AIRCRAFT INCLUDING ELECTRIC STARTER-GENERATOR FOR EACH TURBOJET ENGINE AND CHASSIS EQUIPPED WITH A STEERING MOTOR

摘要

1. Aircraft containing the first turbojet engine (M1), equipped with a first electric starter-generator (DG1), and a landing gear (16), equipped with an electric motor (17) for taxiing on the ground, and the aircraft, characterized in that it includes an electric power converter (14) suitable for connection with a starter-generator or with an electric motor for taxiing through a configurable electric power distribution module (12). 2. The aircraft according to claim 1, characterized in that it further includes an auxiliary onboard power module (20) equipped with an electric power generator (22), and characterized in that the electric power generator is connected to an electric power distribution module (12) to power the converter ( 14) electricity. 3. Aircraft according to claim 1, characterized in that the power distribution module (12) further includes a power input (26) for external power to the converter. Aircraft according to claim 3, characterized in that the power distribution module (12) includes a configuration connecting the power input (26) to the converter input, and the converter output to the first starter-generator (DG1) operating as a starter. . Aircraft according to claim 2, characterized in that the power distribution module (12) includes a configuration that connects the output of the power generator to the input of the converter, and the output of the converter (14) to the first electric starter-generator (DG1) operating as a starter .6. The aircraft according to claim 1, characterized in that the power distribution module includes a configuration