Search NASA⌕ Search

Engineering topics

Huang, H. T.

Publications and source records attributed to Huang, H. T..

Microstructures of chemical vapor deposited high-purity tungsten achieved by two different precursors

Highlights: • CVD tungsten used as electron emitters of thermionic fuel elements was investigated. • Microstructures were characterized with metallography analysis. • The preferred orientation was determined with XRD and EBSD. • The surface morphology was observed with SEM and WLI. • Tungsten via thermolysis of WCl{sub 6} is better for thermionic fuel elements. - Abstract: Chemical vapor deposited (CVD) high-purity tungsten can be manufactured as electron emitters in thermionic fuel elements. Exposed surface planes of the emitter emit electrons and affect the efficiency and load capacity of the thermionic fuel element. In order to determine the electron emission planes of the emitter, the metallurgic structures, the preferred orientation and the as-deposited surface morphology of CVD tungsten have been investigated. In this work, high-purity (over 99.99%) tungsten was achieved by two different precursors: hydrogen reduction of tungsten hexafluoride (WF{sub 6}) and thermolysis of tungsten hexachloride (WCl{sub 6}). The microstructures of CVD tungsten were characterized by metallography analysis, X-ray diffraction (XRD), electron backscattered diffraction (EBSD), and white light interference (WLI). Tungsten fabricated by hydrogen reduction of WF{sub 6} and thermolysis of WCl{sub 6} has <100>-preferred columnar microstructures. However, the latter exhibits larger columnar grains and preferred <100> less. The preferred orientation is caused by the higher growth rate of the <100> orientation and competition between the <100> orientations of different grains. The as-deposited surface consists of tiny pyramids, with <100> axis and {111} side faces. In contrast to tungsten produced by hydrogen reduction of WF{sub 6}, the pyramid on tungsten synthesized via thermolysis of WCl{sub 6} contains small {110} facets on the four edges. Therefore, tungsten made via thermolysis of WCl{sub 6} is a better candidate for thermionic fuel elements, because the higher work function of {110} planes enables better output efficiency.

36 MATERIALS SCIENCE↗

Application of HOST technology to the SSME HPFTP blade

The development of turbine blade analysis tools as they moved from research contracts under the NASA HOST (Hot Section Technology) program to a PC-based system for preliminary design and to use in evaluating the SSME HPFTP (Space Shuttle Main Engine High Pressure Fuel Turbo Pump) blade is discussed. The heat transfer and structural analysis of the blade, the development of a data base for constitutive modeling of the blade materials, including coatings, and the use of advanced nonlinear finite element methods are addressed.

Mcknight, R. L.↗

3D inelastic analysis methods for hot section components

The objective is to develop analytical tools capable of economically evaluating the cyclic time dependent plasticity which occurs in hot section engine components in areas of strain concentration resulting from the combination of both mechanical and thermal stresses. Three models were developed. A simple model performs time dependent inelastic analysis using the power law creep equation. The second model is the classical model of Professors Walter Haisler and David Allen of Texas A and M University. The third model is the unified model of Bodner, Partom, et al. All models were customized for linear variation of loads and temperatures with all material properties and constitutive models being temperature dependent.

Dame, L. T.↗