Method and device for controlling and braking an aircraft...

Fluid-pressure and analogous brake systems – Speed-controlled – Automatic braking including speed governor or hydraulic...

Reexamination Certificate

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C303S009620, C303S113500

Reexamination Certificate

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11101414

ABSTRACT:
Method and device for controlling and braking an aircraft running on the groundAccording to the invention, the aircraft (1) comprises two close undercarriage wheel assemblies (2D,2G) and two distant undercarriage wheel assemblies (3D,3G), the biggest of the braking commands (FD, FG) can, under certain conditions, be applied not only to the corresponding two undercarriage wheel assemblies, but also to the close undercarriage wheel assembly corresponding to the smallest braking command.

REFERENCES:
patent: 4006941 (1977-02-01), DeVlieg
patent: 4923056 (1990-05-01), Nedelk
patent: 5172960 (1992-12-01), Chareire
patent: 5217282 (1993-06-01), Guichard
patent: 5397173 (1995-03-01), Bourguet
patent: 5417477 (1995-05-01), Lasbleis
patent: 5845975 (1998-12-01), Wells
patent: 6029931 (2000-02-01), Encarthe et al.
patent: 6604708 (2003-08-01), DeVlieg
patent: 6663192 (2003-12-01), Bourguet et al.
Preliminary Search Report dated Sep. 29, 2004 with English translation.

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