| 摘要 |
A chain of components for transmitting electric power of an aircraft includes an auxiliary power unit (APU), main engines and end consumer systems via power networks and electronic connections controlled by a unit. The APU supplies power to a shaft by a connection to at least one energy converter unit, via a transmission unit, each converter unit comprising only one convertible electromechanical component. The transmission of power is effected by a direct connection to the transmission unit and to the end consumer system. The connection between a converter unit and the APU is provided by connecting the shaft of the APU to the shaft of the starter/generator (SG) via a directional transmission of power operating in one direction only from the shaft of the APU to the shaft of the SG. |
