DESCRIPTION OF THE DRAWINGS
FIG. 1A is a perspective view of a prior art ceramic honeycomb structure of which the invention is applicable to.
FIG. 1B is a plan view of an octant section of the honeycomb structure of FIG. 1A along the section lines 1B-1B.
FIG. 2A is an enlarged, finite element analysis of the upper-most circled area of FIG. 1B, illustrating the stress concentrations at the joint between an obliquely orientated web, and the inner edge of the outer skin of the structure.
FIG. 2B is an enlarged, finite element analysis illustrating the stress concentration associated with the joint between another obliquely orientated web, and the inner edge of the outer skin of the structure.
FIG. 3 is a plan view of an octant section of a first embodiment of the invention.
FIG. 4 is a plan view of an octant section of a second embodiment of the invention.
FIG. 5 is a half cross section of a third embodiment of the invention having an elliptical cross section.
FIG. 6 is a bar graph that graphically displays the percentage improvement (simulated) of the inventive honeycomb structure over the prior art honeycomb structure illustrated in FIGS. 1A and 1B in resistance to radial tension, radial compression, heat up thermal load, and cool down thermal load.
FIG. 7 is a finite element analysis illustrating the areas of maximum stress experienced by the several embodiments of the invention.