A high performance 0.12 /spl mu/m CMOS with manufacturable 0.18 /spl mu/m technology
High-performance 0.12 /spl mu/m CMOS devices with manufacturable 0.18 /spl mu/m technology are presented. A nominal I/sub dsat/N/P of 950/410 /spl mu/A//spl mu/m at an I/sub off/ of 12 nA//spl mu/m is achieved by reducing the body effect. The double-sidewall structure developed can reduce gate-fringe capacitance without increasing the junction leakage, and the inverter delay of 11 ps/stage is achieved at a nominal L/sub gate/ of 0.12 /spl mu/m. Small 6T-SRAM cells of 3.1 /spl mu/m/sup 2/ with 0.5 /spl mu/m gate pitch are implemented using a vertical well isolation and a self-aligned contact (SAC). In the SAC process, a blanket Si/sub 3/N/sub 4/ layer used as an etching stopper is optimized for the I/sub dsat/N/P ratio and the negative bias temperature instability (NBTI) reliability. The 9-level interconnection is optimized to reduce a long wire RC-delay.
Improvement of thermal stability of via resistance in dual damascene copper interconnection
Thermal stability of via resistance in the multilevel dual damascene Cu interconnection was investigated. The via resistance stability strongly depends on via size, via density and width of connecting Cu wires. The significant via-resistance shift was introduced by stress-induced voiding. To avoid the voiding failure, optimization of heat treatments after electroplating (EP)-Cu deposition are necessary for both stability of Cu films and adhesion of barrier layer with Cu. Thermal stress balance between Cu wires and inter-level-dielectric (ILD) is also important to suppress the via degradation. The dual damascene structure with lower-stress and lower-Young's modulus ILD films such as FSG can provide wider process windows for the stability of the via resistance.
Knocking in an Internal-Combustion Engine
The question remains open of the relation between the phenomena of knocking in the engine and the explosion wave. The solution of this problem is the object of this paper. The tests were conducted on an aircraft engine with a pyrex glass window in the cylinder head. Photographs were then taken of various combinations of fuels and conditions.