Process for reducing aerodynamic loads applied to aircraft...

Details Process for reducing aerodynamic loads applied to aircraft... Process for reducing aerodynamic loads applied to aircraft...

B - Operations, Transporting

64

C

B64C 5/10 (2006.01) B64C 5/00 (2006.01) B64C 5/02 (2006.01) B64C 5/14 (2006.01) B64C 5/16 (2006.01) B64C 9/00 (2006.01) B64C 9/02 (2006.01) B64C 9/04 (2006.01) B64C 9/06 (2006.01) B64C 9/08 (2006.01) B64C 9/10 (2006.01) B64C 9/12 (2006.01) B64C 9/30 (2006.01) B64C 13/00 (2006.01)

Patent

CA 2489794

According to the invention, prior to the rotation, the adjustable horizontal tailplane (2) is nose-up overdeflected and the elevators (4) are nose-down deflected.

- Selon l'invention, préalablement à la rotation, on surbraque à cabrer l'empennage horizontal réglable (2) et on braque à piquer les gouvernes de profondeur (4).

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