Servo-control device for controlling a control surface of an aircraft

Claim 2

A servocontrol device for controlling a control surface of an aircraft, which device is associated with a mechanical control member such as a control column, a wheel or pedals, and which comprises two identical double-acting hydraulic rams, integral with each other and each controlled by means of a slide valve, said slide valves each being controlled by a servovalve, whilst each servovalve is controlled by an electrical chain associated therewith, emitting an electrical control signal taking into account the displacements of said control member, wherein said chains are connected to each other by crossed connections and comprise means for delivering equal signals to said electrovalves, each chain comprising a by-two divider and three adders each having two inputs and one output, the first of said adders receiving said electrical control signal and a signal corresponding to the effective displacement of the control surface, whilst the second and third adders both receive the output signal of the first adders on one of their inputs, the other input of the second adder receiving the output signal of the first adder of the other chain and the other input of the third adder receiving the output signal of said second adder through said by-two divider, whilst the output signal of the third adder is supplied to a corresponding servovalve.

Claim 3

A device as claimed in claim 1, wherein a low-pass feedback circuit adapted to reintroduce an output signal with a delay is disposed between said output of the first adder an an auxiliary input thereof.

Claim 4

A device as claimed in claim 2, wherein there is disposed between the low-pass feedback circuit and the output of the corresponding first adder, an auxiliary adder receiving, on inputs of different signs, the output signal of said first adder and a signal coming from a slide valve position pick-up activated by the servovalve associated therewith.

Claim 5

A device as claimed in claim 2, wherein the low-pass feedback circuit presents a response of the form ##EQU6## in which p is the Laplace variable and τ a predetermined period of time.

Claim 6

A device as claimed in claim 2, comprising means for reintroducing, on an auxiliary input of the third adder of a chain, a part of the current passing through the corresponding servovalve.

Claim 7

A servocontrol device for controlling a control surface of an aircraft, which device is associated with a mechanical control member such as a control column, a wheel or pedals, and which comprises two identical double-acting hydraulic rams, integral with each other and each controlled by means of a slide valve, said slide valves each being controlled by a servovalve, whilst each servovalve is controlled by an electrical chain associated therewith, emitting an electrical control signal taking into account the displacements of said control member, wherein said chains are connected to each other by crossed connections and comprise means for delivering equal signals to said electrovalves, each chain comprising three adders each having two inputs and one output, the first adder receiving said electrical control signal and a signal corresponding to the effective displacement of the control surface, whilst the second and third adders both receive the output signal of the first adder on one of their inputs, the other input of the second adder receiving the output signal of the first adder of the other chain and the other input of the third adder receiving the output signal of said second adder whilst the output signal of the third adder is supplied to a corresponding servovalve, an electrical signal limiter being disposed between the output of the second adder and said other input of the third adder.

Claim 8

A servocontrol device for controlling a control surface of an aircraft, which device is associated with a mechanical control member such as a control column, a wheel or pedals, and which comprises two identical double-acting hydraulic rams, integral with each other and each controlled by means of a slide valve, said slide valves each being controlled by a servovalve, whilst each servovalve is controlled by an electrical chain associated therewith, emitting an electrical control signal taking into account the displacements of said control member, wherein said chains are connected to each other by crossed connections and comprise means for delivering equal signals to said electrovalves, each chain comprising three adders each having two inputs and one output, the first adder receiving said electrical control signal and a signal corresponding to the effective displacement of the control surface, whilst the second and third adders both receive the output signal of the first adder on one of their inputs, the other input of the second adder receiving the output signal of the first adder of the other chain and the other input of the third adder receiving the output signal of said second adder whilst the output signal of the third adder is supplied to a corresponding servovalve, an electrical signal limiter being disposed between the output of the second adder and said other input of the third adder.