IT1109912B - Paletta di rotore o paletta direttrice per turbina a gas - Google Patents

Paletta di rotore o paletta direttrice per turbina a gas

Info

Publication number
IT1109912B
IT1109912B IT19045/79A IT1904579A IT1109912B IT 1109912 B IT1109912 B IT 1109912B IT 19045/79 A IT19045/79 A IT 19045/79A IT 1904579 A IT1904579 A IT 1904579A IT 1109912 B IT1109912 B IT 1109912B
Authority
IT
Italy
Prior art keywords
blade
gas turbine
direct
rotor blade
rotor
Prior art date
Application number
IT19045/79A
Other languages
English (en)
Other versions
IT7919045A0 (it
Original Assignee
Rolls Royce
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 Rolls Royce filed Critical Rolls Royce
Publication of IT7919045A0 publication Critical patent/IT7919045A0/it
Application granted granted Critical
Publication of IT1109912B publication Critical patent/IT1109912B/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
IT19045/79A 1978-01-14 1979-01-03 Paletta di rotore o paletta direttrice per turbina a gas IT1109912B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB155278 1978-01-14

Publications (2)

Publication Number Publication Date
IT7919045A0 IT7919045A0 (it) 1979-01-03
IT1109912B true IT1109912B (it) 1985-12-23

Family

ID=9723956

Family Applications (1)

Application Number Title Priority Date Filing Date
IT19045/79A IT1109912B (it) 1978-01-14 1979-01-03 Paletta di rotore o paletta direttrice per turbina a gas

Country Status (5)

Country Link
US (1) US4286924A (it)
JP (1) JPS54101014A (it)
DE (1) DE2900545C3 (it)
FR (1) FR2414619A1 (it)
IT (1) IT1109912B (it)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4601638A (en) * 1984-12-21 1986-07-22 United Technologies Corporation Airfoil trailing edge cooling arrangement
US5197852A (en) * 1990-05-31 1993-03-30 General Electric Company Nozzle band overhang cooling
US5405242A (en) * 1990-07-09 1995-04-11 United Technologies Corporation Cooled vane
US5439354A (en) * 1993-06-15 1995-08-08 General Electric Company Hollow airfoil impact resistance improvement
DE19963349A1 (de) 1999-12-27 2001-06-28 Abb Alstom Power Ch Ag Schaufel für Gasturbinen mit Drosselquerschnitt an Hinterkante
EP1245785B1 (de) * 2001-03-26 2005-06-01 Siemens Aktiengesellschaft Verfahren zur Herstellung einer Turbinenschaufel
JP4103812B2 (ja) * 2003-03-05 2008-06-18 株式会社Ｉｈｉ 鋳型の製造方法
US7665968B2 (en) * 2004-05-27 2010-02-23 United Technologies Corporation Cooled rotor blade
DE102005051931B4 (de) * 2005-10-29 2007-08-09 Nordex Energy Gmbh Rotorblatt für Windkraftanlagen
US20080110024A1 (en) * 2006-11-14 2008-05-15 Reilly P Brennan Airfoil casting methods
US9611744B2 (en) 2014-04-04 2017-04-04 Betty Jean Taylor Intercooled compressor for a gas turbine engine
DE102015203765A1 (de) * 2015-03-03 2016-09-08 Siemens Aktiengesellschaft Massives hohles Bauteil mit Blech zur Erzeugung eines Hohlraums
US10364681B2 (en) * 2015-10-15 2019-07-30 General Electric Company Turbine blade
US10934850B2 (en) * 2017-08-25 2021-03-02 DOOSAN Heavy Industries Construction Co., LTD Turbine blade having an additive manufacturing trailing edge

