1. Field of the Invention
Embodiments of the invention relate to semiconductor devices manufactured with silicon carbide and methods of manufacturing such devices. One particular embodiment of the invention relates to the manufacture of MOSFETs (metal-oxide-semiconductor field effect transistors) using silicon carbide. Embodiments of the invention also relate to aircraft power distribution systems that utilise such MOSFETs.
2. Description of Related Art
The use of silicon carbide, SiC, in the manufacture of MOSFETs provides a number of benefits over traditional silicon substrates. For example, SiC has very high strength and does not melt at any known pressure and is chemically highly stable. Further, SiC allows the production of devices having a lower on-state resistance than silicon devices. Thus SiC lends itself to use in high power MOSFETs.
One problem associated with the manufacture of MOSFETS using SiC is that it has not been possible to make a channel region of the MOSFET with high enough quality to produce viable devices that are sufficiently reliable for practical use. In a MOSFET, the channel region lies beneath the oxide layer at the gate of the MOSFET, and when the MOSFET is switched on the channel region allows the flow of current through the device. Previous attempts to produce SiC MOSFETs have been subject to the problem of carbon gettering at the interface, whereby carbon impurities are thrilled at the interface, adversely affecting the electrical behaviour of the device.
U.S. Pat. No. 5,744,826 discloses a process for producing silicon carbide semiconductor devices, such as MOSFETs, wherein a gate insulating film is formed on the surface of a SiC semiconductor layer, by thermal oxidation of the SiC layer.
In order to provide the required electrical properties in the channel region, it is important that a good quality interface is defined between the oxide and the SiC beneath it.
According to embodiments of the present invention, there is provided a method of manufacturing a semiconductor device comprising applying a first layer comprising silicon to a second layer comprising silicon carbide, whereby an interface is defined between the first and second layers, and oxidising some or all of the first layer.
By virtue of applying the first layer comprising silicon to the second layer comprising SiC, the quality of each surface of the first and second layers can be independently ensured, thereby resulting in high quality of each surface, and especially the interface between the layers. Further, as this process does not oxidise any SiC, the problems associated with carbon gettering at the interface are overcome. Thus the interface provided by embodiments of the present invention is of high quality. Naturally, great care is needed in the preparation of the SiC layer as high levels of cleanliness and flatness are desired.
Wafer bonding can be used to attach the first and second layers to one another. In wafer bonding, a thin layer of single crystal silicon is transferred from a carrier wafer on to the surface of another target wafer, in this case the SiC layer. The transferred layer is of high quality, so it can be oxidised to form an oxide of correspondingly high quality.
Further, embodiments of the present invention provide a semiconductor device manufactured according to the above described method comprising a first layer comprising SiO2 joined to a second layer comprising silicon carbide, whereby an interface is defined between the first and second layers. Additionally, an embodiment of the invention provides an aircraft power distribution system including such a semiconductor device.
There follows a detailed description of embodiments of the invention by way of example only with reference to the accompanying drawings, in which:
Following the completion of the oxidation process, the SiO2 layer 16 is etched away in regions 26,27 shown in
SiC MOSFETs embodying the present invention are particularly suited for use in aircraft power distribution systems. The issue of aircraft wiring safety has received widespread attention in recent years. Both “smoke in the cockpit” and arcing events are relevant here, and efforts are being made to improve the safety of such systems. Aircraft electric power systems are exposed to a wide range of disturbances, which may initiate such events. These include current and voltage transients and short-circuit conditions, arising from equipment failure and lightning strikes, for example. Electro-mechanical circuit breakers have traditionally been used to protect against such faults; however many of the faults are below the time protection curve threshold designed to protect the power system.
SSPC's (Solid State Power Controllers) can replace electro-mechanical controllers and provide improved performance, including very fast response, limiting the fault current within safe limits, and a long multi-operation life span. They further allow a flexible construction and control scheme, being fully controllable for both functions of current limiting and interruption. SSPCs also are of low cost and require minimal maintenance.
Generally, MOSFETs have a very low on-state resistance, allowing a low voltage drop and hence a small power dissipation (as heat) during operation. However, in order to be able to withstand the short-circuit or fault current for the designated time, a plurality of MOSFETs may have to be placed in parallel to enable the devices to withstand the associated energy losses. There are two principal constraints in action: (1) The steady-state cooling requirements, i.e. size, mass and heat transfer, are defined by normal operation, and (2) the number of devices in parallel is defined by fault conditions; in this case the high power dissipation levels will not act for long enough to heat up the external contact to the devices (i.e. the case), due to the short time of action and the diffusion of heat from the semiconductor device itself to the case. In other words, if there are not enough SSPCs provided in the system, excessive heating can occur during fault conditions. Reducing the number of parallel MOSFETs, and thus giving improvements in size and mass, would be acceptable for normal operation; however this would not allow the fault conditions to be safely contained.
MOSFET devices manufactured using SiC as provided by embodiments of the present invention provide a solution to this problem as they have a much smaller on-state resistance than corresponding Si devices. Improved sensitivity to fault currents can thereby be provided, as well as reduced I2R heating. Silicon carbide is also a much better thermal conductor and has a higher melting/sublimation temperature than Si and so is able to run hotter, thus reducing the requirement for heavy heatsink arrangements. Together, the material advantages of silicon carbide allow much higher power densities to be achieved.
Number | Date | Country | Kind |
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1015595.0 | Sep 2010 | GB | national |