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FR975879A - Further training in the construction of cylinders for gas turbines - Google Patents

Further training in the construction of cylinders for gas turbines

Info

Publication number
FR975879A
FR975879A FR975879DA FR975879A FR 975879 A FR975879 A FR 975879A FR 975879D A FR975879D A FR 975879DA FR 975879 A FR975879 A FR 975879A
Authority
FR
France
Prior art keywords
cylinders
construction
gas turbines
further training
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)
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.)
CONST ET D EQUIPEMENTS MECANIQ
Original Assignee
CONST ET D EQUIPEMENTS MECANIQ
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 CONST ET D EQUIPEMENTS MECANIQ filed Critical CONST ET D EQUIPEMENTS MECANIQ
Application granted granted Critical
Publication of FR975879A publication Critical patent/FR975879A/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
    • F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
    • F01D11/16—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means
    • F01D11/18—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means using stator or rotor components with predetermined thermal response, e.g. selective insulation, thermal inertia, differential expansion

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR975879D 1948-12-06 1948-12-06 Further training in the construction of cylinders for gas turbines Expired FR975879A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR975879T 1948-12-06

Publications (1)

Publication Number Publication Date
FR975879A true FR975879A (en) 1951-03-12

Family

ID=9518372

Family Applications (1)

Application Number Title Priority Date Filing Date
FR975879D Expired FR975879A (en) 1948-12-06 1948-12-06 Further training in the construction of cylinders for gas turbines

Country Status (1)

Country Link
FR (1) FR975879A (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2930521A (en) * 1955-08-17 1960-03-29 Gen Motors Corp Gas turbine structure
US3070353A (en) * 1958-12-03 1962-12-25 Gen Motors Corp Shroud assembly
US3173605A (en) * 1963-06-21 1965-03-16 Rotron Mfg Co Fan housing
US3243158A (en) * 1964-01-15 1966-03-29 United Aircraft Corp Turbine construction
DE1259142B (en) * 1962-02-14 1968-01-18 Licentia Gmbh Ring flange of the tubular inner or outer housing of an axial gas or steam turbine
FR2482662A1 (en) * 1980-05-16 1981-11-20 Mtu Muenchen Gmbh EXTERNAL HOUSING FOR AXIAL COMPRESSOR OR AXIAL TURBINE OF A FLUIDIC MACHINE
FR2607198A1 (en) * 1986-11-26 1988-05-27 Snecma COMPRESSOR HOUSING SUITABLE FOR ACTIVE PILOTAGE OF ITS EXPANSIONS AND MANUFACTURING METHOD THEREOF
US5161940A (en) * 1991-06-21 1992-11-10 Pratt & Whitney Canada, Inc. Annular support
US5181826A (en) * 1990-11-23 1993-01-26 General Electric Company Attenuating shroud support
EP0651139A1 (en) * 1993-10-27 1995-05-03 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Turbomachine with means to control the tip clearance between rotor and stator
US6099165A (en) * 1999-01-19 2000-08-08 Pratt & Whitney Canada Corp. Soft bearing support

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2930521A (en) * 1955-08-17 1960-03-29 Gen Motors Corp Gas turbine structure
US3070353A (en) * 1958-12-03 1962-12-25 Gen Motors Corp Shroud assembly
DE1259142B (en) * 1962-02-14 1968-01-18 Licentia Gmbh Ring flange of the tubular inner or outer housing of an axial gas or steam turbine
US3173605A (en) * 1963-06-21 1965-03-16 Rotron Mfg Co Fan housing
US3243158A (en) * 1964-01-15 1966-03-29 United Aircraft Corp Turbine construction
FR2482662A1 (en) * 1980-05-16 1981-11-20 Mtu Muenchen Gmbh EXTERNAL HOUSING FOR AXIAL COMPRESSOR OR AXIAL TURBINE OF A FLUIDIC MACHINE
FR2607198A1 (en) * 1986-11-26 1988-05-27 Snecma COMPRESSOR HOUSING SUITABLE FOR ACTIVE PILOTAGE OF ITS EXPANSIONS AND MANUFACTURING METHOD THEREOF
EP0273790A1 (en) * 1986-11-26 1988-07-06 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Compressor housing adapted for active regulated thermal dilatation, and method for its production
US4762462A (en) * 1986-11-26 1988-08-09 Societe Nationale D'etude Et De Construction De Moteurs D'aviation (Snecma) Housing for an axial compressor
US5181826A (en) * 1990-11-23 1993-01-26 General Electric Company Attenuating shroud support
US5161940A (en) * 1991-06-21 1992-11-10 Pratt & Whitney Canada, Inc. Annular support
EP0651139A1 (en) * 1993-10-27 1995-05-03 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Turbomachine with means to control the tip clearance between rotor and stator
FR2711730A1 (en) * 1993-10-27 1995-05-05 Snecma Turbomachine equipped with means for controlling the clearances between the rotor and the stator.
US6099165A (en) * 1999-01-19 2000-08-08 Pratt & Whitney Canada Corp. Soft bearing support

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