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AIRCRAFT PROVIDED WITH A DEVICE FOR ASSISTING THE PILOT WHEN CARRYING AN EXTERNAL LOAD WITH A SLING, AND A METHOD IMPLEMENTED BY SAID DEVICE
AIRCRAFT PROVIDED WITH A DEVICE FOR ASSISTING THE PILOT WHEN CARRYING AN EXTERNAL LOAD WITH A SLING, AND A METHOD IMPLEMENTED BY SAID DEVICE
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机译:提供有用于在利用吊索承载外部载荷时辅助驾驶员的装置的飞机以及由所述装置实施的方法
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摘要
The present invention relates to an aircraft (1) having a sling (3) fastened to a fastening point (9), a local transverse vertical plane (P1) containing said fastening point (9) being parallel to a yaw axis (AX1) and to a pitch axis (AX2), a local longitudinal vertical plane (P2) containing said fastening point (9) being parallel to a yaw axis (AX1) and to a roll axis (AX3), said local longitudinal and transverse vertical planes (P2 and P1) intersecting at a vertical axis (AX4). The aircraft (1) is provided with a piloting assistance device (10) comprising firstly main determination means (20) for determining a first main angle (α1) between said vertical axis (AX4) and a first primary projection (3′) of said sling (3) on said local transverse vertical plane (P1) and a second main angle (α2) between said vertical axis (AX4) and a second primary projection (3″) of said sling (3) on said local longitudinal vertical plane (P2); and secondly display means (30) provided with a display screen (31) for quantitatively displaying said first and second main angles (α1, α2).
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