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Title: AGT-102 automotive gas turbine. Summary report

Technical Report ·
OSTI ID:5697159

Ultimate program goals were to demonstrate at least a 30 percent fuel economy improvement over a comparable SI reciprocating engine, operation within .41 HC, 3.4 CO, and .40 NO/sub x/ grams per mile emissions levels, and the ability to use a variety of alternate fuels. The powertrain concept consists of a single-shaft engine with a ceramic inner shell for containment of hot gases 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 wide-range continuously-variable transmission (CVT), which utilizes gearing and a variable-ratio metal compression belt. A response assist flywheel (RAF) 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. Detailed combustor characterization analytical studies were completed, and preliminary design work was accomplished for the regenerator, aerodynamic components, and the high-speed shaft system. Methods were developed for processing close-tolerance ceramic stationary parts, studies were carried out to characterize ceramic interfacing and brazing, and coatings were developed for the regenerator rubbing seal surface.

Research Organization:
Chrysler Corp., Detroit, MI (USA); Williams Research Corp., Walled Lake, MI (USA)
DOE Contract Number:
AC02-76CS52749
OSTI ID:
5697159
Report Number(s):
DOE/NASA/2749-81/1; NASA/CR-165353; ON: DE83016119
Resource Relation:
Other Information: Portions are illegible in microfiche products
Country of Publication:
United States
Language:
English