FR1111358A - Adjustable casing ring segments for gas turbines - Google Patents

Adjustable casing ring segments for gas turbines

Info

Publication number
FR1111358A
FR1111358A FR1111358DA FR1111358A FR 1111358 A FR1111358 A FR 1111358A FR 1111358D A FR1111358D A FR 1111358DA FR 1111358 A FR1111358 A FR 1111358A
Authority
FR
France
Prior art keywords
gas turbines
ring segments
casing ring
adjustable casing
adjustable
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.)
Canadian Patents and Development Ltd
Original Assignee
Canadian Patents 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 Canadian Patents and Development Ltd filed Critical Canadian Patents and Development Ltd
Application granted granted Critical
Publication of FR1111358A publication Critical patent/FR1111358A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/14Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR1111358D 1954-02-04 1954-10-29 Adjustable casing ring segments for gas turbines Expired FR1111358A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US1111358XA 1954-02-04 1954-02-04

Publications (1)

Publication Number Publication Date
FR1111358A true FR1111358A (en) 1956-02-27

Family

ID=22336806

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1111358D Expired FR1111358A (en) 1954-02-04 1954-10-29 Adjustable casing ring segments for gas turbines

Country Status (1)

Country Link
FR (1) FR1111358A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3313475A (en) * 1965-07-29 1967-04-11 Gen Electric Mounting of hardware on axial flow compressor casings
US3325087A (en) * 1965-04-28 1967-06-13 David R Davis Stator casing construction for gas turbine engines
FR2540938A1 (en) * 1983-02-10 1984-08-17 Snecma Turbine ring for a turbine machine
EP0375593A1 (en) * 1988-12-21 1990-06-27 United Technologies Corporation Adjustable spacer
FR2651832A1 (en) * 1989-09-08 1991-03-15 Gen Electric RADIAL ADJUSTMENT MECHANISM FOR A DEVICE FOR CONTROLLING THE PLAY OF THE END OF AUBES.

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3325087A (en) * 1965-04-28 1967-06-13 David R Davis Stator casing construction for gas turbine engines
US3313475A (en) * 1965-07-29 1967-04-11 Gen Electric Mounting of hardware on axial flow compressor casings
FR2540938A1 (en) * 1983-02-10 1984-08-17 Snecma Turbine ring for a turbine machine
EP0375593A1 (en) * 1988-12-21 1990-06-27 United Technologies Corporation Adjustable spacer
FR2651832A1 (en) * 1989-09-08 1991-03-15 Gen Electric RADIAL ADJUSTMENT MECHANISM FOR A DEVICE FOR CONTROLLING THE PLAY OF THE END OF AUBES.

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