| 摘要 |
<p>The microlight aircraft comprises a main one-piece beam (4) which is shaped to receive semi-rigid delta or rectangular wings. The front part of the beam incorporates a jib-shaped upright (7), the rear face of which carries the mechanism for adjusting the angle of the main wing (1). The rear part of the beam houses the engine (15) and incorporates a second upright which is lower than the front upright and supports the rear wing (2).</p> |
