A 1 ： 2 demultiplexer（DEMUX） that is fabricated using 0. 18 μm CMOS （complementary metaloxide-semiconductor transistor） technology is presented. The DEMUX consists of a master-slave-slave, masterslave D flip-flo...A 1 ： 2 demultiplexer（DEMUX） that is fabricated using 0. 18 μm CMOS （complementary metaloxide-semiconductor transistor） technology is presented. The DEMUX consists of a master-slave-slave, masterslave D flip-flops and output buffers. The D flip-flop employs a dynamic-loading structure and common-gate topology with single clock phase for the bias transistors. The dynamic-loading structure can make the circuit work faster because it decreases the charge/discharge time of the output node, and it consumes lower power because its working current is in a switch mode. In addition, the positive feedback loop, which is made up of a cross-coupled transistor pair in the latch, speeds up the circuit. Measurement results at 20 Gbit/s 2^23 - 1 pseudo random bit sequence （PRBS） via on-wafer testing show that the 1： 2 DEMUX can operate well. The power dissipation is 108 mW with the area of 475μm×578μm.展开更多
In this paper a numerical investigation has been presented on the stall mechanism of a highly loaded Single Stage Low Speed Fan designed for the research test facility to be installed at North Western Polytechnic Univ...In this paper a numerical investigation has been presented on the stall mechanism of a highly loaded Single Stage Low Speed Fan designed for the research test facility to be installed at North Western Polytechnic University (NWPU) Xi’an, China. The results presented are for the design point, near stall and just stall operating conditions at design speed. Design point studies have been found to be an indicative of stall area. Unsteady method of domain scaling has been used to compute the results at near stall and just stall conditions. It has been found that unlike the conventional tip leakage flow of the rotor, stator hub section is mainly responsible for the stall of the fan. The flow mechanism has been discussed with correlation to the design variables and previous investigations. Commercial CFD code NUMECA FINE/Turbo has been used for computations; results have been compared with results obtained from commercial CFD code ANSYS-CFX. The loss prediction of latter code is conservative than the former. The stall mechanism predicted by both codes is analogous.展开更多
文摘A 1 ： 2 demultiplexer（DEMUX） that is fabricated using 0. 18 μm CMOS （complementary metaloxide-semiconductor transistor） technology is presented. The DEMUX consists of a master-slave-slave, masterslave D flip-flops and output buffers. The D flip-flop employs a dynamic-loading structure and common-gate topology with single clock phase for the bias transistors. The dynamic-loading structure can make the circuit work faster because it decreases the charge/discharge time of the output node, and it consumes lower power because its working current is in a switch mode. In addition, the positive feedback loop, which is made up of a cross-coupled transistor pair in the latch, speeds up the circuit. Measurement results at 20 Gbit/s 2^23 - 1 pseudo random bit sequence （PRBS） via on-wafer testing show that the 1： 2 DEMUX can operate well. The power dissipation is 108 mW with the area of 475μm×578μm.
文摘In this paper a numerical investigation has been presented on the stall mechanism of a highly loaded Single Stage Low Speed Fan designed for the research test facility to be installed at North Western Polytechnic University (NWPU) Xi’an, China. The results presented are for the design point, near stall and just stall operating conditions at design speed. Design point studies have been found to be an indicative of stall area. Unsteady method of domain scaling has been used to compute the results at near stall and just stall conditions. It has been found that unlike the conventional tip leakage flow of the rotor, stator hub section is mainly responsible for the stall of the fan. The flow mechanism has been discussed with correlation to the design variables and previous investigations. Commercial CFD code NUMECA FINE/Turbo has been used for computations; results have been compared with results obtained from commercial CFD code ANSYS-CFX. The loss prediction of latter code is conservative than the former. The stall mechanism predicted by both codes is analogous.
