GB1075030A - A vane or blade of stacked wafer const ruction for a turbine or like fluid flow machine - Google Patents

A vane or blade of stacked wafer const ruction for a turbine or like fluid flow machine

Info

Publication number
GB1075030A
GB1075030A GB52269/65A GB5226965A GB1075030A GB 1075030 A GB1075030 A GB 1075030A GB 52269/65 A GB52269/65 A GB 52269/65A GB 5226965 A GB5226965 A GB 5226965A GB 1075030 A GB1075030 A GB 1075030A
Authority
GB
United Kingdom
Prior art keywords
groove
lamination
laminations
cooling air
turbine
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
GB52269/65A
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.)
Raytheon Technologies Corp
Original Assignee
United Aircraft Corp
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 United Aircraft Corp filed Critical United Aircraft Corp
Publication of GB1075030A publication Critical patent/GB1075030A/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
    • 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
    • F01D5/182—Transpiration cooling
    • F01D5/184—Blade walls being made of perforated sheet laminae
    • 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
    • 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
    • F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
    • 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

1,075,030. Turbine blades. UNITED AIRCRAFT CORPORATION. Dec.9, 1965 [Dec. 22, 1964], No. 52269/65. Heading F1T. Each turbine nozzle guide blade 34 in a gas turbine engine consists of stacked thin aerofoil section laminations 50 secured together by bolts 56, 58 passing through the laminations and through segmental shroud platforms 52, 54. The platforms are secured to adjacent casing structure by bolts 74, 76 respectively. Cooling air is supplied through a pipe 104 from the engine compressor to an annular chamber 100 at the radially outer end of the guide blades 34 to supply passages within the blades. These passages comprise, Fig. 3 (not shown), a main channel (114) extending radially through the laminations 50 and communicating through ports (116) with a groove (110) formed in one face of each lamination. Cooling air from the groove (110) leaves the trailing edge of the lamination through a further groove (112). The bolt 56 extends through the centre of the channel (114) and has radially spaced cooling air passages (118). The width (t) of the groove (110) is varied along its length to satisfy the local cooling requirements. In a modification, Fig. 6 (not shown), each lamination (50A) has two main channels (214, 220) and the cooling air from a. groove (210) is discharged through openings (211, 213) in the convex and concave sides of the lamination. Figs. 7, 9 (not shown) illustrate further modifications, the main channel (414) through the laminations (50C) in Fig. 9 containing a baffle member (422).
GB52269/65A 1964-12-22 1965-12-09 A vane or blade of stacked wafer const ruction for a turbine or like fluid flow machine Expired GB1075030A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US420338A US3301526A (en) 1964-12-22 1964-12-22 Stacked-wafer turbine vane or blade

Publications (1)

Publication Number Publication Date
GB1075030A true GB1075030A (en) 1967-07-12

Family

ID=23666062

Family Applications (1)

Application Number Title Priority Date Filing Date
GB52269/65A Expired GB1075030A (en) 1964-12-22 1965-12-09 A vane or blade of stacked wafer const ruction for a turbine or like fluid flow machine

Country Status (3)

Country Link
US (1) US3301526A (en)
DE (1) DE1476921B1 (en)
GB (1) GB1075030A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2834864A1 (en) * 1978-08-09 1980-02-14 Motoren Turbinen Union COMPOSED CERAMIC GAS TURBINE BLADE
FR2484014A1 (en) * 1980-06-05 1981-12-11 United Technologies Corp ROTOR BLADE WITH HEAD CONSISTING OF COOLING PLATES

