FR1303779A - Turbine à gaz - Google Patents

Turbine à gaz

Info

Publication number
FR1303779A
FR1303779A FR875924A FR875924A FR1303779A FR 1303779 A FR1303779 A FR 1303779A FR 875924 A FR875924 A FR 875924A FR 875924 A FR875924 A FR 875924A FR 1303779 A FR1303779 A FR 1303779A
Authority
FR
France
Prior art keywords
gas turbine
turbine
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
FR875924A
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.)
KOHNLE AG
Howden Turbo GmbH
Original Assignee
KOHNLE AG
Siemens Turbomachinery Equipment GmbH
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
Priority to NL270226D priority Critical patent/NL270226A/xx
Application filed by KOHNLE AG, Siemens Turbomachinery Equipment GmbH filed Critical KOHNLE AG
Priority to FR875924A priority patent/FR1303779A/fr
Application granted granted Critical
Publication of FR1303779A publication Critical patent/FR1303779A/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
    • F01D17/167—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes of vanes moving in translation
    • 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
    • F05D2220/00—Application
    • F05D2220/40—Application in turbochargers

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR875924A 1961-10-13 1961-10-13 Turbine à gaz Expired FR1303779A (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
NL270226D NL270226A (fr) 1961-10-13
FR875924A FR1303779A (fr) 1961-10-13 1961-10-13 Turbine à gaz

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR875924A FR1303779A (fr) 1961-10-13 1961-10-13 Turbine à gaz

Publications (1)

Publication Number Publication Date
FR1303779A true FR1303779A (fr) 1962-09-14

Family

ID=8764658

Family Applications (1)

Application Number Title Priority Date Filing Date
FR875924A Expired FR1303779A (fr) 1961-10-13 1961-10-13 Turbine à gaz

Country Status (2)

Country Link
FR (1) FR1303779A (fr)
NL (1) NL270226A (fr)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4183209A (en) * 1976-09-24 1980-01-15 Kronogard Sven Olof Gas turbine guide apparatus
WO2004009961A1 (fr) * 2002-07-20 2004-01-29 Daimlerchrysler Ag Turbocompresseur a gaz d'echappement pour moteur a combustion
WO2004074643A1 (fr) * 2003-02-19 2004-09-02 Honeywell International Inc. Ajutage pour turbocompresseur et procede de commande associe
US7412830B2 (en) * 2003-06-30 2008-08-19 Daimler Ag Compressor in the induction tract of an internal combustion engine
WO2013156048A1 (fr) * 2012-04-19 2013-10-24 Ihi Charging Systems International Gmbh Turbine à géométrie de turbine variable pour turbocompresseur à gaz d'échappement

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4183209A (en) * 1976-09-24 1980-01-15 Kronogard Sven Olof Gas turbine guide apparatus
WO2004009961A1 (fr) * 2002-07-20 2004-01-29 Daimlerchrysler Ag Turbocompresseur a gaz d'echappement pour moteur a combustion
US7350356B2 (en) * 2002-07-20 2008-04-01 Daimler Ag Exhaust gas turbocharger for an internal combustion engine
WO2004074643A1 (fr) * 2003-02-19 2004-09-02 Honeywell International Inc. Ajutage pour turbocompresseur et procede de commande associe
US7412830B2 (en) * 2003-06-30 2008-08-19 Daimler Ag Compressor in the induction tract of an internal combustion engine
WO2013156048A1 (fr) * 2012-04-19 2013-10-24 Ihi Charging Systems International Gmbh Turbine à géométrie de turbine variable pour turbocompresseur à gaz d'échappement
WO2013156047A3 (fr) * 2012-04-19 2014-02-20 Ihi Charging Systems International Gmbh Turbine pour turbocompresseur à gaz d'échappement

Also Published As

Publication number Publication date
NL270226A (fr)

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