GB1222565A - Gas turbine guide blade - Google Patents

Gas turbine guide blade

Info

Publication number
GB1222565A
GB1222565A GB37086/68A GB3708668A GB1222565A GB 1222565 A GB1222565 A GB 1222565A GB 37086/68 A GB37086/68 A GB 37086/68A GB 3708668 A GB3708668 A GB 3708668A GB 1222565 A GB1222565 A GB 1222565A
Authority
GB
United Kingdom
Prior art keywords
ducts
insert
blade
aperture
cooling air
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
GB37086/68A
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.)
MTU Aero Engines GmbH
Original Assignee
MTU Motoren und Turbinen Union Muenchen GmbH
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 MTU Motoren und Turbinen Union Muenchen GmbH filed Critical MTU Motoren und Turbinen Union Muenchen GmbH
Publication of GB1222565A publication Critical patent/GB1222565A/en
Expired legal-status Critical Current

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
    • 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
    • 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
    • F05D2260/221—Improvement of heat transfer
    • F05D2260/2212—Improvement of heat transfer by creating turbulence
    • 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

Abstract

1,222,565. Turbine blades. MOTOREN-UND TURBINEN-UNION MUNCHEN G.m.b.H. Aug. 2, 1968 [Aug.3, 1967], No.37086/68 Heading F1T. A hollow turbine guide blade for a gas turbine engine contains, in one arrangement Figs.1, 2, a hollow insert 2 having chordwise extending corrugations defining cooling air ducts 4 with the blade wall 1. The corrugations may be shallower on one side of the blade than on the other. The cooling air is supplied to the interior 3 of the insert 2 from the engine compressor and flows to the ducts 4 through holes 5 in the insert, thence flowing rearwardly to discharge through an aperture 6 adjacent the trailing edge. The latter is arranged so that one edge 7 of the blade wall 1 extends beyond the aperture 6 and at least one edge 8 of the insert 2 extends through the aperture. In a modification, Fig. 5, the ducts 4 are formed in the wall of the insert 2 and receive cooling air through holes 5 from the insert interior 3. The ducts 4 may be oval, as shown, triangular or lenticular, Figs. 6, 7 (not shown). In Fig. 8 and in Figs. 9, 10,12 (not shown), the ducts 4 are formed in the blade wall 1, and in Fig. 11 the ducts 4 are formed in inserts 10 mounted only in particularly hot regions of the blade.
GB37086/68A 1967-08-03 1968-08-02 Gas turbine guide blade Expired GB1222565A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19671601613 DE1601613A1 (en) 1967-08-03 1967-08-03 Turbine blades, in particular turbine guide blades for gas turbine engines

Publications (1)

Publication Number Publication Date
GB1222565A true GB1222565A (en) 1971-02-17

Family

ID=5680944

Family Applications (1)

Application Number Title Priority Date Filing Date
GB37086/68A Expired GB1222565A (en) 1967-08-03 1968-08-02 Gas turbine guide blade

Country Status (4)

Country Link
AT (1) AT289474B (en)
DE (1) DE1601613A1 (en)
FR (1) FR1575301A (en)
GB (1) GB1222565A (en)

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3767322A (en) * 1971-07-30 1973-10-23 Westinghouse Electric Corp Internal cooling for turbine vanes
US3806275A (en) * 1972-08-30 1974-04-23 Gen Motors Corp Cooled airfoil
US3809494A (en) * 1971-06-30 1974-05-07 Rolls Royce 1971 Ltd Vane or blade for a gas turbine engine
US4080095A (en) * 1976-09-02 1978-03-21 Westinghouse Electric Corporation Cooled turbine vane
US4229140A (en) * 1972-11-28 1980-10-21 Rolls-Royce (1971) Ltd. Turbine blade
DE3003347A1 (en) * 1979-12-20 1981-06-25 BBC AG Brown, Boveri & Cie., Baden, Aargau COOLED WALL
US4303374A (en) * 1978-12-15 1981-12-01 General Electric Company Film cooled airfoil body
GB2264149A (en) * 1992-02-13 1993-08-18 Preci Spark Ltd Reinforced turbocharger vane.
US5259730A (en) * 1991-11-04 1993-11-09 General Electric Company Impingement cooled airfoil with bonding foil insert
US5509783A (en) * 1993-02-09 1996-04-23 Preci-Spark, Ltd. Reinforced vane
US5538394A (en) * 1993-12-28 1996-07-23 Kabushiki Kaisha Toshiba Cooled turbine blade for a gas turbine
CN113236371A (en) * 2021-06-04 2021-08-10 中国航发沈阳发动机研究所 Blade air conditioning duct

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0756201B2 (en) * 1984-03-13 1995-06-14 株式会社東芝 Gas turbine blades
US4601638A (en) * 1984-12-21 1986-07-22 United Technologies Corporation Airfoil trailing edge cooling arrangement
FR2586268B1 (en) * 1985-08-14 1989-06-09 Snecma DEVICE FOR VARIATION OF THE PASSAGE SECTION OF A TURBINE DISTRIBUTOR
RU2151303C1 (en) * 1996-03-14 2000-06-20 АББ Унитурбо Лтд. Cooled moving or nozzle blade of gas turbine
FR2758587B1 (en) * 1997-01-23 1999-02-19 Snecma DEVICE FOR COOLING A TURBINE BLADE
JP4170400B2 (en) * 1997-04-07 2008-10-22 シーメンス アクチエンゲゼルシヤフト Turbine blade, its use and cooling method of turbine blade
EP1659262A1 (en) 2004-11-23 2006-05-24 Siemens Aktiengesellschaft Cooled gas turbine blade and cooling method thereof

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3809494A (en) * 1971-06-30 1974-05-07 Rolls Royce 1971 Ltd Vane or blade for a gas turbine engine
US3767322A (en) * 1971-07-30 1973-10-23 Westinghouse Electric Corp Internal cooling for turbine vanes
US3806275A (en) * 1972-08-30 1974-04-23 Gen Motors Corp Cooled airfoil
US4229140A (en) * 1972-11-28 1980-10-21 Rolls-Royce (1971) Ltd. Turbine blade
US4080095A (en) * 1976-09-02 1978-03-21 Westinghouse Electric Corporation Cooled turbine vane
US4303374A (en) * 1978-12-15 1981-12-01 General Electric Company Film cooled airfoil body
DE3003347A1 (en) * 1979-12-20 1981-06-25 BBC AG Brown, Boveri & Cie., Baden, Aargau COOLED WALL
US5259730A (en) * 1991-11-04 1993-11-09 General Electric Company Impingement cooled airfoil with bonding foil insert
GB2264149A (en) * 1992-02-13 1993-08-18 Preci Spark Ltd Reinforced turbocharger vane.
GB2264149B (en) * 1992-02-13 1995-07-05 Preci Spark Ltd Reinforced vane
US5509783A (en) * 1993-02-09 1996-04-23 Preci-Spark, Ltd. Reinforced vane
US5538394A (en) * 1993-12-28 1996-07-23 Kabushiki Kaisha Toshiba Cooled turbine blade for a gas turbine
CN113236371A (en) * 2021-06-04 2021-08-10 中国航发沈阳发动机研究所 Blade air conditioning duct

Also Published As

Publication number Publication date
DE1601613A1 (en) 1970-12-17
AT289474B (en) 1971-04-26
FR1575301A (en) 1969-07-18

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