GB1270905A - Cooling system for an axial flow elastic fluid utilizing machine - Google Patents

Cooling system for an axial flow elastic fluid utilizing machine

Info

Publication number
GB1270905A
GB1270905A GB40125/70A GB4012570A GB1270905A GB 1270905 A GB1270905 A GB 1270905A GB 40125/70 A GB40125/70 A GB 40125/70A GB 4012570 A GB4012570 A GB 4012570A GB 1270905 A GB1270905 A GB 1270905A
Authority
GB
United Kingdom
Prior art keywords
rotor
passageway
annular
blades
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
GB40125/70A
Other languages
English (en)
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.)
Westinghouse Electric Corp
Original Assignee
Westinghouse Electric 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 Westinghouse Electric Corp filed Critical Westinghouse Electric Corp
Publication of GB1270905A publication Critical patent/GB1270905A/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
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/08—Heating, heat-insulating or cooling means

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Motor Or Generator Cooling System (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
GB40125/70A 1969-09-29 1970-08-20 Cooling system for an axial flow elastic fluid utilizing machine Expired GB1270905A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US86197769A 1969-09-29 1969-09-29

Publications (1)

Publication Number Publication Date
GB1270905A true GB1270905A (en) 1972-04-19

Family

ID=25337275

Family Applications (1)

Application Number Title Priority Date Filing Date
GB40125/70A Expired GB1270905A (en) 1969-09-29 1970-08-20 Cooling system for an axial flow elastic fluid utilizing machine

Country Status (7)

Country Link
US (1) US3602605A (enExample)
AT (1) AT301273B (enExample)
CA (1) CA919091A (enExample)
CH (1) CH519096A (enExample)
DE (2) DE2043480A1 (enExample)
FR (1) FR2062769A5 (enExample)
GB (1) GB1270905A (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4674955A (en) * 1984-12-21 1987-06-23 The Garrett Corporation Radial inboard preswirl system

Families Citing this family (37)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3750398A (en) * 1971-05-17 1973-08-07 Westinghouse Electric Corp Static seal structure
US3842595A (en) * 1972-12-26 1974-10-22 Gen Electric Modular gas turbine engine
US3945758A (en) * 1974-02-28 1976-03-23 Westinghouse Electric Corporation Cooling system for a gas turbine
US3904307A (en) * 1974-04-10 1975-09-09 United Technologies Corp Gas generator turbine cooling scheme
US3990812A (en) * 1975-03-03 1976-11-09 United Technologies Corporation Radial inflow blade cooling system
GB1501916A (en) * 1975-06-20 1978-02-22 Rolls Royce Matching thermal expansions of components of turbo-machines
US4113406A (en) * 1976-11-17 1978-09-12 Westinghouse Electric Corp. Cooling system for a gas turbine engine
US4184797A (en) * 1977-10-17 1980-01-22 General Electric Company Liquid-cooled turbine rotor
US4306834A (en) * 1979-06-25 1981-12-22 Westinghouse Electric Corp. Balance piston and seal for gas turbine engine
DE3014279A1 (de) * 1980-04-15 1981-10-22 M.A.N. Maschinenfabrik Augsburg-Nürnberg AG, 4200 Oberhausen Einrichtung zur kuehlung des inneren einer gasturbine
FR2484574A1 (fr) * 1980-06-13 1981-12-18 Snecma Palier inter-arbres de turbomachine multi-corps a amortissement par pellicule d'huile
DE3310396A1 (de) * 1983-03-18 1984-09-20 Kraftwerk Union AG, 4330 Mülheim Md-dampfturbine in einflutiger bauweise fuer eine hochtemperaturdampfturbinenanlage mit zwischenueberhitzung
DE3473000D1 (en) * 1983-12-05 1988-09-01 Westinghouse Electric Corp Cascaded air supply for gas turbine cooling
DE3424139C2 (de) * 1984-06-30 1996-02-22 Bbc Brown Boveri & Cie Gasturbinenrotor
US4759688A (en) * 1986-12-16 1988-07-26 Allied-Signal Inc. Cooling flow side entry for cooled turbine blading
US5340271A (en) * 1990-08-18 1994-08-23 Rolls-Royce Plc Flow control method and means
DE4337281A1 (de) * 1993-11-02 1995-05-04 Abb Management Ag Verdichter
DE4433289A1 (de) * 1994-09-19 1996-03-21 Abb Management Ag Axialdurchströmte Gasturbine
DE4435322B4 (de) * 1994-10-01 2005-05-04 Alstom Verfahren und Vorrichtung zur Wellendichtung und zur Kühlung auf der Abgasseite einer axialdurchströmten Gasturbine
JP3652780B2 (ja) * 1996-04-08 2005-05-25 三菱重工業株式会社 タービン冷却装置
SE508085C2 (sv) * 1996-12-12 1998-08-24 Abb Carbon Ab Förfarande för luftflödesstyrning av förbränningsluft samt spärrluftanordning
CA2264282C (en) * 1997-06-20 2002-03-05 Mitsubishi Heavy Industries, Ltd. Gas turbine air separator
US6234746B1 (en) * 1999-08-04 2001-05-22 General Electric Co. Apparatus and methods for cooling rotary components in a turbine
JP4067709B2 (ja) * 1999-08-23 2008-03-26 三菱重工業株式会社 ロータ冷却空気供給装置
DE102004016244B4 (de) * 2004-04-02 2007-08-23 Mtu Aero Engines Gmbh Rotor für eine Turbomaschine
GB2424927A (en) * 2005-04-06 2006-10-11 Rolls Royce Plc A pre-swirl nozzle ring and a method of manufacturing a pre-swirl nozzle ring
US7244104B2 (en) * 2005-05-31 2007-07-17 Pratt & Whitney Canada Corp. Deflectors for controlling entry of fluid leakage into the working fluid flowpath of a gas turbine engine
US7189056B2 (en) * 2005-05-31 2007-03-13 Pratt & Whitney Canada Corp. Blade and disk radial pre-swirlers
US7189055B2 (en) * 2005-05-31 2007-03-13 Pratt & Whitney Canada Corp. Coverplate deflectors for redirecting a fluid flow
US8192151B2 (en) 2009-04-29 2012-06-05 General Electric Company Turbine engine having cooling gland
US8529195B2 (en) 2010-10-12 2013-09-10 General Electric Company Inducer for gas turbine system
US9435206B2 (en) * 2012-09-11 2016-09-06 General Electric Company Flow inducer for a gas turbine system
US9441540B2 (en) * 2012-11-05 2016-09-13 General Electric Company Inducer guide vanes
US9039357B2 (en) * 2013-01-23 2015-05-26 Siemens Aktiengesellschaft Seal assembly including grooves in a radially outwardly facing side of a platform in a gas turbine engine
US9556737B2 (en) 2013-11-18 2017-01-31 Siemens Energy, Inc. Air separator for gas turbine engine
CA2964126C (en) * 2016-04-12 2019-01-08 Airtek Systems Inc. System and method for generating rotational power
US11242804B2 (en) * 2017-06-14 2022-02-08 General Electric Company Inleakage management apparatus

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4674955A (en) * 1984-12-21 1987-06-23 The Garrett Corporation Radial inboard preswirl system

Also Published As

Publication number Publication date
CA919091A (en) 1973-01-16
FR2062769A5 (enExample) 1971-06-25
DE2047648A1 (de) 1971-05-19
DE2043480A1 (de) 1971-04-01
AT301273B (de) 1972-08-25
US3602605A (en) 1971-08-31
CH519096A (de) 1972-02-15

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