发明名称 |
Climb-optimized auto takeoff system |
摘要 |
The Climb-Optimized Takeoff System is an aircraft functionality aimed at improving the takeoff performance. The improvement is obtained by allowing the airplane to rotate to an optimized pitch attitude at and after VR, while ensuring that the minimum required takeoff climb gradients and the geometric limitations of the airplane are being respected. The optimum takeoff performance is obtained by granting that the airplane pitch attitude, instead of being limited by a single takeoff constraint (such as a given pitch to avoid tail strike) is being tracked to its instantaneous, most constraining limit during the air transition phase (d2). |
申请公布号 |
EP2533122(A2) |
申请公布日期 |
2012.12.12 |
申请号 |
EP20120170788 |
申请日期 |
2012.06.05 |
申请人 |
EMBRAER , S.A. |
发明人 |
GUEDES, PATRICE LONDON;WALLACH, RICARDO;VERHALEN, GUILHERME MAXIMILIANO;DA CUNHA RONCONI, SALVADOR JORGE |
分类号 |
G05D1/06 |
主分类号 |
G05D1/06 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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