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AGT-102 automotive gas turbineDevelopment of a gas turbine powertrain with a 30% fuel economy improvement over a comparable S1 reciprocating engine, operation within 0.41 HC, 3.4 CO, and 0.40 NOx grams per mile emissions levels, and ability to use a variety of alternate fuels is summarized. The powertrain concept consists of a single-shaft engine with a ceramic inner shell for containment of hot gasses and support of twin regenerators. It uses a fixed-geometry, lean, premixed, prevaporized combustor, and a ceramic radial turbine rotor supported by an air-lubricated journal bearing. The engine is coupled to the vehicle through a widerange continuously variable transmission, which utilizes gearing and a variable-ratio metal compression belt. A response assist flywheel is used to achieve acceptable levels of engine response. The package offers a 100 lb weight advantage in a Chrysler K Car front-wheel-drive installation. Initial layout studies, preliminary transient thermal analysis, ceramic inner housing structural analysis, and detailed performance analysis were carried out for the basic engine.
Document ID
19820004571
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 4, 2013
Publication Date
June 1, 1981
Subject Category
Mechanical Engineering
Report/Patent Number
DOE/NASA/2749-81/1
NASA-CR-165353
Report Number: DOE/NASA/2749-81/1
Report Number: NASA-CR-165353
Accession Number
82N12444
Funding Number(s)
CONTRACT_GRANT: DE-AC02-76CS-52749
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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