[go: up one dir, main page]

GB742288A - Improvements in the cooling of turbines - Google Patents

Improvements in the cooling of turbines

Info

Publication number
GB742288A
GB742288A GB591454A GB591454A GB742288A GB 742288 A GB742288 A GB 742288A GB 591454 A GB591454 A GB 591454A GB 591454 A GB591454 A GB 591454A GB 742288 A GB742288 A GB 742288A
Authority
GB
United Kingdom
Prior art keywords
stator
rotor
blades
feb
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
GB591454A
Inventor
Georges Henry Roesch
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.)
Power Jets Research and Development Ltd
Original Assignee
Power Jets Research and Development Ltd
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 Power Jets Research and Development Ltd filed Critical Power Jets Research and Development Ltd
Priority to GB591454A priority Critical patent/GB742288A/en
Publication of GB742288A publication Critical patent/GB742288A/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
    • F01D5/081—Cooling fluid being directed on the side of the rotor disc or at the roots of the 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
    • F01D9/00—Stators
    • F01D9/06—Fluid supply conduits to nozzles or the like
    • F01D9/065—Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

742,288. Gas turbines. POWER JETS (RESEARCH & DEVELOPMENT), Ltd. Feb. 15, 1952 [Feb. 15, 1951], No. 5914/54. Divided out of 742,241. Drawings to Specification. Class 110(3) The shroud rings for a row of rotor or stator blades is formed by integral blade platforms in the adjacent row of stator or rotor blades, the platforms being spaced from the stator or rotor, and the blades are supplied with a coolant. The subjectmatter is identical with that described in Specification 742,241 but the claims differ.
GB591454A 1951-02-15 1951-02-15 Improvements in the cooling of turbines Expired GB742288A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB591454A GB742288A (en) 1951-02-15 1951-02-15 Improvements in the cooling of turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB591454A GB742288A (en) 1951-02-15 1951-02-15 Improvements in the cooling of turbines

Publications (1)

Publication Number Publication Date
GB742288A true GB742288A (en) 1955-12-21

Family

ID=9804994

Family Applications (1)

Application Number Title Priority Date Filing Date
GB591454A Expired GB742288A (en) 1951-02-15 1951-02-15 Improvements in the cooling of turbines

Country Status (1)

Country Link
GB (1) GB742288A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3730644A (en) * 1969-06-26 1973-05-01 Rolls Royce Gas turbine engine
FR2598179A1 (en) * 1986-04-30 1987-11-06 Gen Electric COOLING AIR TRANSFER DEVICE FOR A TURBINE
US5340278A (en) * 1992-11-24 1994-08-23 United Technologies Corporation Rotor blade with integral platform and a fillet cooling passage
US5344283A (en) * 1993-01-21 1994-09-06 United Technologies Corporation Turbine vane having dedicated inner platform cooling
US5382135A (en) * 1992-11-24 1995-01-17 United Technologies Corporation Rotor blade with cooled integral platform
EP1318275A2 (en) * 2001-12-10 2003-06-11 Nuovo Pignone Holding S.P.A. Structure for separating the high and low pressure turboexpanders of a gas turbine
DE19807563B4 (en) * 1997-02-25 2007-07-19 Mitsubishi Heavy Industries, Ltd. Cooling structure for cooling the platform of a turbine blade
WO2008102497A1 (en) * 2007-02-21 2008-08-28 Mitsubishi Heavy Industries, Ltd. Platform cooling structure of gas turbine rotor blade
JP2011241836A (en) * 2011-08-02 2011-12-01 Mitsubishi Heavy Ind Ltd Platform cooling structure of gas turbine moving blade
EP2938857B1 (en) 2012-12-29 2017-09-27 United Technologies Corporation Heat shield for cooling a strut

