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Conceptual design study of an improved automotive gas turbine powertrainAutomotive gas turbine concepts with significant technological advantages over the spark ignition (SI) engine were assessed. Possible design concepts were rated with respect to fuel economy and near-term application. A program plan which outlines the development of the improved gas turbine (IGT) concept that best met the goals and objectives of the study identifies the research and development work needed to meet the goal of entering a production engineering phase by 1983. The fuel economy goal is to show at least a 20% improvement over a conventional 1976 SI engine/vehicle system. On the basis of achieving the fuel economy goal, of overall suitability to mechanical design, and of automotive mass production cost, the powertrain selected was a single-shaft engine with a radial turbine and a continuously variable transmission (CVT). Design turbine inlet temperature was 1150 C. Reflecting near-term technology, the turbine rotor would be made of an advanced superalloy, and the transmission would be a hydromechanical CVT. With successful progress in long-lead R&D in ceramic technology and the belt-drive CVT, the turbine inlet temperature would be 1350 C to achieve near-maximum fuel economy.
Document ID
19800016128
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Wagner, C. E.
(Chrysler Corp. Detroit, MI, United States)
Pampreen, R. C.
(Chrysler Corp. Detroit, MI, United States)
Date Acquired
September 4, 2013
Publication Date
June 1, 1979
Subject Category
Mechanical Engineering
Report/Patent Number
DOE/NASA/2749-79/3-VOL-3
COO-2749-40
NASA-CR-159672
Report Number: DOE/NASA/2749-79/3-VOL-3
Report Number: COO-2749-40
Report Number: NASA-CR-159672
Accession Number
80N24621
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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