Single-channel more electric aircraft power system framework
A technology of multi-electric aircraft and power supply system, which is applied in the direction of emergency power supply arrangements, electrical components, circuit devices, etc., can solve the problems of inconvenient assembly and complex structure of onboard power distribution devices, and achieve the effect of improving power levels
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[0047] The present invention will be further described in detail below through specific embodiments in conjunction with the accompanying drawings. It should be noted here that the descriptions of these embodiments are used to help understand the present invention, but are not intended to limit the present invention. In addition, the technical features involved in the various embodiments of the present invention described below can be combined with each other as long as they do not constitute a conflict with each other.
[0048] See figure 1 , the figure shows the power system architecture of a new type of single-channel multi-electric aircraft.
[0049] The bus bar L 235VAC Bus is selectively powered by one of the main generator GEN L, the auxiliary generator APU GEN and the main generator GEN R.
[0050] The bus bar R 235VAC Bus is selectively powered by one of the main generator GEN R, the auxiliary generator APU GEN and the main generator GEN L.
[0051] There are two co...
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