FR822695A - Perfectionnements aux dispositifs de réglage pour turbines à vapeur et à gaz - Google Patents

Perfectionnements aux dispositifs de réglage pour turbines à vapeur et à gaz

Info

Publication number
FR822695A
FR822695A FR822695DA FR822695A FR 822695 A FR822695 A FR 822695A FR 822695D A FR822695D A FR 822695DA FR 822695 A FR822695 A FR 822695A
Authority
FR
France
Prior art keywords
regulators
steam
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.)
Goetaverken AB
Original Assignee
Goetaverken AB
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 Goetaverken AB filed Critical Goetaverken AB
Application granted granted Critical
Publication of FR822695A publication Critical patent/FR822695A/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
    • 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
    • F01D17/18—Final actuators arranged in stator parts varying effective number of nozzles or guide conduits, e.g. sequentially operable valves for steam turbines

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
FR822695D 1935-12-07 1937-06-04 Perfectionnements aux dispositifs de réglage pour turbines à vapeur et à gaz Expired FR822695A (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
SE479889X 1935-12-07
DEA83092D DE756302C (de) 1935-12-07 1937-05-28 Regelungsvorrichtung fuer Niederdruckdampf- oder Niederdruckgasturbinen
FR822695T 1937-06-04

Publications (1)

Publication Number Publication Date
FR822695A true FR822695A (fr) 1938-01-05

Family

ID=20310443

Family Applications (1)

Application Number Title Priority Date Filing Date
FR822695D Expired FR822695A (fr) 1935-12-07 1937-06-04 Perfectionnements aux dispositifs de réglage pour turbines à vapeur et à gaz

Country Status (3)

Country Link
DE (1) DE756302C (fr)
FR (1) FR822695A (fr)
GB (1) GB479889A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2608678A1 (fr) * 1986-12-17 1988-06-24 Snecma Dispositif de commande d'aubes a calage variable de redresseur de turbomachine

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2759718A (en) * 1953-06-17 1956-08-21 James G Culbertson Internal combustion engine carburetor
US2815188A (en) * 1954-01-11 1957-12-03 Marquardt Aircraft Co Auxiliary power unit
US2828066A (en) * 1954-07-05 1958-03-25 Sulzer Ag Turbocompressor plant
US2988327A (en) * 1956-02-03 1961-06-13 Plessey Co Ltd Emergency power systems for aircraft auxiliary apparatus
US2835470A (en) * 1956-02-17 1958-05-20 Piessey Company Ltd Fluid turbines
US8505299B2 (en) 2010-07-14 2013-08-13 General Electric Company Steam turbine flow adjustment system
US10767564B2 (en) 2017-03-17 2020-09-08 Hamilton Sunstrand Corporation Air turbine starter with automated variable inlet vanes

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1978809A (en) * 1931-05-26 1934-10-30 Moody Lewis Ferry Hydraulic apparatus
US2037395A (en) * 1935-04-26 1936-04-14 Alfred E Seelig Multistage fan

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2608678A1 (fr) * 1986-12-17 1988-06-24 Snecma Dispositif de commande d'aubes a calage variable de redresseur de turbomachine
EP0274931A2 (fr) * 1986-12-17 1988-07-20 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Dispositif de commande d'aubes à calage variable de redresseur de turbomachine
EP0274931A3 (en) * 1986-12-17 1988-07-27 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Adjusting device for the stator vanes of a turbo machine
US4773821A (en) * 1986-12-17 1988-09-27 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Control mechanism for variably settable vanes of a flow straightener in a turbine plant

Also Published As

Publication number Publication date
DE756302C (de) 1951-08-06
GB479889A (en) 1938-02-14

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