| 摘要 |
FIELD: power engineering. ^ SUBSTANCE: in an aviation power plant with a generator of fuel elements, comprising a generator on fuel elements, a stabiliser, the first DC-DC converter, the first inverter, three switching elements and a unit of automatic monitoring and control, additionally the second DC-DC converter is introduced, as well as the second inverter and a protection unit, the first, second and third outputs of which are connected to appropriate inputs of switching elements, and at the same time it is connected to the fourth output of the automatic monitoring and control unit, the first, second and third outputs of which are the outputs of devices, besides, the generator output is the input of the stabiliser, the output of which is the input of the first DC-DC converter, the output of which via switching elements is connected in parallel to the inputs of the second DC-DC converter, the first and second inverters, the outputs of which are the inputs of the automatic monitoring and control unit. ^ EFFECT: conversion of fuel elements energy into electric energy of higher quality with specified output parameters for reliable supply of aircraft air-borne loads by all types of electric current, excluding supply of voltage in case of emergencies. ^ 1 dwg |
