Control and power supply system for at least two airplane seats

Error detection/correction and fault detection/recovery – Data processing system error or fault handling – Reliability and availability

Reexamination Certificate

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Details

C714S022000

Reexamination Certificate

active

10485686

ABSTRACT:
A control and power supply system for the actuators of at least two airplane seats, which are preferably adjacent. The actuators of an airplane seat and the actuators of at least one other airplane seat are connected to a common control unit by a data link device. Each actuator can be supplied by at least two power units. In case of control unit failure, at least one actuator takes over the function of the control unit. For uncoupling defective parts of the corresponding bus structure, all the actuators are provided with elements for cutting the ingoing and outgoing data lines and power lines.

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