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Advanced Turbine Technology Applications Project (ATTAP)The Advanced Turbine Technologies Application Project (ATTAP) is in the fifth year of a multiyear development program to bring the automotive gas turbine engine to a state at which industry can make commercialization decisions. Activities during the past year included reference powertrain design updates, test-bed engine design and development, ceramic component design, materials and component characterization, ceramic component process development and fabrication, ceramic component rig testing, and test-bed engine fabrication and testing. Engine design and development included mechanical design, combustion system development, alternate aerodynamic flow testing, and controls development. Design activities included development of the ceramic gasifier turbine static structure, the ceramic gasifier rotor, and the ceramic power turbine rotor. Material characterization efforts included the testing and evaluation of five candidate high temperature ceramic materials. Ceramic component process development and fabrication, with the objective of approaching automotive volumes and costs, continued for the gasifier turbine rotor, gasifier turbine scroll, extruded regenerator disks, and thermal insulation. Engine and rig fabrication, testing, and development supported improvements in ceramic component technology. Total test time in 1992 amounted to 599 hours, of which 147 hours were engine testing and 452 were hot rig testing.
Document ID
19960001641
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 6, 2013
Publication Date
December 1, 1993
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-195446
E-9499
NAS 1.26:195446
EDR-17038
DOE/NASA-0336-5
Report Number: NASA-CR-195446
Report Number: E-9499
Report Number: NAS 1.26:195446
Report Number: EDR-17038
Report Number: DOE/NASA-0336-5
Accession Number
96N11649
Funding Number(s)
CONTRACT_GRANT: DEN3-336
CONTRACT_GRANT: DE-AI01-90CE-50330
PROJECT: RTOP 778-32-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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