Families Citing this family (39)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1075910A (en) * 1966-04-04 1967-07-19 Rolls Royce Improvements in or relating to blades for mounting in fluid flow ducts
US3619077A (en) * 1966-09-30 1971-11-09 Gen Electric High-temperature airfoil
US3443791A (en) * 1966-11-23 1969-05-13 United Aircraft Corp Turbine vane assembly
US3423069A (en) * 1967-09-29 1969-01-21 Trw Inc Airfoil
US3778183A (en) * 1968-04-22 1973-12-11 Aerojet General Co Cooling passages wafer blade assemblies for turbine engines, compressors and the like
US3515499A (en) * 1968-04-22 1970-06-02 Aerojet General Co Blades and blade assemblies for turbine engines,compressors and the like
US3630707A (en) * 1969-06-11 1971-12-28 Corning Glass Works Temperature control system for glass-shaping molds
US3628885A (en) * 1969-10-01 1971-12-21 Gen Electric Fluid-cooled airfoil
DE1951356C3 (en) * 1969-10-11 1980-08-28 Mtu Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Gas turbine engine for aircraft
US3891348A (en) * 1972-04-24 1975-06-24 Gen Electric Turbine blade with increased film cooling
US3872563A (en) * 1972-11-13 1975-03-25 United Aircraft Corp Method of blade construction
US3906725A (en) * 1973-07-02 1975-09-23 Aerojet General Co Exhaust emissions control device
GB1596255A (en) * 1973-07-26 1981-08-26 Rolls Royce Stator blade for a gas turbine engine
US4069662A (en) * 1975-12-05 1978-01-24 United Technologies Corporation Clearance control for gas turbine engine
US4270883A (en) * 1977-04-20 1981-06-02 The Garrett Corporation Laminated airfoil
US4221539A (en) * 1977-04-20 1980-09-09 The Garrett Corporation Laminated airfoil and method for turbomachinery
US7934900B1 (en) * 1977-08-03 2011-05-03 Rolls-Royce Limited Nozzle guide vane for a gas turbine engine
US4203706A (en) * 1977-12-28 1980-05-20 United Technologies Corporation Radial wafer airfoil construction
US4314794A (en) * 1979-10-25 1982-02-09 Westinghouse Electric Corp. Transpiration cooled blade for a gas turbine engine
US4318668A (en) * 1979-11-01 1982-03-09 United Technologies Corporation Seal means for a gas turbine engine
US4462204A (en) * 1982-07-23 1984-07-31 General Electric Company Gas turbine engine cooling airflow modulator
US4526512A (en) * 1983-03-28 1985-07-02 General Electric Co. Cooling flow control device for turbine blades
US4859147A (en) * 1988-01-25 1989-08-22 United Technologies Corporation Cooled gas turbine blade
JPH0663442B2 (en) * 1989-09-04 1994-08-22 株式会社日立製作所 Turbine blades
US5493855A (en) * 1992-12-17 1996-02-27 Alfred E. Tisch Turbine having suspended rotor blades
US6099251A (en) * 1998-07-06 2000-08-08 United Technologies Corporation Coolable airfoil for a gas turbine engine
US7247003B2 (en) 2004-12-02 2007-07-24 Siemens Power Generation, Inc. Stacked lamellate assembly
US7255535B2 (en) * 2004-12-02 2007-08-14 Albrecht Harry A Cooling systems for stacked laminate CMC vane
US7198458B2 (en) * 2004-12-02 2007-04-03 Siemens Power Generation, Inc. Fail safe cooling system for turbine vanes
US7247002B2 (en) * 2004-12-02 2007-07-24 Siemens Power Generation, Inc. Lamellate CMC structure with interlock to metallic support structure
US7153096B2 (en) * 2004-12-02 2006-12-26 Siemens Power Generation, Inc. Stacked laminate CMC turbine vane
US8137611B2 (en) * 2005-03-17 2012-03-20 Siemens Energy, Inc. Processing method for solid core ceramic matrix composite airfoil
US8251651B2 (en) * 2009-01-28 2012-08-28 United Technologies Corporation Segmented ceramic matrix composite turbine airfoil component
GB2471119B (en) * 2009-06-17 2013-11-27 Nebb Technology As Rotor or stator blade and method for forming such rotor or stator blade
US8678771B2 (en) * 2009-12-14 2014-03-25 Siemens Energy, Inc. Process for manufacturing a component
US9670797B2 (en) * 2012-09-28 2017-06-06 United Technologies Corporation Modulated turbine vane cooling
EP3048254B1 (en) * 2015-01-22 2017-12-27 Rolls-Royce Corporation Vane assembly for a gas turbine engine
DE102015212419A1 (en) * 2015-07-02 2017-01-05 Siemens Aktiengesellschaft Blade assembly for a gas turbine
US20190024520A1 (en) * 2017-07-19 2019-01-24 Micro Cooling Concepts, Inc. Turbine blade cooling

