AU2460684A - Turbocompound system - Google Patents

Turbocompound system

Info

Publication number
AU2460684A
AU2460684A AU24606/84A AU2460684A AU2460684A AU 2460684 A AU2460684 A AU 2460684A AU 24606/84 A AU24606/84 A AU 24606/84A AU 2460684 A AU2460684 A AU 2460684A AU 2460684 A AU2460684 A AU 2460684A
Authority
AU
Australia
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.)
Abandoned
Application number
AU24606/84A
Inventor
Adell Warren II Brecheisen
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 AU2460684A publication Critical patent/AU2460684A/en
Abandoned 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

Landscapes

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

Abstract

The engine has a fuel and air intake, an exhaust outlet and an output drive shaft. A turbocharger has a turbine with an inlet and an outlet and a compressor with an inlet and an outlet. The turbine inlet is communicated with the engine exhaust outlet and the compressor outlet with the engine air intake. An auxiliary combustion chamber receives exhaust gases from the turbine outlet of the turbocharger. A power turbine is coupled to the drive shaft and driven by exhaust gases from the auxiliary combustion chamber for supplying auxiliary power to the drive shaft. -
AU24606/84A 1983-03-14 1984-02-15 Turbocompound system Abandoned AU2460684A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US47475983A 1983-03-14 1983-03-14
US474759 1983-03-14

Publications (1)

Publication Number Publication Date
AU2460684A true AU2460684A (en) 1984-09-20

Family

ID=23884824

Family Applications (1)

Application Number Title Priority Date Filing Date
AU24606/84A Abandoned AU2460684A (en) 1983-03-14 1984-02-15 Turbocompound system

Country Status (4)

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

Cited By (1)

* 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

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BR102017008570A2 (en) * 2017-04-26 2018-11-21 Associacao Paranaense De Cultura - Apc diesel and binary-isobaric-adiabatic combined cycle engine and process control for the thermodynamic cycle of the combined cycle engine

Cited By (1)

* 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

Also Published As

Publication number Publication date
ES530542A0 (en) 1985-02-01
ES8507224A1 (en) 1985-02-01
JPS59176420A (en) 1984-10-05
BR8400959A (en) 1984-10-23

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