IT1048628B - Paletta direttrice per turbine a gas - Google Patents

Paletta direttrice per turbine a gas

Info

Publication number
IT1048628B
IT1048628B IT29100/75A IT2910075A IT1048628B IT 1048628 B IT1048628 B IT 1048628B IT 29100/75 A IT29100/75 A IT 29100/75A IT 2910075 A IT2910075 A IT 2910075A IT 1048628 B IT1048628 B IT 1048628B
Authority
IT
Italy
Prior art keywords
gas turbines
directing vane
vane
directing
turbines
Prior art date
Application number
IT29100/75A
Other languages
English (en)
Original Assignee
Bbc Sulzer Turbomaschinen
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 Bbc Sulzer Turbomaschinen filed Critical Bbc Sulzer Turbomaschinen
Application granted granted Critical
Publication of IT1048628B publication Critical patent/IT1048628B/it

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
    • F01D5/187—Convection cooling
    • F01D5/188—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall
    • F01D5/189—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall the insert having a tubular cross-section, e.g. airfoil shape
    • 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
    • F05D2260/201—Heat transfer, e.g. cooling by impingement of a fluid

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Control Of Turbines (AREA)
IT29100/75A 1974-11-08 1975-11-07 Paletta direttrice per turbine a gas IT1048628B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH1495274A CH584347A5 (it) 1974-11-08 1974-11-08

Publications (1)

Publication Number Publication Date
IT1048628B true IT1048628B (it) 1980-12-20

Family

ID=4405143

Family Applications (1)

Application Number Title Priority Date Filing Date
IT29100/75A IT1048628B (it) 1974-11-08 1975-11-07 Paletta direttrice per turbine a gas

Country Status (7)

Country Link
US (1) US4021139A (it)
JP (1) JPS554932B2 (it)
CH (1) CH584347A5 (it)
FR (1) FR2290569A1 (it)
GB (1) GB1489098A (it)
IT (1) IT1048628B (it)
NO (1) NO145962C (it)

