| 摘要 |
<p>An aircraft (1), capable of hovering, having drive means (7); and at least one exhaust duct (8, 8') connected to an outlet of the drive means (7) to expel the exhaust gas, produced by fuel combustion, from the aircraft. At least part of the exhaust duct (8, 8') has a thermoelectric conversion circuit (15) for Seebeck-effect converting to electric energy the thermal gradient produced between the inside and outside of the exhaust duct (8, 8') by flow of the exhaust gas. ( Figure 2 )</p> |