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US730363A (en) * 1902-08-21 1903-06-09 Gen Electric Detachable turbine-bucket.
DE767546C (en) * 1938-09-12 1952-11-04 Bmw Flugmotorenbau G M B H Internally cooled turbine blade
US2618462A (en) * 1948-12-30 1952-11-18 Kane Saul Allan Turbine rotor formed of laminated plates with aperture overlap
US2853271A (en) * 1951-06-28 1958-09-23 Eaton Mfg Co Blade structure
US2879028A (en) * 1954-03-31 1959-03-24 Edward A Stalker Cooled turbine blades
DE1024754B (en) * 1956-02-11 1958-02-20 Maschf Augsburg Nuernberg Ag Cooled blade for hot operated turbines or compressors
BE557503A (en) * 1956-05-15
DE1062496B (en) * 1958-01-14 1959-07-30 Daimler Benz Ag Blade for flow machines, especially guide blade for gas turbines
US3163397A (en) * 1958-01-14 1964-12-29 Daimler Benz Ag Vane construction
DE1064757B (en) * 1958-01-14 1959-09-03 Daimler Benz Ag Ceramic blade, especially blade for flow machines

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2834864A1 (en) * 1978-08-09 1980-02-14 Motoren Turbinen Union COMPOSED CERAMIC GAS TURBINE BLADE
FR2484014A1 (en) * 1980-06-05 1981-12-11 United Technologies Corp ROTOR BLADE WITH HEAD CONSISTING OF COOLING PLATES

Also Published As

Publication number Publication date
US3301526A (en) 1967-01-31
DE1476921B1 (en) 1970-03-26

Similar Documents

Publication Publication Date Title
GB1075030A (en) A vane or blade of stacked wafer const ruction for a turbine or like fluid flow machine
US4222707A (en) Device for the impact cooling of the turbine packing rings of a turbojet engine
GB1338354A (en) Fluid-directing cascade for reaction with high-temperature gases
GB1070475A (en) Improvements in hollow turbine or compressor stator vane or rotor blade
GB971548A (en) Fluid flow control apparatus
GB1177410A (en) Improvements in Gas Turbine Engine Turbine Rotor Shrouds
GB1457634A (en) Converging-diverging supersonic nozzles
GB1088360A (en) Improvements in gas turbine ducted fan engine sealing means
GB1144036A (en) A vane for an aerial flow turbomachine
GB1240568A (en) Outlet housing of an axial-flow turbomachine
GB1129410A (en) Improvements in or relating to fluid flow machines
GB1075910A (en) Improvements in or relating to blades for mounting in fluid flow ducts
GB1345910A (en) Gas turbine engines
US4066381A (en) Turbine stator nozzles
GB1373898A (en) Gas turbine nozzle vane structure
GB1376966A (en) Porous abradable seal structures
GB825967A (en) Improvements in turbines and in particular gas turbines
GB1135879A (en) Improvements in fluid cooled stator arrangements in axial flow rotary machines
GB1081458A (en) Blade assembly for a fluid flow machine such as a gas turbine engine
GB742477A (en) Improvements in or relating to bladed stator or rotor constructions for fluid machines such as axial-flow turbines or compressors
GB1034260A (en) Aerofoil-shaped blade for use in a fluid flow machine
US2682363A (en) Gas turbine engine
GB1301002A (en) Improvements relating to fluid-flow machines
GB1516757A (en) Turbomachinery vane or blade with cooled platforms
GB1161297A (en) Turbomachine Rotors