FR1163559A - Turbine training - Google Patents

Turbine training

Info

Publication number
FR1163559A
FR1163559A FR1163559DA FR1163559A FR 1163559 A FR1163559 A FR 1163559A FR 1163559D A FR1163559D A FR 1163559DA FR 1163559 A FR1163559 A FR 1163559A
Authority
FR
France
Prior art keywords
turbine
training
turbine training
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
Other languages
French (fr)
Inventor
Jean-Henri Bertin
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.)
Bertin Technologies SAS
Original Assignee
Bertin et Cie SA
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 Bertin et Cie SA filed Critical Bertin et Cie SA
Application granted granted Critical
Publication of FR1163559A publication Critical patent/FR1163559A/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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/10—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using sealing fluid, e.g. steam

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR1163559D 1956-12-21 1956-12-21 Turbine training Expired FR1163559A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1163559T 1956-12-21

Publications (1)

Publication Number Publication Date
FR1163559A true FR1163559A (en) 1958-09-29

Family

ID=9653571

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1163559D Expired FR1163559A (en) 1956-12-21 1956-12-21 Turbine training

Country Status (1)

Country Link
FR (1) FR1163559A (en)

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3597102A (en) * 1968-06-10 1971-08-03 English Electric Co Ltd Turbines
FR2384949A1 (en) * 1977-03-26 1978-10-20 Rolls Royce SEALING DEVICE FOR GAS TURBINE ROTOR
FR2426159A1 (en) * 1978-05-20 1979-12-14 Rolls Royce REFRIGERANT AIR SUPPLY DEVICE FOR GAS TURBINE ENGINE
US4732531A (en) * 1986-08-11 1988-03-22 National Aerospace Laboratory of Science and Technoloyg Agency Air sealed turbine blades
WO2000053897A1 (en) * 1999-03-11 2000-09-14 Alm Development, Inc. Gas turbine engine
US6305157B1 (en) 1998-09-25 2001-10-23 Alm Development, Inc. Gas turbine engine
US6363708B1 (en) 1999-10-12 2002-04-02 Alm Development, Inc. Gas turbine engine
US6397576B1 (en) 1999-10-12 2002-06-04 Alm Development, Inc. Gas turbine engine with exhaust compressor having outlet tap control
US6442945B1 (en) 2000-08-04 2002-09-03 Alm Development, Inc. Gas turbine engine
US6460324B1 (en) 1999-10-12 2002-10-08 Alm Development, Inc. Gas turbine engine
EP1591626A1 (en) * 2004-04-30 2005-11-02 Alstom Technology Ltd Blade for gas turbine
US8549862B2 (en) 2009-09-13 2013-10-08 Lean Flame, Inc. Method of fuel staging in combustion apparatus

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3597102A (en) * 1968-06-10 1971-08-03 English Electric Co Ltd Turbines
FR2384949A1 (en) * 1977-03-26 1978-10-20 Rolls Royce SEALING DEVICE FOR GAS TURBINE ROTOR
FR2426159A1 (en) * 1978-05-20 1979-12-14 Rolls Royce REFRIGERANT AIR SUPPLY DEVICE FOR GAS TURBINE ENGINE
US4732531A (en) * 1986-08-11 1988-03-22 National Aerospace Laboratory of Science and Technoloyg Agency Air sealed turbine blades
US6305157B1 (en) 1998-09-25 2001-10-23 Alm Development, Inc. Gas turbine engine
WO2000053897A1 (en) * 1999-03-11 2000-09-14 Alm Development, Inc. Gas turbine engine
US6460324B1 (en) 1999-10-12 2002-10-08 Alm Development, Inc. Gas turbine engine
US6363708B1 (en) 1999-10-12 2002-04-02 Alm Development, Inc. Gas turbine engine
US6397576B1 (en) 1999-10-12 2002-06-04 Alm Development, Inc. Gas turbine engine with exhaust compressor having outlet tap control
US6442945B1 (en) 2000-08-04 2002-09-03 Alm Development, Inc. Gas turbine engine
EP1591626A1 (en) * 2004-04-30 2005-11-02 Alstom Technology Ltd Blade for gas turbine
WO2005106208A1 (en) * 2004-04-30 2005-11-10 Alstom Technology Ltd Blade for a gas turbine
US7273347B2 (en) 2004-04-30 2007-09-25 Alstom Technology Ltd. Blade for a gas turbine
AU2005238655B2 (en) * 2004-04-30 2010-08-26 General Electric Technology Gmbh Blade for a gas turbine
AU2005238655C1 (en) * 2004-04-30 2011-06-09 General Electric Technology Gmbh Blade for a gas turbine
US8549862B2 (en) 2009-09-13 2013-10-08 Lean Flame, Inc. Method of fuel staging in combustion apparatus
US8689561B2 (en) 2009-09-13 2014-04-08 Donald W. Kendrick Vortex premixer for combustion apparatus
US8689562B2 (en) 2009-09-13 2014-04-08 Donald W. Kendrick Combustion cavity layouts for fuel staging in trapped vortex combustors

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