ES8507224A1 - Sistema compuesto turboalimentado - Google Patents

Sistema compuesto turboalimentado

Info

Publication number
ES8507224A1
ES8507224A1 ES530542A ES530542A ES8507224A1 ES 8507224 A1 ES8507224 A1 ES 8507224A1 ES 530542 A ES530542 A ES 530542A ES 530542 A ES530542 A ES 530542A ES 8507224 A1 ES8507224 A1 ES 8507224A1
Authority
ES
Spain
Prior art keywords
outlet
turbine
drive shaft
inlet
engine
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
ES530542A
Other languages
English (en)
Other versions
ES530542A0 (es
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.)
Deere and Co
Original Assignee
Deere and Co
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 Deere and Co filed Critical Deere and Co
Publication of ES530542A0 publication Critical patent/ES530542A0/es
Publication of ES8507224A1 publication Critical patent/ES8507224A1/es
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F02B41/00—Engines characterised by special means for improving conversion of heat or pressure energy into mechanical power
    • F02B41/02—Engines with prolonged expansion
    • F02B41/10—Engines with prolonged expansion in exhaust turbines
    • 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
    • F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/12—Control of the pumps
    • F02B37/16—Control of the pumps by bypassing charging air
    • F02B37/164—Control of the pumps by bypassing charging air the bypassed air being used in an auxiliary apparatus, e.g. in an air turbine
    • F02B37/166—Control of the pumps by bypassing charging air the bypassed air being used in an auxiliary apparatus, e.g. in an air turbine the auxiliary apparatus being a combustion chamber, e.g. upstream of turbine
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/10—Internal combustion engine [ICE] based vehicles
    • Y02T10/12—Improving ICE efficiencies

Abstract

SISTEMA COMPUESTO TURBOALIMENTADO.CONSTA DE: UNA MAQUINA MOTRIZ DE COMBUSTION (12) CON UN SUMINISTRO (18) DE COMBUSTIBLE; UNA ENTRADA (14) DE AIRE DE COMBUSTION; UNA SALIDA (16) DE GASES DE ESCAPE Y UN ARBOL DE SALIDA (46): UN TURBOALIMENTADOR (20) DE GASES DE ESCAPE CON UNA TURBINA (21) QUE TIENE UNA ENTRADA Y UNA SALIDA DE GASES DE ESCAPE, Y UN COMPRESOR (22) CON ENTRADA Y SALIDA DE AIRE; UNA CAMARA DE POSTCOMBUSTION (30) EN LA QUE SE INTRODUCE EL GAS DE ESCAPE DE LA MAQUINA; Y UNA TURBINA DE ACCIONAMIENTO (44) ACCIONADA POR EL GAS DE ESCAPE PROCEDENTE DE LA CAMARA DE POSTCOMBUSTION (30) Y UNIDA CON EL ARBOL DE SALIDA (46).
ES530542A 1983-03-14 1984-03-13 Sistema compuesto turboalimentado Expired ES8507224A1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US47475983A 1983-03-14 1983-03-14

Publications (2)

Publication Number Publication Date
ES530542A0 ES530542A0 (es) 1985-02-01
ES8507224A1 true ES8507224A1 (es) 1985-02-01

Family

ID=23884824

Family Applications (1)

Application Number Title Priority Date Filing Date
ES530542A Expired ES8507224A1 (es) 1983-03-14 1984-03-13 Sistema compuesto turboalimentado

Country Status (4)

Country Link
JP (1) JPS59176420A (es)
AU (1) AU2460684A (es)
BR (1) BR8400959A (es)
ES (1) ES8507224A1 (es)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU571015B2 (en) * 1984-07-13 1988-03-31 Caterpillar Inc. Turbocompound engine with turbine connected to timing gear
BR102017008570A2 (pt) * 2017-04-26 2018-11-21 Associacao Paranaense De Cultura - Apc motor de ciclo combinado diesel e binário-isobárico-adiabático e processo de controle para o ciclo termodinâmico do motor de ciclo combinado

Also Published As

Publication number Publication date
ES530542A0 (es) 1985-02-01
BR8400959A (pt) 1984-10-23
JPS59176420A (ja) 1984-10-05
AU2460684A (en) 1984-09-20

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