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3730644A (en) * 1969-06-26 1973-05-01 Rolls Royce Gas turbine engine
FR2598179A1 (en) * 1986-04-30 1987-11-06 Gen Electric COOLING AIR TRANSFER DEVICE FOR A TURBINE
US5340278A (en) * 1992-11-24 1994-08-23 United Technologies Corporation Rotor blade with integral platform and a fillet cooling passage
US5382135A (en) * 1992-11-24 1995-01-17 United Technologies Corporation Rotor blade with cooled integral platform
US5344283A (en) * 1993-01-21 1994-09-06 United Technologies Corporation Turbine vane having dedicated inner platform cooling
DE19807563B4 (en) * 1997-02-25 2007-07-19 Mitsubishi Heavy Industries, Ltd. Cooling structure for cooling the platform of a turbine blade
EP1318275A2 (en) * 2001-12-10 2003-06-11 Nuovo Pignone Holding S.P.A. Structure for separating the high and low pressure turboexpanders of a gas turbine
EP1318275A3 (en) * 2001-12-10 2004-09-08 Nuovo Pignone Holding S.P.A. Structure for separating the high and low pressure turboexpanders of a gas turbine
WO2008102497A1 (en) * 2007-02-21 2008-08-28 Mitsubishi Heavy Industries, Ltd. Platform cooling structure of gas turbine rotor blade
JP2008202547A (en) * 2007-02-21 2008-09-04 Mitsubishi Heavy Ind Ltd Platform cooling structure of gas turbine moving blade
EP2037081A1 (en) * 2007-02-21 2009-03-18 Mitsubishi Heavy Industries, Ltd. Platform cooling structure of gas turbine rotor blade
CN101473107B (en) * 2007-02-21 2012-05-30 三菱重工业株式会社 Platform cooling structure of gas turbine rotor blade
KR101133491B1 (en) * 2007-02-21 2012-06-21 미츠비시 쥬고교 가부시키가이샤 Platform cooling structure of gas turbine rotor blade
US8231348B2 (en) 2007-02-21 2012-07-31 Mitsubishi Heavy Industries, Ltd. Platform cooling structure for gas turbine moving blade
EP2037081A4 (en) * 2007-02-21 2013-05-01 Mitsubishi Heavy Ind Ltd GAS TURBINE ROTOR BLADE COOLING PLATFORM COOLING STRUCTURE
JP2011241836A (en) * 2011-08-02 2011-12-01 Mitsubishi Heavy Ind Ltd Platform cooling structure of gas turbine moving blade
EP2938857B1 (en) 2012-12-29 2017-09-27 United Technologies Corporation Heat shield for cooling a strut
EP2938857B2 (en) † 2012-12-29 2020-11-25 United Technologies Corporation Heat shield for cooling a strut

Similar Documents

Publication Publication Date Title
GB1357713A (en) Cooled rotor blades for gas turbines
GB590420A (en) Improvements in and relating to gas turbines
FR2117848A1 (en)
GB742288A (en) Improvements in the cooling of turbines
GB1161298A (en) Turbomachine Rotors
GB1513338A (en) Rotor blade for a gas turbine engine
GB452412A (en) Improvements relating to apparatus for cooling the rotors of turbines
GB586557A (en) Improvements in internal combustion turbine plant for propulsion
GB1450133A (en) Cooling of gas turbine engines
GB693727A (en) Improvements relating to bladed rotary fluid-flow machines
GB838602A (en) Improvements in or relating to gas turbine plant
GB854812A (en) Gas turbine blade
GB609322A (en) Improvements relating to axial-flow compressors and like machines, and blading thereof
GB656930A (en) Improvements in gas turbines
GB586551A (en) Improvements in or relating to internal combustion power turbine plant for propulsion in air
GB586838A (en) Elastic fluid turbines
GB624777A (en) Improvements in or relating to stator casings for compressors and like machines
GB561692A (en) Improvements in or relating to thermal power plants
GB640969A (en) Improvements in compressor and turbine rotors
GB477449A (en) Improvements in or relating to ventilating fans and the like
GB585345A (en) Internal-combustion turbine plant
GB711528A (en) Elastic fluid turbine plant
GB989581A (en) High power steam turbine
GB713647A (en) Improvements in or relating to water-cooled gas turbines
GB701561A (en) Improvements relating to gas turbine plant