FR1454951A - Nouveau type d'aube pour turbines à gaz ou à vapeur - Google Patents

Nouveau type d'aube pour turbines à gaz ou à vapeur

Info

Publication number
FR1454951A
FR1454951A FR40128A FR40128A FR1454951A FR 1454951 A FR1454951 A FR 1454951A FR 40128 A FR40128 A FR 40128A FR 40128 A FR40128 A FR 40128A FR 1454951 A FR1454951 A FR 1454951A
Authority
FR
France
Prior art keywords
blade
gas
new type
steam turbines
turbines
Prior art date
Legal status (The legal status 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 status listed.)
Expired
Application number
FR40128A
Other languages
English (en)
Inventor
Arthur Bill
Thomas Steele
Michael Poucher
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 PLC filed Critical Rolls Royce PLC
Application granted granted Critical
Publication of FR1454951A publication Critical patent/FR1454951A/fr
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • 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
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
FR40128A 1964-12-02 1965-11-29 Nouveau type d'aube pour turbines à gaz ou à vapeur Expired FR1454951A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB49101/64A GB1034260A (en) 1964-12-02 1964-12-02 Aerofoil-shaped blade for use in a fluid flow machine

Publications (1)

Publication Number Publication Date
FR1454951A true FR1454951A (fr) 1966-02-11

Family

ID=10451151

Family Applications (1)

Application Number Title Priority Date Filing Date
FR40128A Expired FR1454951A (fr) 1964-12-02 1965-11-29 Nouveau type d'aube pour turbines à gaz ou à vapeur

Country Status (5)

Country Link
US (1) US3353351A (fr)
DE (2) DE1280618B (fr)
FR (1) FR1454951A (fr)
GB (2) GB1034260A (fr)
MY (1) MY6800109A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1609950A2 (fr) 2004-06-25 2005-12-28 United Technologies Corporation Manchon crénelé pour aube de turbomachine

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3412979A (en) * 1965-12-10 1968-11-26 Rolls Royce Aerofoil-shaped blade for use in a fluid flow machine such as a turbine
US3726604A (en) * 1971-10-13 1973-04-10 Gen Motors Corp Cooled jet flap vane
US5220794A (en) * 1988-12-12 1993-06-22 Sundstrand Corporation Improved fuel injector for a gas turbine engine
US4989404A (en) * 1988-12-12 1991-02-05 Sundstrand Corporation Turbine engine with high efficiency fuel atomization
US4967563A (en) * 1988-12-12 1990-11-06 Sundstrand Corporation Turbine engine with high efficiency fuel atomization
US4967562A (en) * 1988-12-12 1990-11-06 Sundstrand Corporation Turbine engine with high efficiency fuel atomization
US5027603A (en) * 1988-12-28 1991-07-02 Sundstrand Corporation Turbine engine with start injector
US5241818A (en) * 1989-07-13 1993-09-07 Sundstrand Corporation Fuel injector for a gas turbine engine
US5239818A (en) * 1992-03-30 1993-08-31 General Electric Company Dilution pole combustor and method
DE4309131A1 (de) * 1993-03-22 1994-09-29 Abb Management Ag Verfahren und Vorrichtung zur Nachlaufbeeinflussung bei Brennkammereinbauten
DE4336143C2 (de) * 1993-10-22 1995-11-16 Erich Wuerzinger Kühlverfahren für Turbomaschinen
DE19651881A1 (de) * 1996-12-13 1998-06-18 Asea Brown Boveri Brennkammer mit integrierten Leitschaufeln
EP1270874B1 (fr) 2001-06-18 2005-08-31 Siemens Aktiengesellschaft Turbine à gaz avec un compresseur d'air
WO2006053825A1 (fr) * 2004-11-16 2006-05-26 Alstom Technology Ltd Dispositif de turbine a gaz, et chambre de combustion correspondante
US8713909B2 (en) * 2009-03-04 2014-05-06 United Technologies Corporation Elimination of unfavorable outflow margin
US10711702B2 (en) * 2015-08-18 2020-07-14 General Electric Company Mixed flow turbocore
US10578028B2 (en) 2015-08-18 2020-03-03 General Electric Company Compressor bleed auxiliary turbine
US20200182068A1 (en) * 2018-12-05 2020-06-11 United Technologies Corporation Axial flow cooling scheme with structural rib for a gas turbine engine
US10822963B2 (en) 2018-12-05 2020-11-03 Raytheon Technologies Corporation Axial flow cooling scheme with castable structural rib for a gas turbine engine
US11603766B1 (en) 2022-05-04 2023-03-14 Pratt & Whitney Canada Corp. Turbine stator vanes having inserts and splitter plates

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2641040A (en) * 1948-01-02 1953-06-09 Esther C Goddard Means for cooling turbine blades by air
US2858100A (en) * 1952-02-01 1958-10-28 Stalker Dev Company Blade structure for turbines and the like
GB753224A (en) * 1953-04-13 1956-07-18 Rolls Royce Improvements in or relating to blading for turbines or compressors
DE1055884B (de) * 1954-03-02 1959-04-23 Bristol Aero Engines Ltd Flammrohr fuer eine Brennkammer eines Gasturbinenmotors
US2920866A (en) * 1954-12-20 1960-01-12 A V Roe Canada Ltd Hollow air cooled sheet metal turbine blade
FR1177035A (fr) * 1957-05-28 1959-04-20 Snecma Procédé et dispositif de refroidissement d'organes de machines
GB854135A (en) * 1958-03-05 1960-11-16 Rolls Royce Improvements in or relating to combustion equipment
DE1204021B (de) * 1959-04-27 1965-10-28 Rolls Royce Schaufel fuer Axialstroemungsmaschinen, insbesondere Gasturbinen
GB898368A (en) * 1959-06-23 1962-06-06 Rolls Royce Improved combustion chamber
US3242674A (en) * 1961-05-05 1966-03-29 Lucas Industries Ltd Liquid fuel combustion apparatus
GB938247A (en) * 1962-03-26 1963-10-02 Rolls Royce Gas turbine engine having cooled turbine blading

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1609950A2 (fr) 2004-06-25 2005-12-28 United Technologies Corporation Manchon crénelé pour aube de turbomachine
EP1609950A3 (fr) * 2004-06-25 2009-07-22 United Technologies Corporation Manchon crénelé pour aube de turbomachine

Also Published As

Publication number Publication date
US3353351A (en) 1967-11-21
GB1068280A (en) 1967-05-10
GB1034260A (en) 1966-06-29
DE1476892A1 (de) 1970-07-16
DE1280618B (de) 1968-10-17
DE1476892B2 (de) 1970-11-12
MY6800109A (en) 1968-12-31

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