| 摘要 |
FIELD: transport. ^ SUBSTANCE: set of invention relates to aircraft electric power supply circuit. Proposed circuit comprises power distribution circuit 16 and electric hardware supply circuit 5b, and electric power generator 27 incorporates with aircraft engine to supply anti-icing circuit 5a. Electric hardware comprises nacelle consuming components 5b connected DC voltage distribution with bus 35 connected with voltage converter circuit 34 supplied by distribution circuit 17. Anti-icing circuit 5a comprises, at least, one resistor 61 to dissipate electricity sent back to DC voltage distribution circuit 35 by, at least, some of nacelle consuming components. Aircraft comprises above described power supply circuit. ^ EFFECT: simplified design, reduced power consumption and power losses. ^ 9 cl, 3 dwg |
