FR2193429A5 - - Google Patents

Info

Publication number
FR2193429A5
FR2193429A5 FR7325658A FR7325658A FR2193429A5 FR 2193429 A5 FR2193429 A5 FR 2193429A5 FR 7325658 A FR7325658 A FR 7325658A FR 7325658 A FR7325658 A FR 7325658A FR 2193429 A5 FR2193429 A5 FR 2193429A5
Authority
FR
France
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
FR7325658A
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.)
Brown Boveri Sulzer Turbomaschinen AG
Original Assignee
Brown Boveri Sulzer Turbomaschinen AG
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 Brown Boveri Sulzer Turbomaschinen AG filed Critical Brown Boveri Sulzer Turbomaschinen AG
Application granted granted Critical
Publication of FR2193429A5 publication Critical patent/FR2193429A5/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
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/162—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/52—Casings; Connections of working fluid for axial pumps
    • F04D29/54—Fluid-guiding means, e.g. diffusers
    • F04D29/56—Fluid-guiding means, e.g. diffusers adjustable
    • F04D29/563—Fluid-guiding means, e.g. diffusers adjustable specially adapted for elastic fluid pumps
FR7325658A 1972-07-13 1973-07-12 Expired FR2193429A5 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH1051572A CH553921A (en) 1972-07-13 1972-07-13 ADJUSTING DEVICE FOR THE VANES OF AN AXIAL COMPRESSOR.

Publications (1)

Publication Number Publication Date
FR2193429A5 true FR2193429A5 (en) 1974-02-15

Family

ID=4364037

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7325658A Expired FR2193429A5 (en) 1972-07-13 1973-07-12

Country Status (8)

Country Link
US (1) US3860356A (en)
JP (1) JPS5222445B2 (en)
CH (1) CH553921A (en)
DE (1) DE2235188B2 (en)
FR (1) FR2193429A5 (en)
GB (1) GB1378604A (en)
IT (1) IT991104B (en)
NL (1) NL7309567A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2495239A1 (en) * 1980-11-05 1982-06-04 Sulzer Ag Guide blade adjustment for axial flow compressor - has adjusting sleeve for all stages moved by single motor through several rods
FR2681640A1 (en) * 1991-09-25 1993-03-26 Snecma TURBOMACHINE WITH STATOR AUBES WITH VARIABLE TIMING.

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4222708A (en) * 1978-06-26 1980-09-16 General Electric Company Method and apparatus for reducing eccentricity in a turbomachine
GB2392956A (en) * 2002-09-12 2004-03-17 Honeywell Uk Ltd Controlling inlet to turbocharger turbine
US9624933B2 (en) * 2013-08-29 2017-04-18 Dresser-Rand Company Support assembly for a turbomachine

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2861724A (en) * 1954-07-22 1958-11-25 Sidney M Kaplan Condiment shaker
US3094270A (en) * 1958-08-05 1963-06-18 Rolls Royce Annular valve device
GB903236A (en) * 1960-06-07 1962-08-15 Rolls Royce Improvements in and relating to the compressors of gas turbine engines

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2495239A1 (en) * 1980-11-05 1982-06-04 Sulzer Ag Guide blade adjustment for axial flow compressor - has adjusting sleeve for all stages moved by single motor through several rods
FR2681640A1 (en) * 1991-09-25 1993-03-26 Snecma TURBOMACHINE WITH STATOR AUBES WITH VARIABLE TIMING.
US5224820A (en) * 1991-09-25 1993-07-06 Societe Nationale D'etude Et De Construction De Moteurs D'aviation Operating mechanism for variably settable blades of a turbomachine

Also Published As

Publication number Publication date
CH553921A (en) 1974-09-13
JPS5222445B2 (en) 1977-06-17
IT991104B (en) 1975-07-30
DE2235188B2 (en) 1975-08-21
JPS4958407A (en) 1974-06-06
US3860356A (en) 1975-01-14
GB1378604A (en) 1974-12-27
NL7309567A (en) 1974-01-15
DE2235188A1 (en) 1974-02-07

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Legal Events

Date Code Title Description
ST Notification of lapse