| 摘要 |
An aircraft taxi system (100) includes a controllable voltage AC generator (103) configured to be connected to a power generation turbine shaft (102) and configured to convert rotational energy to electrical energy, wherein the controllable voltage AC generator (103) is configured to output a desired voltage irrespective of a change in a rotational speed of the power generation turbine shaft (102), an AC electric motor (105) configured to rotate at least one wheel of an aircraft landing gear, and an AC bus connecting the controllable voltage AC generator to each of the AC electric motor. |
