FR2592916A1 - Dispositif permettant l'amelioration et l'extension de l'utilisation des turbo-compresseurs dans les moteurs thermiques. - Google Patents

Dispositif permettant l'amelioration et l'extension de l'utilisation des turbo-compresseurs dans les moteurs thermiques.

Info

Publication number
FR2592916A1
FR2592916A1 FR8600420A FR8600420A FR2592916A1 FR 2592916 A1 FR2592916 A1 FR 2592916A1 FR 8600420 A FR8600420 A FR 8600420A FR 8600420 A FR8600420 A FR 8600420A FR 2592916 A1 FR2592916 A1 FR 2592916A1
Authority
FR
France
Prior art keywords
heat engine
extension
improvement
device allowing
actuating
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.)
Withdrawn
Application number
FR8600420A
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.)
RIVART JEAN CLAUDE
Original Assignee
RIVART JEAN CLAUDE
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 RIVART JEAN CLAUDE filed Critical RIVART JEAN CLAUDE
Priority to FR8600420A priority Critical patent/FR2592916A1/fr
Publication of FR2592916A1 publication Critical patent/FR2592916A1/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/10—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output supplying working fluid to a user, e.g. a chemical process, which returns working fluid to a turbine of the plant
    • F02C6/12—Turbochargers, i.e. plants for augmenting mechanical power output of internal-combustion piston engines by increase of charge pressure
    • 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
    • F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
    • F01D15/10—Adaptations for driving, or combinations with, electric generators
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B39/00—Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00
    • F02B39/02—Drives of pumps; Varying pump drive gear ratio
    • F02B39/08—Non-mechanical drives, e.g. fluid drives having variable gear ratio
    • F02B39/10—Non-mechanical drives, e.g. fluid drives having variable gear ratio electric
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/107—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with two or more rotors connected by power transmission
    • F02C3/113—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with two or more rotors connected by power transmission with variable power transmission between rotors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Supercharger (AREA)

Abstract

L'invention consiste à utiliser pour augmenter la puissance d'un moteur thermique 5, au lieu d'un seul dispositif (turbo-compresseur) deux dispositifs séparés, l'un étant chargé de la récupération de l'énergie dans les gaz d'échappement, l'organe de récupération 1 actionnant un moyen de production d'électricité 2 par ex-alternateur, l'autre comprendra un moteur électrique 3 actionnant un dispositif de compression de l'air d'admission 4 ce qui permet d'éviter le "trou" du turbo-compresseur actuel, facilite le montage, permet le montage sur moteur thermique existant, supprime la soupape de régulation et permet de disposer de la puissance maxi à tous les régimes. La présente invention peut être utilisée avec n'importe quel moteur thermique et notamment ceux qui équipent les automobiles. (CF DESSIN DANS BOPI)
FR8600420A 1986-01-14 1986-01-14 Dispositif permettant l'amelioration et l'extension de l'utilisation des turbo-compresseurs dans les moteurs thermiques. Withdrawn FR2592916A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR8600420A FR2592916A1 (fr) 1986-01-14 1986-01-14 Dispositif permettant l'amelioration et l'extension de l'utilisation des turbo-compresseurs dans les moteurs thermiques.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8600420A FR2592916A1 (fr) 1986-01-14 1986-01-14 Dispositif permettant l'amelioration et l'extension de l'utilisation des turbo-compresseurs dans les moteurs thermiques.

Publications (1)

Publication Number Publication Date
FR2592916A1 true FR2592916A1 (fr) 1987-07-17

Family

ID=9331082

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8600420A Withdrawn FR2592916A1 (fr) 1986-01-14 1986-01-14 Dispositif permettant l'amelioration et l'extension de l'utilisation des turbo-compresseurs dans les moteurs thermiques.

Country Status (1)

Country Link
FR (1) FR2592916A1 (fr)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2004011790A1 (fr) * 2002-07-30 2004-02-05 Honeywell International Inc. Generateur et/ou surpresseur electriques
GB2477548A (en) * 2010-02-05 2011-08-10 Graham Michael North Decoupled gas turbine engine
CN102482988A (zh) * 2009-08-28 2012-05-30 瓦锡兰芬兰有限公司 内燃发动机装置
US8584459B2 (en) 2006-12-09 2013-11-19 Aeristech Limited Engine induction system
US20160138463A1 (en) * 2014-11-17 2016-05-19 Arnold Magnetic Technologies System and method for providing multiple voltage buses on a single vehicle

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2004011790A1 (fr) * 2002-07-30 2004-02-05 Honeywell International Inc. Generateur et/ou surpresseur electriques
US8584459B2 (en) 2006-12-09 2013-11-19 Aeristech Limited Engine induction system
CN102482988A (zh) * 2009-08-28 2012-05-30 瓦锡兰芬兰有限公司 内燃发动机装置
EP2470762B1 (fr) * 2009-08-28 2015-08-26 Wärtsilä Finland Oy Agencement de moteur à combustion interne
GB2477548A (en) * 2010-02-05 2011-08-10 Graham Michael North Decoupled gas turbine engine
US20160138463A1 (en) * 2014-11-17 2016-05-19 Arnold Magnetic Technologies System and method for providing multiple voltage buses on a single vehicle

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Legal Events

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ST Notification of lapse