading edge cooling passage
US20110097188A1 (en) * 2009-10-23 2011-04-28 General Electric Company Structure and method for improving film cooling using shallow trench with holes oriented along length of trench
US8608443B2 (en) * 2010-06-11 2013-12-17 Siemens Energy, Inc. Film cooled component wall in a turbine engine
US8628293B2 (en) * 2010-06-17 2014-01-14 Honeywell International Inc. Gas turbine engine components with cooling hole trenches
JP5636774B2 (ja) * 2010-07-09 2014-12-10 株式会社Ihi タービン翼及びエンジン部品

Also Published As

Publication number Publication date
JP2013144981A (ja) 2013-07-25
US8870535B2 (en) 2014-10-28
CN103206261A (zh) 2013-07-17
EP2615245B1 (en) 2021-08-25
JP6105942B2 (ja) 2017-03-29
EP2615245A3 (en) 2017-08-02
US20130183165A1 (en) 2013-07-18
EP2615245A2 (en) 2013-07-17

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Legal Events

Date Code Title Description
FA92 Acknowledgement of application withdrawn (lack of supplementary materials submitted)

Effective date: 20171109