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE737479C (de) * 1939-01-26 1943-07-15 Versuchsanstalt Fuer Luftfahrt Gasturbinenschaufel
US2675208A (en) * 1948-10-11 1954-04-13 Packard Motor Car Co Turbine rotor blade
GB679931A (en) * 1949-12-02 1952-09-24 Bristol Aeroplane Co Ltd Improvements in or relating to blades for turbines or the like
US2848192A (en) * 1953-03-12 1958-08-19 Gen Motors Corp Multi-piece hollow turbine bucket
GB893706A (en) * 1960-01-05 1962-04-11 Rolls Royce Blades for fluid flow machines
GB1078116A (en) * 1963-07-18 1967-08-02 Bristol Siddeley Engines Ltd Stator blades for combustion turbines
CH426883A (de) * 1964-11-26 1966-12-31 Elin Union Ag Entwässerungseinrichtung an der Niederdruckstufe einer Dampfturbine
US3844678A (en) * 1967-11-17 1974-10-29 Gen Electric Cooled high strength turbine bucket
DE1776015A1 (de) * 1968-09-04 1971-09-16 Daimler Benz Ag Turbinenschaufel
US3623825A (en) * 1969-11-13 1971-11-30 Avco Corp Liquid-metal-filled rotor blade
US3650635A (en) * 1970-03-09 1972-03-21 Chromalloy American Corp Turbine vanes
US3628226A (en) * 1970-03-16 1971-12-21 Aerojet General Co Method of making hollow compressor blades
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
BE795073A (fr) * 1972-03-02 1973-05-29 Gen Electric Procede pour la fabrication d'aubes creuses
US3781130A (en) * 1972-06-27 1973-12-25 Us Air Force Turbine blade manufactured of self-carrying laminates
GB1400285A (en) * 1972-08-02 1975-07-16 Rolls Royce Hollow cooled vane or blade for a gas turbine engine
US3934322A (en) * 1972-09-21 1976-01-27 General Electric Company Method for forming cooling slot in airfoil blades
US3921271A (en) * 1973-01-02 1975-11-25 Gen Electric Air-cooled turbine blade and method of making same
US4026659A (en) * 1975-10-16 1977-05-31 Avco Corporation Cooled composite vanes for turbine nozzles

Also Published As

Publication number Publication date
DE2900545A1 (de) 1979-07-19
DE2900545B2 (de) 1980-06-26
US4286924A (en) 1981-09-01
JPS54101014A (en) 1979-08-09
IT7919045A0 (it) 1979-01-03
DE2900545C3 (de) 1981-02-19
FR2414619A1 (fr) 1979-08-10

Similar Documents

Publication Publication Date Title
JPS5529099A (en) Blade member for gas turbine
AR211811A1 (es) Paleta de rotor de turbina de gas
GB2027495B (en) Turbine blade
GB2030657B (en) Blade for gas turbine engine
JPS54160911A (en) Blade for gas turbine engine
DK150022C (da) Holdeindretning til et rotorblad eller en rotorvinge
IT7924547A0 (it) Perfezionata paletta di turbomacchina.
AU2381177A (en) Ceramic rotor blade assembly for gas turbine
SE7901165L (sv) Turbin
IT8020482A0 (it) Rotore palettato per motore a turbina a gas.
IT7821869A0 (it) Paletta di rotore raffreddata per motore a turbina a gas.
GB2027496B (en) Turbine blade
PL212218A1 (pl) Turbina gazowa
SE7812460L (sv) Rotorblad for en vindmotor
GB2015658B (en) Turbine blade
DK154239C (da) Rotor til en vindmoelle
IT1109912B (it) Paletta di rotore o paletta direttrice per turbina a gas
BE894260A (fr) Aubes de rotor de turbine
IT7927522A0 (it) Carcassa di turbina a gas.
IT1085791B (it) Paletta di rotore per motore a turbina a gas
GB2021699B (en) Gas turbine blade cooling arrangement
IT1121263B (it) Disposizione di montaggio cedevole per rotore di elicottero a lama passante
IT7919648A0 (it) Motori a turbina a gas.
IT7822908A0 (it) Paletta di rotore per motore a turbina a gas.
GB2030233B (en) Gas turbine engine blade