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FR1062311A - Perfectionnements aux turbines à gaz - Google Patents

Perfectionnements aux turbines à gaz

Info

Publication number
FR1062311A
FR1062311A FR1062311DA FR1062311A FR 1062311 A FR1062311 A FR 1062311A FR 1062311D A FR1062311D A FR 1062311DA FR 1062311 A FR1062311 A FR 1062311A
Authority
FR
France
Prior art keywords
gas turbines
turbines
gas
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
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.)
Metropolitan Vickers Electrical Co Ltd
Original Assignee
Metropolitan Vickers Electrical Co 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 Metropolitan Vickers Electrical Co Ltd filed Critical Metropolitan Vickers Electrical Co Ltd
Application granted granted Critical
Publication of FR1062311A publication Critical patent/FR1062311A/fr
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
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/246—Fastening of diaphragms or stator-rings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/11—Shroud seal segments

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR1062311D 1951-10-19 1952-08-29 Perfectionnements aux turbines à gaz Expired FR1062311A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB312374X 1951-10-19

Publications (1)

Publication Number Publication Date
FR1062311A true FR1062311A (fr) 1954-04-21

Family

ID=10320096

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1062311D Expired FR1062311A (fr) 1951-10-19 1952-08-29 Perfectionnements aux turbines à gaz

Country Status (3)

Country Link
CH (1) CH312374A (fr)
FR (1) FR1062311A (fr)
GB (1) GB721453A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2577281A1 (fr) * 1985-02-13 1986-08-14 Snecma Carter de turbomachine associe a un dispositif pour ajuster le jeu entre aubes mobiles et carter

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2959394A (en) * 1953-12-11 1960-11-08 Havilland Engine Co Ltd Stators of multi-stage axial flow compressors or turbines
NL103792C (fr) * 1954-12-16
US3043564A (en) * 1960-03-14 1962-07-10 United Aircraft Corp Stator construction
GB2239678B (en) * 1989-12-08 1993-03-03 Rolls Royce Plc Gas turbine engine blade shroud assembly
GB9306719D0 (en) * 1993-03-31 1993-06-02 Rolls Royce Plc A turbine assembly for a gas turbine engine
US6142731A (en) * 1997-07-21 2000-11-07 Caterpillar Inc. Low thermal expansion seal ring support
JP2002213207A (ja) * 2001-01-15 2002-07-31 Mitsubishi Heavy Ind Ltd ガスタービン分割環
DE102005013796A1 (de) * 2005-03-24 2006-09-28 Alstom Technology Ltd. Wärmestausegment
DE102005013797A1 (de) * 2005-03-24 2006-09-28 Alstom Technology Ltd. Wärmestausegment

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2577281A1 (fr) * 1985-02-13 1986-08-14 Snecma Carter de turbomachine associe a un dispositif pour ajuster le jeu entre aubes mobiles et carter
US4787817A (en) * 1985-02-13 1988-11-29 Societe Nationale D'etude Et De Construction De Moteurs D-Aviation (Snecma) Device for monitoring clearance between rotor blades and a housing

Also Published As

Publication number Publication date
CH312374A (de) 1955-12-31
GB721453A (en) 1955-01-05

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