Data processing: vehicles – navigation – and relative location – Vehicle control – guidance – operation – or indication – Aeronautical vehicle
Reexamination Certificate
2005-08-09
2005-08-09
Camby, Richard M. (Department: 3661)
Data processing: vehicles, navigation, and relative location
Vehicle control, guidance, operation, or indication
Aeronautical vehicle
C701S014000, C244S075100
Reexamination Certificate
active
06928340
ABSTRACT:
An electric control system (1) comprises a control unit (4) which comprises a member (5) able to be actuated by a pilot and a means of load-wise protection (7), and which delivers a first deflection order representative of the action exerted by the pilot on the member (5), and of the contribution made by the means of load-wise protection (7), an actuator (11) which moves said control surface (2) about an axis (Z—Z), as a function of a deflection order, and a correction device (12) which comprises a means (13) for determining a second deflection order making it possible to limit the load, to which a stabilizer element of the aircraft is subjected, to a maximum load, and a means (14) for choosing one of the first and second deflection orders, which is transmitted to said actuator (11) so as to move said control surface (2).
REFERENCES:
patent: 5170969 (1992-12-01), Lin
patent: 5375794 (1994-12-01), Bleeg
patent: 6209825 (2001-04-01), Scott
patent: 6338454 (2002-01-01), Rollet et al.
patent: 6539290 (2003-03-01), Vos
patent: 2002/0022910 (2002-02-01), Kubica et al.
patent: 2809373 (2001-11-01), None
Cassein Guillaume
Van De Kreeke Marc
Airbus France
Stevens Davis Miller & Mosher LLP
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