A novel heavily doped drift-auxiliary cathode lateral insulated gate transistor structure

A novel CMOS-compatible, heavily doped drift auxiliary cathode lateral insulated gate transistor (HDD-ACLIGT) structure is analyzed using two-dimensional device simulation techniques. Simulation results indicate that low on-resistance and a fast turn-off time of less than 50 ns can be achieved by incorporating an additional n+ region which is self-aligned to the gate between the p+ auxiliary cathode and the p well, together with an extended p buried layer in an anode-shorted modified lateral insulated gate transistor (MLIGT) structure. The on-state and its transient performance are analyzed in detail. The on-state performances of the HDD-ACLIGT and the MLIGT are compared and discussed. The results indicate that the HDD-ACLIGT structure is well suited for HVICs. The device is also well suited for integration with self-aligned digital CMOS.

High-frequency acousto-electric single-photon source

We propose a single optical photon source for quantum cryptography based on the acoustoelectric effect. Surface acoustic waves (SAWs) propagating through a quasi-one-dimensional channel have been shown to produce packets of electrons that reside in the SAW minima and travel at the velocity of sound. In our scheme, the electron packets are injected into a p-type region, resulting in photon emission. Since the number of electrons in each packet can be controlled down to a single electron, a stream of single- (or N-) photon states, with a creation time strongly correlated with the driving acoustic field, should be generated. ©2000 The American Physical Society.

The effects of a trip wire and unsteadiness on a high speed highly loaded low-pressure turbine blade

This paper presents the effect of a single spanwise 2D wire upon the downstream position of boundary layer transition under steady and unsteady inflow conditions. The study is carried out on a high turning, high-speed, low pressure turbine (LPT) profile designed to take account of the unsteady flow conditions. The experiments were carried out in a transonic cascade wind tunnel to which a rotating bar system had been added. The range of Reynolds and Mach numbers studied includes realistic LPT engine conditions and extends up to the transonic regime. Losses are measured to quantify the influence of the roughness with and without wake passing. Time resolved measurements such as hot wire boundary layer surveys and surface unsteady pressure are used to explain the state of the boundary layer. The results suggest that the effect of roughness on boundary layer transition is a stability governed phenomena, even at high Mach numbers. The combination of the effect of the roughness elements with the inviscid Kelvin-Helmholtz instability responsible for the rolling up of the separated shear layer (Stieger [1]) is also examined. Wake traverses using pneumatic probes downstream of the cascade reveal that the use of roughness elements reduces the profile losses up to exit Mach numbers of 0.8. This occurs with both steady and unsteady inflow conditions.