| 摘要 |
<p>The device (20) has a protective plate (21) intended to be interposed between a fuselage (2) and a pyramid-shaped structure. A blade (30) is secured to the protective plate for exerting a force on each rear arm (12) of the structure, so as to break the arm. A chevron (40) includes two branches connected to the protective plate, so as to tend to move each front arm (14) of the structure transversely apart from each other. The protective plate extends longitudinally from a front free end to a rear free end, where the blade and the chevron are arranged between the front and rear free ends. Independent claims are also included for the following: (1) a fastener system for fastening a load to a fuselage of a rotorcraft (2) a rotorcraft (3) a method for protecting a fuselage of a rotorcraft against a pyramid-shaped structure for carrying a load.</p> |
