| 摘要 |
<p>A fuel system (1A) is provided with a constant volume pump (2c) that pressurizes and discharges fuel (N) that is supplied to an aircraft engine (E). The fuel system (1A) is additionally provided with a transmission (2d) that: connects the engine (E) with the constant volume pump (2c), changes the rotational speed of rotational power that is output from the engine (E), and transmits the result to the constant volume pump (2c); and that makes it possible to adjust gear ratio.</p> |
