[PDF] Development Of Advanced In Cylinder Components And Tribological Systems For Low Heat Rejection Diesel Engines Phases 2 3 And 4 - eBooks Review

Development Of Advanced In Cylinder Components And Tribological Systems For Low Heat Rejection Diesel Engines Phases 2 3 And 4


Development Of Advanced In Cylinder Components And Tribological Systems For Low Heat Rejection Diesel Engines Phases 2 3 And 4
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Development Of Advanced In Cylinder Components And Tribological Systems For Low Heat Rejection Diesel Engines Phases 2 3 And 4 Final Report


Development Of Advanced In Cylinder Components And Tribological Systems For Low Heat Rejection Diesel Engines Phases 2 3 And 4 Final Report
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Author :
language : en
Publisher:
Release Date : 1999

Development Of Advanced In Cylinder Components And Tribological Systems For Low Heat Rejection Diesel Engines Phases 2 3 And 4 Final Report written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1999 with categories.




Development Of Advanced In Cylinder Components And Tribological Systems For Low Heat Rejection Diesel Engines Phases 2 3 And 4


Development Of Advanced In Cylinder Components And Tribological Systems For Low Heat Rejection Diesel Engines Phases 2 3 And 4
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Author : T. M. Yonushonis
language : en
Publisher:
Release Date : 1999

Development Of Advanced In Cylinder Components And Tribological Systems For Low Heat Rejection Diesel Engines Phases 2 3 And 4 written by T. M. Yonushonis and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1999 with categories.


In-cylinder components and tribological system concepts were designed, fabricated and tested at conditions anticipated for a 55% thermal efficiency heavy duty diesel engine for the year 2000 and beyond. A Cummins L10 single cylinder research engine was used to evaluate a spherical joint piston and connecting rod with 19.3 MPa (2800 psi) peak cylinder pressure capability, a thermal fatigue resistant insulated cylinder head, radial combustion seal cylinder liners, a highly compliant steel top compression ring, a variable geometry turbocharger, and a microwave heated particulate trap. Components successfully demonstrated in the final test included spherical joint connecting rod with a fiber reinforced piston, high conformability steel top rings with wear resistant coatings, ceramic exhaust ports with strategic oil cooling and radial combustion seal cylinder liner with cooling jacket transfer fins. A Cummins 6B diesel was used to develop the analytical methods, materials, manufacturing technology and engine components for lighter weight diesel engines without sacrificing performance or durability. A 6B diesel engine was built and tested to calibrate analytical models for the aluminum cylinder head and aluminum block.



Development Of Advanced In Cylinder Components And Tribological Systems For Low Heat Rejection Diesel Engines


Development Of Advanced In Cylinder Components And Tribological Systems For Low Heat Rejection Diesel Engines
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Author : National Aeronautics and Space Administration (NASA)
language : en
Publisher: Createspace Independent Publishing Platform
Release Date : 2018-06-27

Development Of Advanced In Cylinder Components And Tribological Systems For Low Heat Rejection Diesel Engines written by National Aeronautics and Space Administration (NASA) and has been published by Createspace Independent Publishing Platform this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-06-27 with categories.


In-cylinder components and tribological system concepts were designed, fabricated and tested at conditions anticipated for a 55% thermal efficiency heavy duty diesel engine for the year 2000 and beyond. A Cummins L10 single cylinder research engine was used to evaluate a spherical joint piston and connecting rod with 19.3 MPa (2800 psi) peak cylinder pressure capability, a thermal fatigue resistant insulated cylinder head, radial combustion seal cylinder liners, a highly compliant steel top compression ring, a variable geometry turbocharger, and a microwave heated particulate trap. Components successfully demonstrated in the final test included spherical joint connecting rod with a fiber reinforced piston, high conformability steel top rings with wear resistant coatings, ceramic exhaust ports with strategic oil cooling and radial combustion seal cylinder liner with cooling jacket transfer fins. A Cummins 6B diesel was used to develop the analytical methods, materials, manufacturing technology and engine components for lighter weight diesel engines without sacrificing performance or durability. A 6B diesel engine was built and tested to calibrate analytical models for the aluminum cylinder head and aluminum block. Yonushonis, T. M. and Wiczynski, P. D. and Myers, M. R. and Anderson, D. D. and McDonald, A. C. and Weber, H. G. and Richardson, D. E. and Stafford, R. J. and Naylor, M. G. Glenn Research Center DEN3-375; DE-AI05-960R22547



Development Of Advanced High Temperature In Cylinder Components And Tribological Systems For Low Heat Rejection Diesel Engines Phase 1


Development Of Advanced High Temperature In Cylinder Components And Tribological Systems For Low Heat Rejection Diesel Engines Phase 1
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Author : National Aeronautics and Space Administration (NASA)
language : en
Publisher: Createspace Independent Publishing Platform
Release Date : 2018-07-06

Development Of Advanced High Temperature In Cylinder Components And Tribological Systems For Low Heat Rejection Diesel Engines Phase 1 written by National Aeronautics and Space Administration (NASA) and has been published by Createspace Independent Publishing Platform this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-07-06 with categories.


Analysis and concept design work completed in Phase 1 have identified a low heat rejection engine configuration with the potential to meet the Heavy Duty Transport Technology program specific fuel consumption goal of 152 g/kW-hr. The proposed engine configuration incorporates low heat rejection, in-cylinder components designed for operation at 24 MPa peak cylinder pressure. Water cooling is eliminated by selective oil cooling of the components. A high temperature lubricant will be required due to increased in-cylinder operating temperatures. A two-stage turbocharger air system with intercooling and aftercooling was selected to meet engine boost and BMEP requirements. A turbocompound turbine stage is incorporated for exhaust energy recovery. The concept engine cost was estimated to be 43 percent higher compared to a Caterpillar 3176 engine. The higher initial engine cost is predicted to be offset by reduced operating costs due the lower fuel consumption. Kroeger, C. A. and Larson, H. J. Unspecified Center...



Development Of An Advanced High Temperature In Cylinder Components And Tribological Systems For Low Heat Rejection Diesel Engines Phase 1 Final Report


Development Of An Advanced High Temperature In Cylinder Components And Tribological Systems For Low Heat Rejection Diesel Engines Phase 1 Final Report
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Author : C. A. Kroeger
language : en
Publisher:
Release Date : 1992

Development Of An Advanced High Temperature In Cylinder Components And Tribological Systems For Low Heat Rejection Diesel Engines Phase 1 Final Report written by C. A. Kroeger and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with categories.




Energy Research Abstracts


Energy Research Abstracts
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Author :
language : en
Publisher:
Release Date : 1991-10

Energy Research Abstracts written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1991-10 with Power resources categories.




Preprints Of The Annual Automotive Technology Development Contractors Coordination Meeting


Preprints Of The Annual Automotive Technology Development Contractors Coordination Meeting
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Author :
language : en
Publisher:
Release Date : 1989

Preprints Of The Annual Automotive Technology Development Contractors Coordination Meeting written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1989 with Engines categories.




Scientific And Technical Aerospace Reports


Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1995

Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1995 with Aeronautics categories.


Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.



Advanced Diesel Engine Component Development Program Tasks 4 14


Advanced Diesel Engine Component Development Program Tasks 4 14
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Author :
language : en
Publisher:
Release Date : 1994

Advanced Diesel Engine Component Development Program Tasks 4 14 written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1994 with categories.




Program Solicitation


Program Solicitation
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Author :
language : en
Publisher:
Release Date : 1989

Program Solicitation written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1989 with Military research categories.