Control arrangement for controlling actuators arranged in rotor blade of aircraft i.e. helicopter, has control device connected with groups of actuators by interface connecting units, respectively

摘要

The arrangement has a control device connectable with a body of an aircraft i.e. helicopter. An interface is arranged in a connecting path system from the control device to actuators (30) and has a set of interface connecting unit. A rotor blade (5) is provided with two groups of actuators (31a-31c, 32a-32c). The control device is connected with the groups of actuators by the interface connecting units, respectively. The control device and the interface are designed to supply the groups of actuators with energy via the interface and via two control units. Independent claims are also included for the following: (1) a method for controlling a set of actuators arranged at a rotor blade (2) a computer program comprising a set of instructions for performing a method for controlling a set of actuators arranged at a rotor blade (3) a Computer-readable medium comprising a set of instructions for performing a method for controlling a set of actuators arranged at a rotor blade.