Families Citing this family (41)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE395934B (sv) * 1976-01-19 1977-08-29 Stal Laval Turbin Ab Kyld-ihalig ledskovel for gasturbin
GB1565361A (en) * 1976-01-29 1980-04-16 Rolls Royce Blade or vane for a gas turbine engien
US4303374A (en) * 1978-12-15 1981-12-01 General Electric Company Film cooled airfoil body
US4384823A (en) * 1980-10-27 1983-05-24 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Curved film cooling admission tube
JPS5874952A (ja) * 1981-10-29 1983-05-06 Honda Motor Co Ltd 変速機における最終駆動軸用軸受の支持及び封絨装置
US4515523A (en) * 1983-10-28 1985-05-07 Westinghouse Electric Corp. Cooling arrangement for airfoil stator vane trailing edge
JPH0663442B2 (ja) * 1989-09-04 1994-08-22 株式会社日立製作所 タービン翼
FR2659689B1 (fr) * 1990-03-14 1992-06-05 Snecma Circuit de refroidissement interne d'une aube directrice de turbine.
FR2678318B1 (fr) * 1991-06-25 1993-09-10 Snecma Aube refroidie de distributeur de turbine.
US5503529A (en) * 1994-12-08 1996-04-02 General Electric Company Turbine blade having angled ejection slot
JPH09303106A (ja) * 1996-05-16 1997-11-25 Mitsubishi Heavy Ind Ltd ガスタービン冷却翼
US6254334B1 (en) 1999-10-05 2001-07-03 United Technologies Corporation Method and apparatus for cooling a wall within a gas turbine engine
US6402470B1 (en) 1999-10-05 2002-06-11 United Technologies Corporation Method and apparatus for cooling a wall within a gas turbine engine
GB0114503D0 (en) * 2001-06-14 2001-08-08 Rolls Royce Plc Air cooled aerofoil
DE10217484B4 (de) 2001-11-02 2018-05-17 Ansaldo Energia Ip Uk Limited Leitschaufel einer thermischen Turbomaschine
US7520723B2 (en) * 2006-07-07 2009-04-21 Siemens Energy, Inc. Turbine airfoil cooling system with near wall vortex cooling chambers
US20100221121A1 (en) * 2006-08-17 2010-09-02 Siemens Power Generation, Inc. Turbine airfoil cooling system with near wall pin fin cooling chambers
DE102006042647A1 (de) * 2006-09-12 2008-03-27 Mtu Aero Engines Gmbh Turbine einer Gasturbine
WO2009016744A1 (ja) * 2007-07-31 2009-02-05 Mitsubishi Heavy Industries, Ltd. タービン用翼
FR2924155B1 (fr) * 2007-11-26 2014-02-14 Snecma Aube de turbomachine
GB2467790B (en) 2009-02-16 2011-06-01 Rolls Royce Plc Vane
US8961133B2 (en) * 2010-12-28 2015-02-24 Rolls-Royce North American Technologies, Inc. Gas turbine engine and cooled airfoil
EP2584145A1 (en) 2011-10-20 2013-04-24 Siemens Aktiengesellschaft A cooled turbine guide vane or blade for a turbomachine
EP2893145B1 (en) * 2012-08-20 2019-05-01 Ansaldo Energia IP UK Limited Internally cooled airfoil for a rotary machine
CN103306744B (zh) * 2013-07-03 2015-04-15 中国航空动力机械研究所 导向叶片的冷却装置
US10337334B2 (en) 2015-12-07 2019-07-02 United Technologies Corporation Gas turbine engine component with a baffle insert
US10280841B2 (en) * 2015-12-07 2019-05-07 United Technologies Corporation Baffle insert for a gas turbine engine component and method of cooling
US10422233B2 (en) 2015-12-07 2019-09-24 United Technologies Corporation Baffle insert for a gas turbine engine component and component with baffle insert
US10577947B2 (en) 2015-12-07 2020-03-03 United Technologies Corporation Baffle insert for a gas turbine engine component
US10156146B2 (en) * 2016-04-25 2018-12-18 General Electric Company Airfoil with variable slot decoupling
US10352176B2 (en) 2016-10-26 2019-07-16 General Electric Company Cooling circuits for a multi-wall blade
US10450950B2 (en) 2016-10-26 2019-10-22 General Electric Company Turbomachine blade with trailing edge cooling circuit
US10465521B2 (en) 2016-10-26 2019-11-05 General Electric Company Turbine airfoil coolant passage created in cover
US10273810B2 (en) * 2016-10-26 2019-04-30 General Electric Company Partially wrapped trailing edge cooling circuit with pressure side serpentine cavities
US10598028B2 (en) 2016-10-26 2020-03-24 General Electric Company Edge coupon including cooling circuit for airfoil
US10301946B2 (en) 2016-10-26 2019-05-28 General Electric Company Partially wrapped trailing edge cooling circuits with pressure side impingements
US10233761B2 (en) 2016-10-26 2019-03-19 General Electric Company Turbine airfoil trailing edge coolant passage created by cover
US10309227B2 (en) 2016-10-26 2019-06-04 General Electric Company Multi-turn cooling circuits for turbine blades
US10450875B2 (en) 2016-10-26 2019-10-22 General Electric Company Varying geometries for cooling circuits of turbine blades
CN109879617A (zh) * 2019-03-29 2019-06-14 郑州三迪建筑科技有限公司 一种磷石膏减水阳光棚
US11814965B2 (en) 2021-11-10 2023-11-14 General Electric Company Turbomachine blade trailing edge cooling circuit with turn passage having set of obstructions

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1177035A (fr) * 1957-05-28 1959-04-20 Snecma Procédé et dispositif de refroidissement d'organes de machines
US3475107A (en) * 1966-12-01 1969-10-28 Gen Electric Cooled turbine nozzle for high temperature turbine
US3574481A (en) * 1968-05-09 1971-04-13 James A Pyne Jr Variable area cooled airfoil construction for gas turbines
US3560107A (en) * 1968-09-25 1971-02-02 Gen Motors Corp Cooled airfoil
US3567333A (en) * 1969-01-31 1971-03-02 Curtiss Wright Corp Gas turbine blade
GB1304678A (it) * 1971-06-30 1973-01-24
GB1355558A (en) * 1971-07-02 1974-06-05 Rolls Royce Cooled vane or blade for a gas turbine engine
GB1400285A (en) * 1972-08-02 1975-07-16 Rolls Royce Hollow cooled vane or blade for a gas turbine engine

Also Published As

Publication number Publication date
FR2290569B1 (it) 1979-07-06
NO753728L (it) 1976-05-11
DE2453801A1 (it) 1975-10-02
JPS5169708A (it) 1976-06-16
GB1489098A (en) 1977-10-19
CH584347A5 (it) 1977-01-31
DE2453801B1 (de) 1975-10-02
US4021139A (en) 1977-05-03
FR2290569A1 (fr) 1976-06-04
JPS554932B2 (it) 1980-02-01
NO145962B (no) 1982-03-22
NO145962C (no) 1982-06-30

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