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Status
Electronic Resource
Call number
Publication
DOE NASA 0336 1; Report; June 1989.
Language
Library's review
ABSTRACT:
ATTAP activities during the past year were highlighted by an extensive materials assessment, execution of a reference powertrain design, test-bed engine design and development, ceramic component design, materials and component characterization, ceramic component process development and
ATTAP activities during the past year were highlighted by an extensive materials assessment, execution of a reference powertrain design, test-bed engine design and development, ceramic component design, materials and component characterization, ceramic component process development and
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fabrication, component rig design and fabrication, test-bed engine fabrication, and hot gasifier rig and engine testing. Although significant technical challenges remain, all areas experienced progress. Materials assessment activities entailed engine environment evaluation of domestically supplied radial gasifier turbine rotors that were available at the conclusion of the Advanced Gas Turbine (ACT) Technology Development Project as well as an extensive survey of both domestic and foreign ceramic suppliers and Government laboratories performing ceramic materials research applicable to advanced heat engines. A reference powertrain design was executed to reflect the selection of the AGT-5 as the ceramic component test-bed engine for the ATTAP. Test-bed engine development activity focused on upgrading the AGT-5 from a 1038 degrees C (1900 degrees F) metal engine to a durable 1371 degrees C (2500 degrees F) structural ceramic component test-bed engine. Ceramic component design activitie1 included the combustor, gasifier turbine static structure, and gasifier turbine rotor. The materials and component characterization efforts have included the testing and evaluation of several candidate ceramic materials and components being developed for use in the ATTAP. Ceramic component proce1a development and fabrication activities were initiated for the gasifier turbine rotor, gasifier turbine vanes, gasifier turbine scroll, extruded regenerator disks, and thermal installation. Plans for 1989 include delivery of gasifier turbine rotors, vanes and scrolls, injection moldable thermal insulation, and extruded regenerator matrix samples. Component rig development activities included combu1tor, hot ga1ifier, and regenerator rigs. Test-bed engine fabrication activities consisted of the fabrication of an all-new AGT-5 durability test-bed engine and support of all engine test activities through instrumentation/build/repair. Hot gasifier rig and test-bed engine testing activities were performed. Show Less